International Astronomical Union IOU Stupidity File

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    Arabs real time AstronomyThe 30 solutions of Mercurys Perihelion

    (I/O) 0 = 0 + [(I O)/O] 0Real time physics = event time physics + time delay physics

    Quantum = classical + relativisticjoenahhas1 [email protected]

    My name is Professor Joe Nahhas Re- founder of Arabs real time physics July 4th 1973There is one and only one physics Arabs real time physics

    his is me in October 2009 flashing my 1979 picture stapled to my thermo book congratulatmyself on 1001 new Arabs real time physics formulas to change physics and history

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    mailto:[email protected]:[email protected]
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    2 = 2 is self evidentImage = image = I is self evident line - 1Object = object = O = self evident line - 2And, - Object = - objects = - O = self evident line - 3I = I line - 1

    O = O line - 2And, - O = - O line - 3Adding: line - 1 and line - 2 and line - 3I + O O = O + (I O) line - 4I = O + (I O); O O = 0 one left side(I/O) = (O/O) + (I O)/O; dividing by on both sides line - 5Or, (I/O) = 1 + (I O)/O; O/O = 1 line - 6(I/O) O = O + [(I O)/O] O Line - 7Real time object = event time Object + time delay objectReal time astronomy = event time astronomy + time delay astronomy

    Car size at distance 4

    Car size at distance 3

    R1 R2 O2 Car size at distance 2

    D D D

    R1 O1 d

    R1 Car size at distance 1

    Observer line: Observer The image ofR1 is R2; or R2 in real time is R1

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    Let us do R1 real time analysis

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    R2 = R2R2 = R1 + (R2 R1)

    Dividing by R1(R2/R1) = (R1/R1) + (R2 R1)/ R1

    Visual measurement scale

    (R2/R1) = 1 + [(R2 R1)/ R1]Distance R1 when measured using light source and not a measuring tape is not the sameas R1 but is measured as R2. R2 is the visual distance of R1. Using an eye as an instrument

    visual distance R2 is smaller than actual distance R1. The percentage of visual distance R2 toactual distance R1 is equal to (R2/R1).

    (R2/R1) = 1 + [(R2 R1)/ R1] = 1 + [(R2/ R1) 1]Percentage = 1 + [percentage 1]

    Multiplying by R1(R2/R1) R1 = R1 + [(R2 R1)/ R1] R1Visual = actual + (Visual actual)

    In clear words when we try to measure the distance R1 using light source reflected fromthe car we see a percentage of R1 which is (R2/R1) R1 and that percentage times R1 is the

    visual we measure R2Real time distance = event time distance + delay time distance

    Visual distance = distance + visual effect

    Visual measurement scale using distanceReal time astronomy scale using distance

    (R2/R1) = 1 + [(R2 R1)/ R1]Visual measurement scale using VelocityReal time astronomy scale using distance

    (V2/V1) = 1 + [(V2 V1)/ V1]

    Visual measurement scale using angleReal time astronomy scale using angle( 2/ 1) = 1 + [( 2 1)/ 1]

    Visual measurement scale using angular velocityReal time astronomy scale using angular velocity

    ( 2/ 1) = 1 + [( 2 1)/ 1]Visual measurement scale using timeReal time astronomy scale using time

    (t 2/ t 1) = 1 + [(t 2 t 1)/ t 1]

    This formula is real time astronomical scale(V/A) = 1 + [(V A)/ A]

    (Visual/Actual) = 1 + [(Visual Actual)/ Actual]

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    Arabs real time astronomy application

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    (I/O) 0 = 0 + [(I O)/O] 0

    Real time physics = event time physics + time delay physics

    In old termsQuantum = classical + relativistic

    (R2/R1) = 1 + [(R2 R1)/ R1]

    (R2/R1) 0 = 0 + [(R2 R1)/ R1] 0

    This is Arabs real time astronomy distance scale to measure the angular velocity 0(V2/V1) = 1 + [(V2 V1)/ V1]

    (V2/V1) 0 = 0 + [(V2 V1)/ V1] 0

    This is Arabs real time astronomy Velocity Scale to measure the angular velocity 0Planet Mercury angular velocity accumulation in arc second per hundred years

    Or, (V2/V1) 0 = 0 + [(V2 V1)/ V1] 0Planet Mercury Angular velocity 0 = 2 /Tm = 2(3.1415)/88 x24x3600Tm = Planet Mercury orbital period = 88 days = 88 x 24 x 3600 seconds

    Planet Mercury angular velocity accumulation in arc second percentury is: 0 = (2 / Tm) (1 century/Tm) (180/ ) (3600)

    Or, 0 = (2 / Tm) (1 century/Tm) (180/ ) (3600)= (2x3.1415/88x24x3600) (36526days/88days) (180/3.1415) (3600)= 70.75

    (R2/R1) 0 = 0 + [(R2 R1)/ R1] 0(R2/R1) 0 = 0 + [(R2 R1)/ R1] 0

    What we see = what there is + visual illusionModern astronomers see = 70.75 + 43What there is = 70.75The visual Illusion is = 43

    [(R2 R1)/ R1] 0 = 43Page 5

    As an example: when Astronomers look at planetary motion around the sun andthey saw the angular velocity in arc second per century:

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    Visual = actual + IllusionsVisual = actual + (visual actual)Quantum = classical + relativisticReal time classical = classical + relativistic illusionsQuantum mechanics and relativity theory is 20th century Garbage for physics.

    Measurements = actual + errorsActual + errors = actual + errors

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    Chapter TwoThe confrontation between Arabs real time Astronomy andWestern Nobel prize winner modern space time astronomy

    Arabs astronomers:

    0

    M Mercury S Sun

    That:

    1- All object classified as planets Suns Moons has a real time circular motionAs:r = r 0 e (+ t)And not1 Kepler - Newtons ellipse r= [a (1 - )/ (1 + cosine )] Or Einsteins rotating ellipse: r= a (1 - )/ [1 + cosine ( - )]

    2- The difference between two real time circular motions is a visual rotating ellipseOr,the difference between r1 = r 10 e [ (1)+ (1) t]and r2 = r 20 e [ (2)+ (2) t]Is Arabs real time ellipse: r= [a (1 - )/ (1 + cosine )]e [+ t]

    3 - Suns moons planets do not rotate around each otherThat is: r= [a (1 - )/ (1 + cosine )]e [+ t]

    Is a visual ellipse4 Gravity does not exist between planets moons and sunThat Newtons F = - G m M/r is wrongThat Einsteins F = - G m M/r + k/r4 is wrong

    5 Gravity is due to atmosphere density and spin periodThat G = G [, T] = G [atmospheric density, spin period]

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    In short: Arabs real time astronomy says

    500 years ago Europeans took 10th century Arabs real time Astronomy and changed it to Space- timeastronomy and in the process physics was changed from an Arabic science to European western stupidity

    globalized through planet of the Apes Institution and best known as Alfred Nobel Prize winner InstitutionPage 7

    Alfred Nobel Prize winner physics theoryApe Man Modern Physicist Nobel Prize winner physicist Ape Ass.

    Alfred Nobel: The Man behind the Nobel Prize; Joe Nahhas: The Man after Alfred Nobel Institution headSince 1901, the Nobel Prize has been honoring men and women from all corners of the globe foroutstanding achievements in physics. The foundations for the prize were laid in 1895 when Alfred Nobelwrote his last will, leaving much of his wealth to the establishment of the Nobel Prize. But who wasAlfred Nobel? Meet Alfred Nobel - scientist, inventor, entrepreneur, author and pacifist. What is modern

    physics? Did anyone hear the big bang? Did anyone saw a black hole? Did anyone find Einsteins gravitywaves? Did anyone hook up a hose to the sky and found dark energy to verify E = mc2? Does anyonehave a proof of Newtons action at a distance? Does anyone have a proof of Einstein time travel? Doesanyone figure out why humans have to accept Alfred Nobel prize winners claim that the universe is madeup of particles that dies and rebirth billion billion times a second? Hey dude I am a redneck onegrandfather was a damn farmer and my other grandfather was a damn Carpenter and my father was aCarpenter by inheritance but I never knew what a dumb ass really is till I met my science teacher! Whatdid Alfred Nobel honor? The difference between an Alfred Nobel Prize winner physicists and fortunetellers is a flip of a coin. Space - Time is not physics but Alfred Nobel physicists flip of a coin between acrime and stupidity. Alfred Nobel Institution honored criminals in Alfred Nobel suit for all of pastcentury. Modern space time physics changed physics from science to stupidity and physicists from

    researchers to criminals. In writing: Yes I am after Alfred Nobel Institution head on my plate and Iaccept nothing less. Space time physics is stupidity itself. Ending Nobel Prize for stupidity from

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    classrooms and scientific calculations is the only Nobel thing left to do. Alfred Nobel Prize became 1001times more worth in cash value. Big Institutions backed wrong physics and physicists for all of pastcentury for a prize and a billion dollars jack pot and garbage for physics. I am Joe Nahhas and I amunknown to the world of physics but I have 1001 new physics formulas to cut Alfred Nobel Institutionhead and delete Alfred Nobel Prize winner physics and physicists without loss of subject. This book is

    just the beginning and it is prime time and it is Arabs real time astronomy

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    Chapter three: 10th century Arabs real time astronomyArab Physicists of Baghdad of 950 Ad had said:

    I: Measurements are made along the line of sight or line of measurement

    Arabs in 950 AD said that light going vertical (blue) to the eye it will go through the eye be seen. The Arabs added that light coming oblique (pink) to the line of sight (blue line) would see the part of light (pink) that is equal to the amount of light of horizontal amoun(blue) or its vertical projection. What the Arabs concluded is that human eye and machinare unidirectional that can only recognize the amount of light along the line of sight or linof measurements. The Arabs mean that any point on the oblique pink line will be measuras its vertical projection as the blue line. The Arabs added that the horizontal projection the pink line is the amount that would be measured as Zero or not seen at all. A point

    location on the pink line would be measured as equal to its vertical projection on the blueline and that part would be seen detected and measured by the eyes and instruments anits horizontal projection would not be detected or measured by the eyes or instruments awould be completely missed.

    r0sine t r0

    t

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    r0cosine tThe angle between the pink line and the blue line is called light aberration angle. Theaberration angle between the line where an object is (pink) and an object projection iswith the eye as center. Light aberrations angle equals to: t = arc tan (v/c) where v= relative velocity of the moving object and c is light velocity. The light coming from adistant object is seen along the line of sight and that meant we do not measure actualdistance of an object r0(pink line)but we measure its image or vertical projectionwhich is r0cosine t (blue line) and we escape measuring the horizontal projectionr0sine t which is perpendicular to the line of sight (black line).

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    In Short, light coming from objects at distance r0 will be seen at r0cosine tUsing real time mathematics to explain what we can see and/or detect or/andmeasure is what the Arabs have/had said and that would mean that if we try to

    measure a distance r0 we would not find r0 but we would find: Arabs real timedistance is seen in real time along the line of sight.

    Or, r = r0cosine t + r0cosine t = r0 e (r) t Eq - 1Or r = real (blue = along line of sight) + imaginary (black = perpendicular to line of si

    Or, r = r0 e (r) t. The absolute value of r = the absolute value ofr0

    This statement said that light coming from objects when measured it is measured along linsight and that meant we see light projections of objects (blue line) of objects positioned at

    positions r0 (pink). We do not see objects at r0 butseeimagesof objects light projectioandimages of objects light projection along the line of sight is r0cosine t and images oobject light projections perpendicular along the line of sight is r0 sine t (blue line).

    The Arabs said that we do not see or measure light reflected from objects but wemeasure light speed projections as constant or light speed projections ismeasured as constant.

    cc

    c

    The Arabs claim that we do not see objects position r0 but we see their visual position r.

    What humans see is r0measured along the line of sight and miss r0 perpendicular to theline of sight.In other wordsan object at a distance r0 humans are not aware that they do

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    not see r0 but they see a visual ofr0 which is r = r0 e (r) t and projection ofr0 alongthe line of sight that humans eye see and instruments measure is r0cosine t and theprojection ofr0perpendicular to the line of sight is r0cosine t. The Arabs added thatwhen accounted for, the difference between an object image or visual position r(quantummechanics) and object location or position r0(classical mechanics) is equal to a time delayeffect (relativistic mechanics)

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    Modern physics is based on 3 different mechanics classical quantum andrelativistic mechanics and their combination known as strings

    Arabs said that there is one and only one mechanics

    Quantum = classical + relativistic

    Arabs real time dependent mechanics (quantum mechanics): r = r0 e (r) t

    Arabs real time independent mechanics (classicalmechanics) is r = r0;t = 0The difference between r = r0 e (r) t; and r = r0Or, r0 e (r) t - r0= Arabs real time mechanics visual effects (relativistic mechanics)

    Or r = r = visual distance and r0 = actual distanceOr, r = r0 + (r - r0)

    Or visual distance = actual distance + (visual distance actual distance)Dividing by r0And r/r0 = r0/r0 +(r r0)/r0And r/r0 = 1+ (r r0)/r0What are wrong in all of modern physics are all wrong physics measurementsWhat this law said is:If the car width is r0 moves away the visual of the car width is r. The quantity r/r0 is the

    percentage that humans eye see and instruments measure and it is equal to 1 and thepercentage difference between the car width and what the human eye see of the carwidth or a time delay effect or a visual distance effect of(r r0)/r0If someone attempts to measure a quantity 0; then multiply by 0And (r /r0) 0= 0 + [(r - r0)/r0] 0What this formula said everything about modern astronomy is all wrongWhat is wrong with all of astronomy? If we to measure the angular velocity ofmoving planets around a star ,or, a star moving around another star in the skie0, then we do not measure actual 0 but we measure 0 + [(r - r0)/r0] 0Or we have antidote to western space time stupidity [(r - r0)/r0] 0

    This is the basis of correct measurements. The entire western civilization 500years of physics and the world 500,000 modern western civilization educated

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    physicists made/make this mistake and globalize their stupidity and to correctthis mistake is to delete western civilization physicists without loss of subject.There is nothing in modern physics that can be considered as correctbecause modern physics is based on wrong measurements. Modern physics iswrong time physics that can be deleted without loss of subject. Arabs real

    time physics is the past present and future of all of physics and it is the subjectof this book.Page 11

    Arabs real time astronomy: The Arabs Astronomers and Physicists said that:We can not see or/and detect or/and measure something in space that did notexist; we can not see or/and detect or/and measure something that had nothappened. We can only see or/and detect or/and measure things and events inspace that had happened. What we see or/and detect or/and measure is notnecessarily what there is and not necessarily what happened. We see or/and detector/and measure traces and images of objects of past event. We see or/and detector/and measure in present time of images of object and events that happened inpast time. That is we measure images and record data of objects of past events inpresent time. An event changes in time and when an event is measured it ismeasured after it happened.

    Present time = present timePresent time = past time + (present time past time)

    Present time = past time + time difference

    Present time = real time; past time = event time; (present time past time) =time delay, or, Real time = event time + time delay

    Real time Astronomy = Event time Astronomy + time delays Astronomy

    In Modern Physics language the Arabs would have saidQuantum = classical + relativisticWhat there is = classical

    What we see and measure and detect and partially record is = quantumWhat we see and measure and has no detection because it is an Illusion =relativisticTime dependent measurements = time independent measurements +(Time dependent measurements time independent measurements)Measured = actual + (measured actual)We do not see object in real time but we see images of objects in real timeIn common Terms: Image = object + (image object)With Image = I; object = OI = O + (I O)I/O = O/O + (I O)/O

    I/O = 1 + (I O)/OArabs real time measurements equation:

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    Is: (I/O) q = q + [(I O)/O] q; q measured quantity ------------- Eq 1That is a quantity q when measured in real time it would appear as q + [(I O)/O] q500 years of modern physics and 500,000 of modern physicists is all wrong because of principle (I/O) q = q + [(I O)/O] ----------------------- Eq - 1Or quantum = classical + relativisticIf Eq 1 is applied it would expose modern physics as stupidity itself and it wouldexpose modern astronomy as astrology itself. The thing about this principle given byEq 1: (I/O) q = q + [(I O)/O] q is that it is flawless physics law or truth itself

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    There are objects at location r0 (actual or classical distance) and when measured inreal time they appear as at a location r (quantum distance) = r 0 e (r) t

    That is the distance in the Universe is a classical distance but when a distance measured in

    real time it appears as quantum distance and the difference between classical distance quantum distance is relativistic distance

    Quantum (real time distance) = classical (event distance) + [Quantum classical]Quantum distance = classical distance + relativistic distanceRelativistic distance = quantum distance classical distance

    We see detect and measure quantum distance r = r0 e (r) tof an actual orclassical distance r0 and the difference betweenquantum distance r = r0 e t

    and actual or classical distance r0 is relativistic distanceTake r = r0 e (r) t

    Quantum (real time) = classical (event time) + [Quantum classical]

    Quantum time = classical time + relativistic time

    Relativistic time = quantum time classical time

    We see detect and measure Arabs real time physics

    Or, t = t0 e (t) tof an actual or classical time t0 ------------------ Eq - 3

    And the difference betweenArabs t = t0 e (t) t and actual or classical time t0 isrelativistic time

    Quantum = classical + [Quantum classical]Quantum = classical + relativistic timeRelativistic = quantum classical

    All there is in the Universe is objects of mass m moving in space (x, y, z) at a locationr = r (x, y, z). The state of any object in the Universe can be expressed as the product

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    S = m r; State = mass x location is all of astronomy needed Equation -1That is if mass of objects in space is known and if the location of object in space isknow then the state S = m r = mass x location of any object in space can beknown and that is all needed to be known to describe space motion of any objectand that is what is called astronomy

    That is mass m location r and time t = Astronomy and from this we can conclude:

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    Quantum (mass) = classical (mass) + [Quantum classical]Quantum mass = classical mass + relativistic massRelativistic mass = quantum mass classical mass

    We see detect and Arabs real time mass m = m0 e (m) t------------- Eq- 4 of

    an actual or classical time m0 and the difference betweenArabs real time mass m= m0 e (m) t and actual or classical time m0 is Arabs real time mass delaySuch a claim by the Arabs that Astronomical measurements are made along the lineIs saying Quantum mass = classical mass + relativistic mass

    And saying (I/O) q = q + [(I O)/O] q; q measured quantity Eq - 1

    And real time distance r = r0 e (r) t Eq - 2And real time t = t0 e (t) t Eq - 3And real time mass m = m0 e (m) t Eq - 4And S = m r, the state equation Eq - 5That is Arabs see detect and measure quantum distance quantity r = r0 e (r) t

    When there is classical distance quantity r0And the difference explains that the universe is seen in real time and not in silly Westerideas of wrong space time. That is the difference between an object location and an objmeasurement of its location is relativistic and that 500 years of western Modernphysics can be deleted without loss of subject and 500,000 Modern physicists can be idiots with no fear or regrets.

    That is Arabs detect and measure quantum time quantity t = t0 e (t) t

    When there is classical time quantity t0That is Arabs see detect and measure quantum mass quantity m = m0 e (m) t

    When there is classical mass quantity m0What is wrong in all of Modern physics is this experimental mistake:[(I O)/O] q in everything that western modern space timers do from spacescience to nuclear structure and this mistake was made by every physicist. Thispainful mistake is the one mistake when corrected it deletes western civilizationphysics and physicists explain the universe correctly and matches experimentalresults with unprecedented accuracy to delete modern physics of past 500 yearsand delete 500,000 modern physicists without loss of subject. What I am going todo

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    1- Show how this one mistake was/is made daily by all western civilizationeducated modern physicists2- How this one mistake won the majority of Nobel prizes and changed physics from1258 Arabic science to 2010 western educated stupidity3 Show how correcting this mistake will solve any and all unsolved physical motion

    problems that is not solvable by space time physics or any read or publishedphysicsArabs real time physics and astronomy is the past present and future of all ofhysics

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    hapter four

    Car size at distance 4

    Car size at distance 3

    Car size at distance 2

    Car size at distance 1

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    Observer line: Observer

    Humans do not see detect or measure cars but humans see detect and measures imageof the car. In other words humans see detect and measure images of objects in realtime.

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    The size of the car object is the same but the size of the car image is dependent on cardistance and transmitted signal. Meaning we see detect and measure an image of size Iin real time (present time) of an object O seen detected and measured in event (pasttime). That is when images of cars are seen these images of the cars are seen in realtime. And when these car objects move the car see itself the same size. That is wemeasure images of object in real time and not objects. The difference between imagesand objects are visual illusions Arabs knew about and described in 10th century Ad.Conclusion:Is that humans see detect and measure images of objects in real time

    Why all Modern Physics and modern astronomy is all wrongWith Image = I; object = OI = O + (I O)I/O = O/O + (I O)/OI/O = 1 + (I O)/OAnd (I/O) q = q + [(I O)/O] q; q measured quantity --------------------- Eq - 1

    Modern physics is all wrong because Modern physics is wrong time physics based onwrong physics measurements that misses by a factor of [(I O)/O] q and thisquantity [(I O)/O] q is taken as real experimental result and not as a relativisticillusion correction. In other words:Correct Physics is: (I/O) q = q + [(I O)/O] q

    Modern Physics is wrong because(I/O) q = q + [(I O)/O] q

    What we measure = what there is + visual effectsQuantum = classical + relativisticQuantum = we see in real time = observer dependent = time dependent measurementClassical = object independent of observer = time independent measurementsRelativity = illusionsIn mathematical terms:Relativity = time dependent measurements time independent measurementsReal time scale

    Real time = event time + (real time event time)Real time = event time + time delay; time delay = (real time event time)With real time = ; event time = t; time delay = ( t)

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    = t + ( t) = t + ; = ( t)/t = t/t + ( t)/t/t = 1 + ( t)/t

    To measure orbital speed using time, then multiply by orbital speed toget the following equation: (/t) 0= 0 + [( t)/t] 0

    And 0 = orbital speedThe quantity 0 measurement is independent of timeThe quantity (/t) 0 measurement is time dependentThe difference = [( t)/t] 0= relativistic = Illusions

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    With (/t) 0= 0 + [( t)/t] 0

    Modern physics is wrong when: In general1 - (/t) 0= 0 Quantum = classical or when someone looks at the car fromdifferent distances and wonder why he/she does not see the same size car.

    An observer sees a car passing by at close distance

    An observer sees a car passing by at far distance

    Each observer will find the car size different

    2 Modern physics is wrong when (/t) 0= [( t)/t] 0

    When quantum = relativistic

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    3 Modern physics is wrong when 0= [( t)/t] 0

    When classical = relativistic

    Let us demonstrate the power of Arabs real time Physics and astronomy and seehow Arabs real time astronomy works but first let us do some definitions.

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    Real time distance scaleMeasured distance = actual distance + [measured distance actual distance]Or, r = r0 + (r x r0)

    And r/r0 = r0/r0 +(r r0)/r0And r/r0 = 1+(r r0)/r0And (r /r0) 0= 0 [(r - r0)/r0] 0

    Real time Velocity Scale vWith r = r0 + (r r0)Divide by tThen r/t = r0/t+ (r/t r0/t)And v = v0 + (v v0); dividing by v0And v/ v0 = 1+ (v v0)/ v0

    Multiplying by 0And (v/ v0) 0= 0+ [(v v0)/ v0] 0

    Real time acceleration scale With r = r0 + (r r0)Divide by tThen r/ t = r0/ t + (r/ t r0/ t)And = 0 + [( 0)]; dividing by v0And / 0 = 1+ [( 0)/ 0]Multiplying by 0And ( / 0) 0= 0+ [( 0)/ 0] 0The angular speed is a 5th grade math that is measured wrong by Astronomers exposethe stupidity of modern physics and the stupidity of modern astronomyThe circumference of a planet circular motion is C = 2 r m where r m is the radius.In 1969 I knew about circular speed v m = 2 r m/ T m where Tm is the period ofrotation. Also, in 1969 I knew about angular speed m = 2 /Tm = (v m/ r m).Or C = 2 r m; v m = 2 r m/Tm; m = 2 /Tm = (v m/ r m)

    m = 2 /Tm= (v m/r m)

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    Angular velocity is m = 2 /Tm= (v m/r m)In arc second per century m = (v m/r m) (180/ ) [36526/Tm (days)] (3600)

    Arabs Real time Astronomy distance scale:Is: (r m/r0) m= m [(r m - r0)/r0] mMultiplying by mThen (r m/r0) m= m + [(r m - r0)/r0] mIn arc second per century m = (v m/r m) (180/ ) [36526/Tm (days)] (3600)The distance Error is: [(r m - r0)/r0] mThe velocity Error is: [(v m - v0)/v0] mThe acceleration error is: [(m 0)/ 0] mThe angular velocity real time distance scale Error:

    Is: [(r m - r0)/r0] m = [(r m - r0)/r0] (v m/r m) (180/ ) [36526/Tm (days)] (3600)The angular velocity real time velocity scale Error:Is: [(v m - v0)/v0] m = [(v m - v0)/v0] (v m /r m) (180/ ) [36526/T m (days)] (3600)The angular velocity real time acceleration scale Error:

    Is: [( m 0)/ 0] m = [( m 0)/ 0] 0 (v m /r m) (180/ ) [36526/T m (days)] (3600As an example: when Astronomers look at planetary motion around the sun andthey saw the angular velocity in arc second per century:Equal to m = (v m /r m) (180/ ) [36526/T m (days)] (3600)

    = 70.75 arc second per centuryAstronomers also saw the visual effect

    Of: [(r m - r0)/r0] m = [(r m - r0)/r0] (v m /r m) (180/ ) [36526/T m (days)] (3600)And it is equal to [(r m - r0)/r0] m = 43Where r m = Mercury Sun distance = 58.2 X 106kmAnd v m = Mercury around the sun orbital speed Sun distance = 47.9 km/secAnd r 0= r e = Earth Sun distance = 149.6 X 106kmAnd T m = Mercury around the sun orbital period

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    This quantity of:[(r m - r0)/r0] m = [(r m - r0)/r0] (v m /r m) (180/ ) [36526/T m (days)] (3600)And it is equal to [(r - r0)/r0] m = 43 is taken as the proof of the existence ofsilly Modern Astronomy notion that the Universe is not made of three dimensional

    Space (x, y, z) = (length, width, height) but made of a more complex space toimaginary time back to space Universe (x, y, z, it) = (length, width, height,imaginary time)

    [(v m v e)/v e] 0 = [(v m v e)/v e] (v m /r m) (180/ ) [36526/T m (days)] (3600)And it is equal to [(r - r0)/r0] m = 43[( m e)/ e] m = [( m e)/ e](v m /r m) (180/ ) [36526/T m (days)] (3600)[( 0)/ 0] m= 43

    Space time is Einsteins crime against physics

    Planet Distance rX 106km

    PlanetOrbit T

    Orbitspeed vinkm/sec

    LessEarthspeed

    Spinspeedkm/sec

    Angular velocity;v/rarc sec/ century

    Mercury 58.2 88 47.9 18.1 .002 70.75Venus 108.2 224.7 35.05 5.7 6.52 10.86Earth 149.6 365.26 29.8 .46511 4.1Mars 227.936 687 24.14 0.2411Jupiter 778.412 4333 13.06 12.6Saturn 1,426.725 10760 9.65 9.87Uranus 2,870.97 30690 6.80 2.59Neptune 4,498 60180 5.43 2.68Pluto 5906.4 90730 4.74

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    I am the Greatest Nuclear Physicist of all timeAnd I have 1001 all new physics formulas to prove it

    My name is Joe Nahhas and I am the greatest Physicist and Astronomer of past

    present and the future because as a teenager I stood up to criminals with Nobelprizes and this book is how to expose criminals with Nobel prizes in physics and thefact that most criminals with Nobel prizes are a product of the big westerninstitutions has nothing to do with science but has something to do with westerncapitalistic greed fraud and arrogance that changed physics from science tostupidity and the time has come to delete stupidity and that is to delete westernphysics and physicists without exception since the rise of western civilization 500years ago starting with Copernicus. There is nothing correct in all westerncivilization physics that is taught in classrooms and used in scientific calculations.Yes, I am saying that all of physics is all wrong and this book is the proof of it and

    there is nothing better than to start with the grand master of stupidity, German American moron of the 20th century, the one and only Albert Einstein.

    Page 20

    Einstein greatest achievement in space saidPlanet Mercury travel in space at an angular speed of 70.75 arcs second per centuryAnd in time at angular speed of 43 arcs second per century

    The Advance of Planet Mercurys Perihelion given by Euclids Geometry[2 /T] [180/][36526/88][3600] = [2 /88 x 24x3600] [180/][36526/88][3600] = 70.75Einsteins time travel space time formula: = - 6 GM/a c (1 - ) [180/ ] [36526/T][3600] = 43 angular velocity time travel ofplanet MercuryG = 6.673 x 10-11= gravitational acceleration constantM =2x1030 kilogram = mass of the SunEccentricity of Mercurys orbit = = 0.206T= 88 days = period of Planet mercurys rotation around the SunAnd c = 299792.458 kilometer/second =light speed in kilometers/second

    And a = 58.2 x 106 km/sec = semi major axis of planet Mercury orbit

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    The grand moron of the west said Planets travel in space and time

    The Grand moron said planets travel in space around the Sun in an elliptical orbit

    The Grand moron said planets travel in time around the Sun rotating the elliptical orbit

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    Planet

    r

    Sun

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    This is space travelAnd the motion of a planet m around the Sun M measured as a rotating ellipse

    This is time travelPage 22

    r

    Sun

    Mercury

    M

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    Unless this moron can prove time travel he can keep his German stupidity to himself and Alfred NobelInstitution because time travel is Einsteins and Alfred Nobel Institution stupidity

    I am not saying Einstein is a moron but what I am saying is all western physicistsare morns to say the least and can be deleted without loss of subject to be exact.Practicing againIf 1= 1

    2 = 23 = 3

    Then we can write anything that is equal to itself as equal to itself like:Visual = Visual

    Actual = actual- Actual = - actual

    ----------------------- AddVisual = Actual + (Visual actual)

    Divide by actualVisual/actual = Actual/actual + (Visual actual)/actual

    OrVisual/actual = 1 + (Visual actual)/actualImage/object = 1 + (Image object)/object

    I/O = 1+ (I O)/OWe do not see object O but we see Image I. If we to look at planet Mercury from

    Earth and not from the Sun, then we are not looking at m= 2 /T m = (v m /r0) butwe are looking:At 0 I/O = 1 0+ [(I O)/O] 0Or 0 I/O = 0+ [(I O)/O] 0The visual illusion and Modern Physicists confusion is: [(I O)/O] 0Where I is Mercury Sun distance = 58,200,000 kilometers = r mAnd O is Earth Sun distance = 149,600,000 kilometers = r eThe Visual Illusions and modern Physicists confusion of Planet Mercury is:[(I O)/O] 0 = [(r m r e)/ r e] 0

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    Multiplying by (t/t) = 1

    [(I O)/O] 0 = [(r m/t r e/t)/ r e/t] 0Then [(I O)/O] 0 = [(v m v e)/ v e] 0[(I O)/O] 0 = [(r m r e)/ r e] 0 = [(r m r e)/ r e](v0/r0)

    [(I O)/O] 0 = [(v m v e)/ v e] 0 = [(v m v e)/ v e](v0/r0)With v0 = v m; and r0 = r mWith r m = 58.2 x 109 m; r e = 149.6 x 109 m; v m = 47.9 km/s; T m = 88 days

    With (v m/r m) [(180/) (3600) (26526/T m) = 70.75 arc second per century

    Copernicus Distance Illusion

    [(I O)/O] 0 = [(r m r e)/ r e](v m/r m) [(180/) (3600) (26526/T m)] = 43= [(58.2 x 109 - 149.6 x 109)/ 149.6 x 109] (70.75)= [(58.2 - 149.6)/ 149.6] (70.75) = 43 arc second per centuryNicklaus CopernicusDistance Illusion

    [(I O)/O] 0 = [(r m r e)/ r e](v m/r m) [(180/) (3600) (26526/T m)] = 43

    M r Copernicus you are wrong and you are deleted

    With [(I O)/O] 0 = [(r m r e)/ r e](v m/r m) [(180/) (3600) (26526/T m)]

    Next

    Is Galileo

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    With r m = v m T m; r e = v e T e

    Or Galileoslinear motion visual Illusion

    [(I O)/O] 0 = [(v m T m v e T e)/ v e T e](v m/r m) [(180/) (3600) (26526/T m)] = 43

    [(I O)/O] 0= [(47.9x88 365.26x29.8)/ 365.26x29.8] (70.75) = 43

    M r Galileo you are wrong and you are deleted

    With[(I O)/O] 0 = [(v m T m v e T e)/ v e T e](v m/r m) [(180/) (3600) (26526/T m)] = 43

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    Tyco Brahe Velocity Illusion: [(r m r e)/ r e]=[(r m /t) (r e/ t)]/ (r e/t) = (v m v e)/ v e

    [(I O)/O] 0 = [(v m v e)/ v e](v m/r m) [(180/) (3600) (26526/T m)] = 43

    [(I O)/O] 0 = [(47.9 29.8)/ 29.8](70.75) = 43

    M r Tyco Brahe you are wrong and you are deletedWith

    [(I O)/O] 0 = [(v m v e)/ v e](v m/r m) [(180/) (3600) (26526/T m)] = 43

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    (I/O) q = q + [(I O)/O] q

    M r Lippershey you can even read the telescope and you are deleted

    Hans Lippershey the person who attempted to get a patent for the telescope in 1609

    Modern Physics is wrong because Hans and the entire Western civilization s

    have no clue how to read the telescope(I/O) q = q + [(I O)/O] q

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    Rene Descartes Cartesian failures

    t = t0 e (t) t

    = te (t) t

    Along the line of sight

    x = t cosine t x = t + ( x t) = t + x; x = ( x t) x /t = t/t + ( x t)/t x /t = 1 + ( x t)/t

    What is [( x t)/t]

    Then x (seconds) = x - t = - 2 t sine {[arc tan (V r m - V r e)/ ( 2c)]/ 2} = 43And in arc x (arc seconds) = x - t= - 30 t sine {[arc tan (V r m - V r e)/ ( 2c)]/ 2} = 43

    Where r = V r; and r = V ; and V r = 2 rr; and V = r

    The confusion is and was r= ; V r = 2 V ; and taking V r = ( 2) V

    And taking V r = V r (Mercury) - V r(Earth) = V r m - V r eAnd V = V r/( 2 x Arc second) = x - t

    = - 30 t sine {[arc tan (V r m - V r e)/ ( 2c)]/ 2} = 43 arc second /century

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    Chapter 3: Arabs real time light motion

    Car size at distance 4

    Car size at distance 3

    Car size at distance 2

    Car size at distance 1

    Observer line: Observer

    Visual objects seen through emitted or reflected light follow this lawLight measurement of visual motion of objects law: (I/O) q = q + [(I O)/O] q

    The proof:Page 29

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    All there is in the Universe is objects of mass m moving in space (x, y, z) at alocationr = r (x, y, z). The state of any object in the Universe can be expressed as theproductS = m r; State = mass x location:

    P = d S/d t = m (d r/d t) + (dm/d t) r = Total moment= change of location + change of mass= m v + m' r; v = velocity = d r/d t; m' = mass change rate

    F = d P/d t = dS/dt = Total force= m (dr/dt) +2(dm/d t) (d r/d t) + (dm/dt) r= m + 2m'v +m" r; = acceleration; m'' = mass acceleration rate

    In polar coordinates system

    r = r r (1) ;v = r' r(1) + r ' (1) ; = (r" - r')r(1) + (2r'' + r ")(1)r = location; v = velocity; = accelerationF = m + 2m'v +m" rF = m [(r"-r') r (1) + (2r'' + r ") (1)]+2m'[r' r (1) + r ' (1)] + (m" r) r(1)

    = [d (m r)/dt - (m r) '] r (1) + (1/m r) [d (mr')/d t] (1)= [-Gm M/r] r (1) ------------------------------- Newton's Gravitational Law

    Proof:First r = r [cosine + sine ] = r r (1)Define r (1) = cosine + sine Define v = d r/d t = r' r (1) + r d[r (1)]/d t = r' r (1) + r'[- sine + cosine ]

    = r' r (1) + r ' (1)

    Define (1) = -sine +cosine ;And with r (1) = cosine + sine Then d [ (1)]/d t= ' [- cosine - sine = - ' r (1)And d [r (1)]/d t = ' [-sine + cosine ] = ' (1)

    Define = d [r' r (1) + r ' (1)] /d t= r" r (1) + r'd [r (1)]/d t + r' ' r (1) + r " r (1) +r 'd [ (1)]/d t

    = (r" - r') r (1) + (2r'' + r ") (1)

    With d (m r)/dt - (m r) ' = F (r)And d (mr')/d t = 0With m = constant, thenWith d r/dt - r ' = F (r) Eq-1And d (r')/d t = 0 Eq-2With d r/dt - r ' = 0 E q 1And d (r')/d t = 0 Eq-2

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    From Eq-2: d (r')/d t = 0Then r' = h = constantDifferentiate with respect to timeThen 2rr'' + r" = 0

    Divide by r'Then 2(r'/r) + "/' = 0And 2(r'/r) = - "/' = 2[ (r) + (r)]Also, r = r0 (, 0) e [ (r) + (r)] t

    And ' = ' 0 (, 0) e -2[ (r) + (r)] tFor a fixed orbit: r = 0Also, r = r 0 (, 0)e t

    And ' = ' 0 (, 0) e -2 tWith d r/dt - r ' = 0

    Let u = 1/r; r = 1/u; r' = h = /uAnd d r/d t = (d r/ d u) (d u /d ) (d / d t) = (- 1/u ) () (d u/ d )

    = - h (d u/ d )

    And d r/ d t = - h () (d u/ d )= [- h/r] (d u/ d )= - h u (d u/ d )

    With d r/dt - r ' = 0 E q 1And - h u (d u/ d ) (1/u) (h u) = 0Then (d u/ d ) + u = 0

    Then u = A e - Then r 0 (, 0) = (1/A) e And r 0 (, 0) = r 0 (0, 0) e And r = r 0 (0, 0) e e tOr, r = r 0 e (+ t)

    This is quantum mechanics

    rabs real time astronomy is actually quantum mechanics r = r0 e (r) t

    Light is emitted and not an emitter and humans have no means of measuring lightin motion and at best they can take a snap shot.In mathematical languageThen r (, 0) = r 0 e at t = 0And r (, t) = r 0 e (+ t)= r 0 e e t= r (, 0) e tAnd r (, t) = r (, 0)[cosine t + sine t]And r x (, t) = r x (, 0)cosine tAnd t = cosine-1 [r x (, t) / r x (, 0)]

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    Then r = r x (, t) - r x (, 0)= r x (, 0)[(cosine t) 1]

    And [r x (, t) - r x (, 0)]/ r x (, 0)

    = [(1 - 2 sine t/2) 1]= - 2 sine t/2; t = cosine-1 [r x (, t) / r x (, 0)]

    Arabs real time astronomy:Image = Image = IObject = Object = O- Object = - Object = - O

    Image = object + (Image Object)I = O + (I O)(I/O) = O/O + [(I O)/O](I/O) = 1 + [(I O)/O](I/O) ' 0 = ' 0 + [(I O)/O] ' 0

    Quantum = classical + relativistic IllusionI = r; O = r 0

    Or, (r / r 0) ' 0 = ' 0 + [(r r 0)/ r 0] ' 0And [(r r 0)/ r 0] ' 0Or [- 2sine t/2] ' 0; t = cosine-1 [r x (, t) / r x (, 0)] = cosine-1 (r/ r 0)For planet Mercury:

    The distance visual effect Error is: [(r m re)/re] m

    The quantity: m = (v m/r m) (180/ ) [36526/Tm (days)] (3600) = 70.75

    With v m = 47.9 km/sec; r m = 58.2 x 106 km; Tm = 88 days

    With r = 58.2 x 109 m = Sun Mercury distance

    And r e =149.6 x 109 m = Sun Earth distance

    With [(r m re)/re] = [- 2sine t/2] = 0.61And t = cosine-1 [r x (, t) / r x (, 0)] = cosine-1 (r/ r 0)Or t = cosine-1 [r x (, t) / r x (, 0)] = cosine-1 (r m/ r e)

    And [(r m re)/re] m= [- 2sine t/2] (v m/r m) (180/ ) [36526/Tm (days)] (3600)= [- 2sine {[cosine-1 (r m/ r e)]/2}] (v m/r m) (180/ ) [36526/Tm (days)] (3600)= 0.61 x 70.75 = 43

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    Chapter five: Arabs real time light Astronomy

    A- Keplers force laws

    F = - a and F = - GmM/aOr, F = - a = - GmM/aAnd T/a = 4 GM

    Mr Kepler you are wrong and you are deleted

    Johannes Keplers:

    Keplers law: a/T = k = constantIsaac Newton space Inverse square law = k/r

    Hookes time Inverse square law = r/t or = r/TKeplers Space time Law: k/r = r/ T; or, a/T = k = constantWhere this law came from?Acceleration = = r/t = k/r = time coordinates r/t = space coordinates k/r; r substituted for t

    = r/t = k/r = - k/r Newtons theft = Newton = - r/t = - r/T = - k r Hookes theft = Hooke lawOf: a/T = k = constantOr, a1/ T1 = a2/ T2Or, a1/ a2 = (T1/ T2)2/3

    And (a1 - a2)/ a2 = (T1/ T2)2/3 1Or (am a e)/ a e = (Tm/ Te) 2/3 1Nicklaus CopernicusDistance Illusion[(I O)/O] 0 = [(r m r e)/ r e](v m/r m) [(180/) (3600) (26526/T m)] = 43Become: Keplers vision of idiot Einstein: Nicklaus CopernicusDistance Illusion[(I O)/O] 0 = [(Tm/ Te) 2/3 1] (v m/r m) [(180/) (3600) (26526/T m)] = 43

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    When Newton came with F = - GmM/rPhysicists calculated: ' c m = v c m/r;Angular velocity with respect to center of mass

    And Astronomers observed: 's = v s/rAngular velocity with to the sun

    And v c m = [GM/ (m + M) a]

    And v s = (GM/a)

    And (' cm - s) /s = [(2 /T c m) - (2 /T s)]/ (2 /T s)= (T c m/T s) 1 = (v s/v c m) 1

    = [ (GM/a)] x { [(m + M) a/ GM]} - 1= [(m + M)/M] - 1= [1 + (m/M)] - 1 1 + (m/2 M) 1 m/2 M

    And (' cm - s) /s (m/2 M)And (' cm - s) / ' s = (2 /T s) (m/2 M)And [(' cm - s)] T s = (m/ M)Multiplying by [(180/) (3600) (26526/T m)]

    [(I O)/O] 0 = ( m/M) [(180/) (3600) (26526/T m)] = 43T/a = 4 /GM with respect to the sunTo T/a = 4 /G (M + m) with respect to the center of massThat is Kepler's measurements data are centered from the sun and Newton's dataare centered at the center of mass and this would explain this mistake like this:T (1)/a = 4 /GM andT (2) /a = 4 /G (M + m)When Newton changed Kepler's equation he solved the advance of perihelion asshown:

    The advance of Mercury perihelion by Newton

    T (1) = T (2) [M/ (M + m)]And 2/ T (1) = [2 / T (2)] (1 + m/M)And ' (1) = ' (2) (1 + m/M)And ' (2) = ' (1) / [1 + (m/M)] [1 - m/ (2M)]This approximation was not on the original workAnd ' (2) - ' (1) = ' (1) [1 / [1 + (m/M)] - 1]And ' (2) - ' (1) - ' (1) (m/2M) = - [2 /T] [m/2M) = - m/MT radians/T

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    W " (calculated) = [- m/MT] (180/ degrees) (3600 seconds) (36526 century); T= days; with m = 0.32 x1024 kg; and M = 2.0 x1030 kg; T = 88 days

    [(I O)/O] 0 = (-180 x 36526 x 3600/T) ( m/M)

    = 43.0" seconds of arc /100 years

    Mr Newton you are wrong and you are deleted

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    Hookes for law F = - x; 3 Newtons law F = - GmM/xIf Hookes law is taken the F = - k r in one dimensionThen r +r = 0; then r (, 0) = r0 e t

    Then r = r0 e

    t

    ; and r = r0 [1- 2 sine t/2]And (r - r0)/ r0 = - 2 sine t/2The distance visual effect Error is: [(r m re)/re] m

    The quantity: m = (v m/r m) (180/ ) [36526/Tm (days)] (3600) = 70.75

    With v m = 47.9 km/sec; r m = 58.2 x 106 km; Tm = 88 days

    With r = 58.2 x 109 m = Sun Mercury distance

    And r e =149.6 x 109

    m = Sun Earth distanceWith [(r m re)/re] = [- 2sine t/2] = 0.61And t = cosine-1 [r x (, t) / r x (, 0)] = cosine-1 (r/ r 0)Or t = cosine-1 [r x (, t) / r x (, 0)] = cosine-1 (r m/ r e)

    And [(r m re)/re] m= [- 2sine t/2] (v m/r m) (180/ ) [36526/Tm (days)] (3600)= [- 2sine {[cosine-1 (r m/ r e)]/2}] (v m/r m) (180/ ) [36526/Tm (days)] (3600)= 0.61 x 70.75 = 43

    Mr Hooke I really like you but you can be deleted

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    Idiot Le Verrier[(I O)/O] 0 = [(r m r e)/ r e](v m/r m) [(180/) (3600) (26526/T m)] = 43[(I O)/O] 0 = [(v m T m v e T e)/ v e T e](v m/r m) [(180/) (3600) (26526/T m)]

    Arabs real time Astronomy is 5 lawsAnd saying (I/O) q = q + [(I O)/O] q; q measured quantity Eq - 1And real time distance r = r0 e (r) t Eq - 2And real time t = t0 e (t) t Eq - 3And real time mass m = m0 e (m) t Eq - 4And S = m r, the state equation Eq - 5

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    hapter six

    Newton equation is a solved wrong for 350 yearsNewtons unprecedented stupidity

    Being a good mathematician is solving own equation wrong?Newton said there is gravity Force F = -GmM/r whose solution is this

    Fig1. Newtons gravitational lawAnd r (, t) = [a (1-)/ (1+ cosine )]But you idiot this solution is wrong

    Real time solution is: r (, t) = [a (1-)/ (1+ cosine )] [ (r)+ (r)] t"Apparent advance of perihelion"[(I O)/O] 0 = (-720x36526x3600/T) {[ (1- )]/ (1-) } x

    [(v+ v*)/c] = 43 arc second per centuryPage 39

    Planet

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    All there is in the Universe is objects of mass m moving in space (x, y, z) at alocation r = r (x, y, z) = r [length, width, height].

    The state of any object in the Universe can be expressed as the product

    S = m r; State = mass x location:

    P = d S/d t = m (d r/d t) + (dm/d t) r = Total moment= change of location + change of mass= m v + m' r; v = velocity = d r/d t; m' = mass change rate

    F = d P/d t = dS/dt = Total force= m (dr/dt) +2(dm/d t) (d r/d t) + (dm/dt) r= m + 2m'v +m" r; = acceleration; m'' = mass acceleration rate

    In polar coordinates system

    Location = r = r r (1)

    Velocity = v = r' r (1) + r ' (1)

    Acceleration = = (r" - r') r (1) + (2r'' + r ") (1)

    F = m + 2m'v +m" r

    F = m [(r"-r') r (1) + (2r'' + r ") (1)]+

    2m'[r' r (1) + r ' (1)] ++ (m" r) r (1)

    F = [d (m r)/dt - (m r) '] r (1)+ (1/mr) [d (mr')/d t] (1)

    F = F1 + F2

    F1 = [d (m r)/dt - (m r) '] r (1)

    F2 = (1/m r) [d (mr')/d t] (1)Newton's Gravitational Equation is: F = -GmM/rWith d (m r)/dt - (m r) ' = -GmM/r (1)And d (mr')/d t = 0 (2)

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    The solution is notAnd r (, t) = [a (1-)/ (1+cos)]But this solution

    Real time solution is: r (, t) = [a (1-)/ (1+ cosine )] [ (r)+ (r)] t

    "Apparent advance of perihelion"[(I O)/O] 0 = (-720x36526x3600/T) {[ (1- )]/ (1-) } x

    [(v+ v*)/c] arc second per centuryProof:

    All there is in the Universe is objects of mass m moving in space (x, y, z) at a location rr (x, y, z) = r [length, width, height].e state of any object in the Universe can be expressed as the product

    S = m r; State = mass x location:P = d S/d t = m (d r/d t) + (dm/d t) r = Total moment

    = change of location + change of mass

    = m v + m' r; v = velocity = d r/d t; m' = mass change rateF = d P/d t = dS/dt = Total force= m (dr/dt) +2(dm/d t) (d r/d t) + (dm/dt) r= m + 2m'v +m" r; = acceleration; m'' = mass acceleration rate

    In polar coordinates systemLocation = r = r r (1)Velocity = v = r' r (1) + r ' (1)Acceleration = = (r" - r') r (1) + (2r'' + r ") (1)F = m + 2m'v +m" rF = m [(r"-r') r (1) + (2r'' + r ") (1)]+

    2m'[r' r (1) + r ' (1)] ++ (m" r) r (1)

    F = [d (m r)/dt - (m r) '] r (1)+ (1/mr) [d (mr')/d t] (1)

    F = F1 + F2F1 = [d (m r)/dt - (m r) '] r (1)F2 = (1/mr) [d (mr')/d t] (1)

    Newtons force law is F1 = [-GmM/r] r (1)Kepler's force law is:F2 = (1/mr) [d (mr)/d t] (1) = 0

    If m is constant then d (mr)/d t = 0; and d (r)/d t = 0Or, r = h = 2 a b/T; a = mean distance from sun and is called semi major axisand b is the semi minor axis.

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    the motion of a planet m around the Sun M measured in real time is a rotating ellipse

    Tyco Brahe Logged observational Data of Planets P motion around the Sun S andthen Kepler stated the areal velocity law: If Planet p observed from the sun then thetrajectory of planet p will cut equal areas in equal times.

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    r

    Sun

    Mercury

    M

    m

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    Page 43

    A

    AA

    A

    S

    A

    A

    A

    S

    T

    T

    TT

    TT

    T

    P

    P

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    When the areas size A are sliced equally it was found that the times spent by planetsorbiting around the Sun and making areas A each are equal also.Or, r (0) ' (0) = r (1) ' (1) = r (2) ' (2) = r (3) ' (3) = --

    = location x [angular speed] = constant= Areal velocity

    If r '= hThen differentiating with respect to timeThen d (r ')/ d t= d h/ d tAnd 2 r r + r = 0Or 2 (r /r) = - (/)

    The r = r0 e t

    And = 0 e 2 t

    With r = r0 e t

    In real time r (n) = r (0) e t

    With r (0) ' (0) = r (1) ' (1)Then ' (1) = [r (0)/ r (1)]' (0)

    And ' (1) = {[e 2 t] ' (0)And (1) = {[cosine 2 t + sine 2 t] 1}' (0) (1) = (x) + (y)

    = [cosine 2 t + sine 2 t] ' (0) (x) = [cosine 2 t] ' (0) (x) = [1 2 sine t] ' (0) (x) - ' (0) = - 2' (0) sine t W = (x) - ' (0) = - 2' (0) sine t

    = -2(2) [ (1-)]/T (1-) ] sine tAnd ' (0) = h/r (0) = 2 a b/T a = 2 (1-)]/T (1-) W = - 4 ) [ (1-)]/T (1-) ] sine tIf this apsidal motion is to be found as visual effects, thenWith, v = spin velocity; v* = orbital velocityAnd v/c = (v* + v)/c = tan t W = -4 [ (1-)]/T (1-) ] sine {Inverse tan [(v* + v)/c]} radiansMultiplication by 180/ to change to degrees W = (-720/T) {[ (1-)]/ (1-) } sine {Inverse tan [(v* + v)/c]} DegreesAnd multiplication by 1 century = 36526 days and using T in daysW (ob) = (-720x36526/Tdays) {[ (1-)]/ (1-) } x

    sine {Inverse tan [(v* + v)/c]} degrees/100 yearsApproximationsWith v

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    Finding orbital velocitiesFrom Newton's inverse square law of an ellipse motion applied to a circular orbitgives the following: m v/ r (cm) = GmM/rPlanet --- r (cm) ----- Center of mass ------- r (CM) --------- Mother SunPlanet ------------------- r -------------------------------------- Mother Sun

    Center of mass law m r (cm) = M r (CM); m = planet mass; M = sun massAnd r (cm) = distance of planet to the center of massAnd r (CM) = distance of sun to center of massAnd r (cm) + r (CM) = r = distance between sun and planetSolving to get: r (cm) = [M/ (m + M)] rAnd r (CM) = [m/ (m + M)] rThen v = [GM r (cm)/ r] = GM/ (m + M) rAnd v = [GM/ (m + M) r = a (1-/4)]Planet orbital velocity or primary velocity:And v* = v (m) = [GM/ (m + M) a (1-/4)] = 48.14 km for planet MercuryVelocity of secondary or Mother Sun velocityAnd v* (M) = [Gm / (m + M) a (1-/4)]Applications: mercury ellipse and its axis rotation of 43 " /century1- Planet Mercury axial "apparent" rotation rate

    W = (-720x36526x3600/T) {[ (1-]/ (1-) } (v* + v/c) seconds of arc pecentury

    The circumference of an ellipse: 2a (1 - /4 + 3/16()- --.) 2a (1-/4); R =a (1-/4)

    Where v* (p) = [G M / (m + M) a (1-/4)] [GM/a (1-/4)]; m

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    Chapter sevenInverse Cube equations F = m = - k/r r (1), then in polar coordinatesWith m [d r/dt - 'r] = - k /r Inverse Cube Gravitational law (1)And d (r')/d t = 0 Kepler's Areal Velocity Equation (2)

    These two equations give an axial rotation rate:One: = (m/ M) (180) [36526/T] [3600] arc second/100 years

    = 43.0344 seconds of arc / century for MercuryTwo: ' = - 720 [36526/T] (3600) (1 - )/ T (1 - ) (v/c) arc second/100years

    = 43.0" seconds of arc /century for MercurySolution:With m = constantThen d r/dt - 'r = - k/ r (1)And d (r')/d t = 0 (2)From (2) d (r')/d t = 0; r' = hFrom (1), ' d r/ d - 'r = - k/ mrAnd ' [d r/ d - r] = - k/ mrAnd d r/ d - r = - (k/mh) rAnd d r/ d - r [1 - (k/mh)] = 0And r (, 0) = r (0, 0) e { [1 - (k/mh)]} From (2) d (r')/d t = 0; r' = hThen 2rr'' + r'' = 0Dividing by r'

    We get 2 (r'/r) + (''/') = 0And 2 (r'/r) = - ''/' = 2 t

    And r = r (0, 0) e { [1 - (k/mh)]}e t

    And ' = ' (, 0) e- 2 tOr r = r (0, 0) e { [1 - (k/mh)]}+ t

    And ' = ' (0, 0) e-2 [{ [1 - (k/mh)]} + t]

    And ' = ' (0, 0) e-2 [{ [1 - (k/mh)]} + t]And ' = (' (0, 0) {cosine 2 [{ [1 - (k/mh)]} + t]

    - sine 2 [{ [1 - (k/mh)]} + t]}

    And ' - ' (0, 0) = - 2 ' (0, 0) sine [{ [1 - (k/mh)]} + t]And ' = - 2 ' (0, 0) sine [{ [1 - (k/mh)]} + t]If k = Gm M (1 - ); h = 2 a b/TThen: k/mh = Gm M a (1 - )/m 4 a b/TAnd k/mh = GM T (1 - )/4 a b; multiply by (a/a)Then [a (1 - )/ b] [GM T/4 a] = [GM T/4 a]

    Then ' = - 2 ' (0, 0)] sine [{ [1 - (GM T/4 a)]} + t]Taking Kepler's: GM T/4a = 1

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    Then ' = - 2 ' (0, 0) sine tAnd ' (0, 0) = h/r = 2ab/Ta (1 - )

    = 2a (1 - )/Ta (1 - ) = 2 (1 - )/T (1 - ) And ' = - 4 (1 - )/ T (1 - ) sine tWith T = arc tan v/c

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    Chapter eight: Nuclear gravityYukawas: O)/O] 0: M r Yukawa travel is not physics but Alfred Nobel physicists stupidity

    Nuclear Gravity F = (-GmM/r) ek/rWith d (m r)/dt (m r) ' = [-GmM/r] e k/ r Nuclear gravity Equation (1)And (mr')/d t = 0 Kepler's Areal Velocity (2)

    (2): d (mr')/d t = 0Then mr' = constant; if m is taken as constant then r' = h

    And (1): d r/dt - r ' = [-GmM/r] ek/r

    Let m r =1/uThen d r/d t = -u'/u

    = - (1/u) (') d u/d = (- '/u) d u/d = - h d u/d

    And d r/dt = -h'du/d= - hu [du/d]

    With d (m r)/dt - (m r) ' = [-GmM/r] ek/r Nuclear Gravity (1)

    With ek/r 1+ k/r; k/r

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    And [1 GMk/h] = (GM/h) a (1-)And h - GM k = G M a (1- )

    Then h/GM a (1- ) = k

    And [1 GMk/h] = {[1 (GM/h) [(h/GM) a (1 - )]}= {[1 1 + (GM/h) a (1 - )]}= [(GM/h) a (1 - )]= {[GMT/4a4 (1 - )] a (1 - )]}= (GMT/4a)= 1; T/ a = 4/ GM Keplers

    Then, r = 1/u = (GM/ h) + A cosine If, T/ a = 4/ G (M +m) NewtonsThen, [1 GMk/h] = (GMT/4a) = [M/ (M + m)]= 1/ [1 + (m/M)] 1/ [1 + (m/2M)] = 1 (m/ 2M)

    And [1 GMk/h]/ (M/ h)]/ {1 + cosine { [1 - GMk/h]} = a (1- )/ [1 + cosine { [1 (GMk/h)]} = a (1- )/ {[1 + cosine [(1 m/2M) ]}= a (1- )/ [1 + cosine ( )]And 2 = 2 (m/ 2M) = (m/M)If Newtons law were to be F = - Gm (M + m)/rThe 2 = 2 [m/ 2(M + m)] = [m/ (m + M)]

    Nuclear Gravity (-GmM/r) e (m / M r)

    Abstract: Yukawa Gravity (-GmM/r) e(m / M r)

    or the nuclear gravity force is thecrudely approximated Newtonian gravity force (-GmM/r) explains planetarymotion around the sun as a rotating ellipse with a rotation rate = [ m/(m + M)](180/)(36526/T)(3600) = 43.03 seconds of an arc per century for the most talkedabout planet of mercury; m = 3.2 x 1024 kg; M = 2x1030 kg; T = 88days

    With d (m r)/dt (m r) ' = (-GmM/r) e (m / M r) Gravity Force (1)And d (mr')/d t = 0 Kepler's Areal Velocity (2)

    Then mr' = constant; if m is taken as constant then r' = hAnd (1): d r/dt - r ' = -GmM/r + Gm/r

    Let m r =1/uThen d r/d t = -u'/u = - (1/u) (') d u/d = (- '/u) d u/d = - h d u/d And d r/dt = -h'du/d = - hu [du/d]-hu [du/d] - (1/u) (hu) = -G M u [1 ( m /M) u]; m /M r

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    = [1 Gm/h]/M/ h]/ {1 + cosine { [1 - Gm/h]}

    Where [1 Gm/h]/GM/h = a (1 )And [1 Gm/h] = (GM/h) a (1-)

    If = a (1 ), the h = G (m + M) a (1- )Then Gm/h = G ma (1 - ) /G (m + M) a (1- )= m/ (m + M)

    With r (, 0) = [1 Gm/h]/M/ h]/ {1 + cosine { [1 Gm/h]} Then r (, 0) = a (1 )/ {1 + cosine { [1 Gm/h]}

    And r (, 0) = a (1 )/ {1 + cosine { [1 m/ (m + M)]} And m

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    Chapter Ten: Space time unlimited stupidityVisual force: F = - Gm M/r - Gm Mk/r

    With m [d r/dt - 'r] = - Gm M/r - Gm Mk/r Visual Gravitational law (1)And d (r')/d t = 0 Kepler's Areal Velocity Equation (2)

    Gives an axial rotation rate ofW = 15 x (36526/T (days)] [(v* m - v*e)/v* e]

    Boundary value LawWith d (m r)/dt - (m r) ' = - k/ r Inverse square Gravitational (1)And d (mr')/d t = 0 Kepler's law (2)At Perihelion: d r/d t - r ' = - GM/r = - r '; d r/d t = 0Then r ' = GM/rA quick answer by Newton would be: First ' = [GM/r]And = [GM/r] [(v* m - v*e)/v* e]

    In arc sec / centuryThen = {[GM/r]} 1/2 [(v* m - v*e)/v* e] [(180/) (3600) (36526/Tm)

    = 43"/century[(I O)/O] 0= {[GM/r]} 1/2 [(v* m - v*e)/v* e] [(180/) (3600) (36526/Tm)

    Constant acceleration lawOr, r 1 /' 1= r 2 /'2 = constantOr, ' 2= {[r 2/ r 1]} ' 1And ' 2 - ' 1= {[ (r 2/ r 1)] - 1} ' 1 ' = {[ (r 2/ r 1)] - 1} ' 1This is the angular time delay and will be seen as angular visual IllusionThe angular speed is ' = v/rFor Mercury: ' = v/r = (47.9km/sec)/58,200,000 km = 0.000000843 radians/secIf you want the accumulation value in arc sec /century W", thenAnd W" = (v/r) (180/) (3600) (26526/T) = angular velocity in arc sec per century.If it is measured for planet Mercury thenW" = (47.9/58,200,000) (180/) (3600) (26526/88)

    W"= 70.75 arc second per centuryOr, W" = {[ (r 2/ r 1)] - 1} W" (1)What is the angular visual Illusion for planet Mercury that would be seen whenmeasured from Earth with Earth location r (1) = Earth = 149.6 x 106

    And r (2) = Mercury = 58.2 x 106

    And W" (2) = - 70.75 arc sec /century W" = {[ (r 2/ r 1)] - 1} W" 1 W" = {{ [149.6/58.2]} - 1} [-70.29] = 43.0" arc per century[(I O)/O] 0 = {{[r e/ r m]} - 1} (v m /r m)] [(180/) (3600) (26526/T)

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    Constant Areal velocity Law

    Or, r 1 '1= r 2 '2 = location x speed = constant = Areal velocity

    Or, r 1 v 1= r 2 v2

    Or, ' 1= (r 2/ r 1) ' 2

    And ' 1 - ' 2= [(r 2/ r 1) - 1] ' 2

    ' = ' 1 - ' 2= [(r 2/ r 1) - 1] ' 2

    ' = [(v 1/ v 2) - 1] ' 2

    This is the angular time delay and will be seen as angular visual IllusionThe angular speed is ' = v/rFor Mercury: ' = v/r = (47.9km/sec)/58,200,000 km = 0.000000843 radians/sec

    If you want the accumulation value in arc sec /century W", thenAnd W" = (v/r) (180/) (3600) (26526/T) = angular velocity in arc sec per century.

    If it is measured for planet Mercury thenW" = (47.9/58,200,000) (180/) (3600) (26526/88)W"= 70.29 arc second per century

    Or, W" = [(v 1/ v 2) - 1] W" (2)

    What is the angular visual Illusion for planet Mercury that would be seen whenmeasured from Earth with Earth location r (1) = Earth = 149.6 x 106

    And r (2) = Mercury = 58.2 x 106

    And W" (2) = - 70.29 arc sec /century

    W" = [(v 1/ v 2) - 1] W" (2)

    W" = [(v 1/ v 2) - 1] (v m /r m)] [(180/) (3600) (26526/T)

    W" = [(29.8/ 47.9) - 1] [-70.75] = 43.0" arc per century

    [(I O)/O] 0

    = [(v e/ v m) - 1] (v m /r m)] [(180/) (3600) (26526/T)

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    No Force solution

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    Newton said there is gravity Force F = -GmM/r whose solution is this

    Fig 1. Newtons gravitational law

    With m [d r/dt - 'r] = 0 Zero force lawequation (1)And d (r')/d t = 0 Kepler's Areal Velocity Equation (2)Equation (2) r = r0 e t; '= '0 e- 2 t

    Equation (1) - h d / d u - h u = 0Or d / d u + u = 0Then u = u0 e - And r0 = r0 (0) e + Or, r = r0 (0) e ( + t) [h/ '0] e ( + t)

    And '= '0 e- 2 t ' = - 2 '0 sine t

    = - 2[2/T] x [180/ ] [38526/T] [3600] sine t= - 2 [2/88 x 24 x 3600] x [180/ ] [38526/T] [3600] sine t

    = - 141.5 sine tAnd t = arc tan [(r m - r e)/ (r m + r e)] = arc tan [(149.6 58.2)/ (149.6 + 58.2)]

    ' = - 141.5 sine arc tan [(149.6 58.2)/ (149.6 + 58.2)] = 43 arc seconds per century

    Planet

    r

    Sun

    Planet Distance rX 106km

    PlanetOrbit T

    Orbitspeed vinkm/sec

    LessEarthspeed

    Spinspeedkm/sec

    Angular velocity;v/rarc sec/ century

    Mercury 58.2 88 47.9 18.1 .002 70.75

    Venus 108.2 224.7 35.05 5.7 6.52 10.86Earth 149.6 365.26 29.8 .46511 4.1Mars 227.936 687 24.14 0.2411Jupiter 778.412 4333 13.06 12.6Saturn 1,426.725 10760 9.65 9.87Uranus 2,870.97 30690 6.80 2.59Neptune 4,498 60180 5.43 2.68Pluto 5906.4 90730 4.74

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    Newtons mathematically wrong [(I O)/O] 0 =(-720x36526x3600/88) (1.552) (48.14/300,000) arc sec per century

    = 43This particular equation structure is the basis of stars studying. Originally, I derived

    it from Arabic real time physics literature.A visual Illusion along the line of sight is constructed as follows:Instead of seeing r0 we see r0 cosine arc tan (v/c) and perpendicular to the lineof sight we see r0 sine arc tan (v/c)Or r = r0 [cosine arc tan (v/c) + sine arc tan (v/c)]

    Or r = r0 e arc tan (v/c)

    Or r = r0 e tAnd areal velocity law gives the same resultsIf r '= hThen differentiating with respect to timeThen d (r ')/ d t= d h/ d tAnd 2 r r + r = 0Or 2 (r /r) = - (/)

    The r = r0 e t

    And = 0 e 2 t

    With r = r0 e t

    In real time r (n) = r (0) e tWith r (0) ' (0) = r (1) ' (1)Then ' (1) = [r (0)/ r (1)]' (0)

    And ' (1) = {[e 2 t] ' (0)And (1) = {[cosine 2 t + sine 2 t] 1}' (0) (1) = (x) + (y)

    = [cosine 2 t + sine 2 t] ' (0) (x) = [cosine 2 t] ' (0) (x) = [1 2 sine t] ' (0) (x) - ' (0) = - 2' (0) sine t W = (x) - ' (0) = - 2' (0) sine t

    = -2(2) [ (1-)]/T (1-) ] sine tAnd ' (0) = h/r (0) = 2 a b/T a = 2 (1-)]/T (1-)

    W = - 4 ) [ (1-)]/T (1-) ] sine tIf this apsidal motion is to be found as visual effects, then

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    With, v = spin velocity; v* = orbital velocityAnd v/c = (v* + v)/c = tan t W = -4 [ (1-)]/T (1-) ] sine {Inverse tan [(v* + v)/c]} radiansMultiplication by 180/ to change to degrees W = (-720/T) {[ (1-)]/ (1-) } sine {Inverse tan [(v* + v)/c]} Degrees

    And multiplication by 1 century = 36526 days and using T in daysW (ob) = (-720x36526/Tdays) {[ (1-)]/ (1-) } xsine {Inverse tan [(v* + v)/c]} degrees/100 years

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    Abstract: light measurements are done along the line of sight and we measure lightprojections to our eye. Meaning, that we do not measure distance r but we measure rcosine arc tan (v/c) when light is used and as a consequence instead of measuring tiT we measure T cosine arc tan (v/c) and here is the experimental proof of it.

    Your eyes

    A000 00000 00 0 0 0 00 0 0 0 00 0 0 0 00 0 (2) 0 0 00 (1) 0 0 (3) 0 0

    0 0 0 0 00 0 0 0 00 0 0 0 00 0 0 0 00 0 0 0 0B------------------------- 0 --------------- 0 ------------- 0

    1 2 3

    The projections of light is what we measure and the projection of 1and 2 and 3 is ABIf the angle between ray 1 and AB is (1)If the angle between ray 1 and AB is (2)If the angle between ray 1 and AB is (3)Then C (1) cosine (1) = C (2) cosine (2) = C (3) cosine (3) = c = ABYou want experimental proof?Here is my iron clad proof of my theory: This is using the lightprojections to be equal c then the advance of perihelion and stars tosolve mercury Venus and DI Herculis binary stars better than all is

    If an object at location A sends light signals in all directions at time at t = 0 whereB1 is;

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    And B1 is moving to B2 then the projection of AB2 of AB1 is measured. AB1 istheorized and AB2 is measured; or AB2 = AB1 cosine And = arc tan (v/c)B1B2 /AB1 = sine ; AB2/AB1 = cosine ; B1B2/AB2 = tan Instead of measuring time t we theorize time t and we measure time = t cosine

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    A Light V E L O C I T Y B2O O O O O O O O O O

    O C O

    O OO OO V O

    O OO O

    O OO O

    OB1

    = t cosine arc tan (v/c) = t {1- 2 sine {[arc tan (v/c)]/2}}

    - t = - 2 t sine {[arc tan (v/c)]/2}With r2 = h and 1/T= / = - 2r/r = 2/t

    Or T = t/2 or the time measurements changes are twice period changesOr ( t)/2 = - t sine {[arc tan (v/c)]/2} is the time delays for periods

    With t = 1 century and t in arc seconds is 15 times time seconds then

    ( t)/2 = - 15 T sine {[arc tan (v/c)]/2}; T = One centuryWith v = 47.9 (mercury) 29.8 (Earth) =18.1 km/sec

    ( t)/2 = - 15 (36526) sine {[arc tan (18.1/300,000)]/2] = 43

    = 15 x (36526/T (days)] [(r m r e)/ r e] = 43

    = 15 x (36526/T (days)] [(v m T m v e T e)/ v e T e] = 43

    = 15 x (36526/T (days)] [(v m v e)/ v e] = 43

    = 15 x (36526/T (days)] [(Tm/ Te) 2/3 1] = 43

    Or, Center of massgravity equation

    [(I O)/O] 0 = [ m/ (m + M)] (180/ ) (36526/ T m) (3600)] = 43

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    Mr Laplace yes you are deleted

    The solution to F = -GmM/r is notr = [a (1-)/ (1+ cosine )] and it is time you get corrected

    Real time solution is: r (, t) = [a (1-)/ (1+ cosine )] [ (r)+ (r)] t"Apparent advance of perihelion"

    Or, Boundary value law[(I O)/O] 0 == {[GM/r]} 1/2 [(r m r e)/ r e] [(180/ ) (3600) (36526/ T m) = 43

    = {[GM/r]} 1/2 [(v m v e)/ v e] [(180/ ) (3600) (36526/ T m) = 43

    = {[GM/r]} 1/2 [(Tm/ Te) 2/3 1] [(180/) (3600) (26526/T m)] = 43

    = {[GM/r]} 1/2 [(v m T m v e T e)/ v e T e][(180/) (3600) (26526/T m) = 43

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    Chapter Eleven

    Arabs real time physics in outer SpaceThe problems Einstein and all others can not solveApparent Apsidal motion of binary (two) stars

    This is the solution to the 150 years apsidal motion puzzle that is not solvable byspace-time physics or any said or published physics including 500 years of Modernphysics and 500,000 modern physicists. Binary stars apsidal motion or "Apparent"rate of orbital axial rotation is a visual effect along the line of sight of movingobjects applied to the angular velocity at Apses. From the thousands of close binarystars astronomers picked a dozen sets of binary stars systems that would be a

    good test of relativity theory and modern physics collected data for all of pastcentury and relativity theory failed every one of them. This rate of "apparent" axialrotation is given by this new equationW (ob) = (-720x36526/T) {[ (1-)]/ (1-) ]} (v* + v/c) degrees/100 yearsT = period; = eccentricity; v = spin velocity effect; v*= orbital velocity effectsThe simplest problem in physics that all 500 years modern physics and500,000 modern physicists could not solve by any physics:

    1 As Camelopardalis2 DI Herculis

    3 V1143 Cygni4 V 541 Cygni5 - AI Hydra6 - V 731 Cephei7 - SW Canis Majoris8 - NV Canis Majoris9 - GG Orion10- CM Draconis11- VV PYX12 EW Oriomis

    13- V1147 Sagittari14 PSR 1913 + 1612 PSR 0737 3039Solution: Location r = r r (1) ; Velocity v = r' r (1) + r ' (1)Acceleration = (r" - r') r (1) + (2r'' + r ") (1)S = m r; State = mass x distanceP = d S/ d t = d (m r)/d t = m (d r/d t) + (d m/d t) rVelocity = v = (d r/d t); mass rate change = m' = (d m/d t)P = m v + m' r; Momentum = change of state = change in location or change inmassF =d P/d t = d S/d t = d [m (d r/d t) + (d m/d t)]/d t

    = m d r/d t + (d m/d t) (d r/d t) + (d m/d t) (d r/d t) + (d m/d t) rPage 59

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    F = m d r/d t + 2 (d m/d t) (d r/d t) + (d m/d t) rForce = Change of momentumF = m a + 2 m ' v + m" r

    F = - GmM/rOr, Newton's Kepler's equation: F = - GmM/rThenWith d (m r)/dt - (m r) ' = -GmM/r Newton's Gravitational Equation (1)And d (mr')/d t = 0 Kepler's force law (2)With m = constant, then m can be taken out from both equations (1) and (2)With d r/d t - r ' = - GM/r Newton's Gravitational Equation (1)And d (r') /d t = 0 Kepler's force law (2)From 2: With m = constant; then d (mr')/d t = 0And m d (r')/d t = 0And d (r')/d t = 0And r' = hWith (1): d (m r)/dt - (m r) ' = -GmM/rWith m = constantThen m [d r/ d t - r '] = - Gm M/ rAnd [d r/ d t - r '] = - G M/ rLet r =1/uThen d r/d t = -u'/u = - (1/u) (') d u/d = (- '/u) d u/d = - h d u/d And d r /d t = - h 'du/d = - h u [du/d]And - h u [du/d] - (1/u) (hu) = - G MuOr, [du/ d] + u = G M/ h

    u = G M/ h + A cosine And r = 1/u = 1/ [G M / h + A cosine ]

    = (h/ G M)/ [1 + (Ah/ GM) cosine ]= (h/GM)/ (1 + cosine )

    Then r (, 0) = a (1-)/ (1+ cosine )

    This is Newton's Classical Equation solution of two body problem. We solved thisequation and we got the motion equation:Is: r (, t) = [a (1-)/ (1+ cosine )] which is the equation of an ellipse with

    eccentricity and semi - major axis a, and a semi- minor axis whose value is b = a [1 - ] and two foci one equals to c = a, and the other foci location equals to -c = - a. Or the motion of one ball around the other ball should be an ellipse withthe other ball at one of the foci +/- a, of the ellipse with semi major axes (- a, a)on x-axis and semi minor axes (-b, b) on y- axis and foci (- c, c) on x- axis againwith angle of rotation . If this law to work on two planets instead of two balls likeplanetary motion around the sun, then Astronomers should see this motion of aplanet moving around the sun in an ellipse with the sun at one of its foci.

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    What astronomers saw was not an ellipse but a rotating ellipse like the ellipsebelow wth rotating angle

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    M

    m

    M

    m

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    When the areas size A are sliced equally it was found that the times spent by planetsorbiting around the Sun and making areas A each are equal also.Or, r (0) ' (0) = r (1) ' (1) = r (2) ' (2) = r (3) ' (3) = --

    = location x [angular speed] = constant= Areal velocity

    If r '= hThen differentiating with respect to timeThen d (r ')/ d t= d h/ d tAnd 2 r r + r = 0Or 2 (r /r) = - (/)

    The r = r0 e t

    And = 0 e 2 t

    With r = r0 e t

    In real time r (n) = r (0) e t

    With r (0) ' (0) = r (1) ' (1)Then ' (1) = [r (0)/ r (1)]' (0)

    And ' (1) = {[e 2 t] ' (0)And (1) = {[cosine 2 t + sine 2 t] 1}' (0) (1) = (x) + (y)

    = [cosine 2 t + sine 2 t] ' (0) (x) = [cosine 2 t] ' (0) (x) = [1 2 sine t] ' (0)

    (x) - ' (0) = - 2' (0) sine t

    W = (x) - ' (0) = - 2' (0) sine t= -2(2) [ (1-)]/T (1-) ] sine tAnd ' (0) = h/r (0) = 2 a b/T a = 2 (1-)]/T (1-)

    W = - 4 ) [ (1-)]/T (1-) ] sine t

    If this apsidal motion is to be found as visual effects, thenWith, v = spin velocity; v* = orbital velocityAnd v/c = (v* + v)/c = tan t

    W = -4 [ (1-)]/T (1-) ] sine {Inverse tan [(v* + v)/c]} radians

    Multiplication by 180/ to change to degrees

    W = (-720/T) {[ (1-)]/ (1-) } sine {Inverse tan [(v* + v)/c]} DegreesAnd multiplication by 1 century = 36526 days and using T in days

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    W (ob) = (-720x36526/Tdays) {[ (1-)]/ (1-) } xsine {Inverse tan [(v* + v)/c]} degrees/100 years

    Astronomy re - written

    W (calculated) = (-720x36526/T) {[ (1- )]/ (1- ) ]} [(v + v*)/degrees/100 years

    1- As Cameloppardalis: Binary stars SystemAS Cam Data T=3.431; r (m) =0.1499; m=3.3 M (0); M=2.5 M (0)R (m) =2.57 R (0); [v (m), v (M)] = [40, 30]; = 0.1695; 1- = 00.8305R (M) = 2.5 R (0); r (M) =0.1111;m + M=5.8 M (0); G=6.673x10-11

    M (0) = 2 x 1030 kg; R (0) = 0.696x109m;The circumference of an ellipse: 2a (1 - /4 + 3/16()- --.) 2a (1-/4); R =a (1-/4)

    Finding orbital velocitiesFrom Newton's inverse square law of an ellipse motion applied to a circular orbitgives the following: m v/ r (cm) = GmM/rPlanet --- r (cm) ----- Center of mass ------- r (CM) --------- Mother SunPlanet ------------------- r -------------------------------------- Mother SunCenter of mass law m r (cm) = M r (CM); m = planet mass; M = sun massAnd r (cm) = distance of planet to the center of mass

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    Primary Secondary

    v(p) v* (p) v (p) v* (p) v (p) v* (p) v (p) V* (p)

    v(s) v* (s) Spin=[,][,]=orbit

    [,][,] [,][,] [,][,]

    Spin results v(p) + v(s) v(p) + v(s) - v(p) + v(s) -v(p) + v(s)Orbit results v*(p) + v*(s) -v*(p) + v*(s) v* (p) + v*(s) -v* (p) + v* (s)Examples AS CAMv (s) v* (s) [,][,] [,][,] [,][,] [,][,]Spin results v(p) + v(s) v(p) + v(s) -v(p) + v(s) -v(p) + v(s)Orbit results v*(p) - v*(s) -v*(p) - v*(s) v*(p) - v*(s) -v* (p) - v* (s)

    Examplesv (p) v*(s) [,][,] [,][,] [,][,] [,][,]Spin results v(p) - v(s) v(p) - v(s) -v(p) - v(s) -v(p) - v(s)Orbit results v*(p) + v*(s) -v*(p) + v*(s) v*(p) + v*(s) -v* (p) + v* (s)Examples AS CAM

    v (s) V*(s) [,][,] [,][,] [,][,] [,][,]Spin results v(p) - v(s) v(p) - v(s) -v(p) - v(s) -v(p) - v(s)Orbit results v*(p) - v*(s) -v*(p) - v*(s) v*(p) - v*(s) -v* (p) - v* (s)Examples AS CAM

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    And r (CM) = distance of sun to center of massAnd r (cm) + r (CM) = r = distance between sun and planetSolving to get: r (cm) = [M/ (m + M)] rAnd r (CM) = [m/ (m + M)] r

    Then v = [GM r (cm)/ r] = GM/ (m + M) rAnd v = [GM/ (m + M) r = a (1-/4)]Planet orbital velocity or primary velocity:

    And v* (m) = v (m) = [GM/ (m + M) a (1-/4)]R =a (1-/4)

    Calculations: (1- /4) = 0.9928[ (1-)]/ (1-) = 1.43With a = [R (m)/r (m)]= (2.57/0.1499) (0.696x109) = 11.9327x109

    And v* (m) = [GM/ (m + M) a (1- /4)] = 110km/sec= [6.673x10-11 (2.5) (2 x 1030)/ (5.8) 11.932x109 (0.9928)] = 110.178km/sec

    And v* (M) = [GM/ (m + M) a (1- /4)]= [6.673x10-11 (3.3) (2 x 1030)/ (5.8) 11.932x109 (0.9928)] = 145.435 km/sec

    Spin: v = 40 + 30=70km/secAnd v* (e) = v* Earth = 29.8 km/secAnd v (e) = 0.465 km/secThen v* + v = v* (m) + v* (M) + v* (e) + v (m) + v (M) + v (e)

    = 110.178 + 145.435 + 70 + 29.8 0.465 = 355 m/sec

    [ (1-)]/ (1-) = 1.43; T = 3.431days

    W= (-720x36526/T) x { [(1-)] (1-) } {[v* + v]/c}

    W= (-720x36526/3.431) x (1.43) (355/ 300,000) = 15.0/centuryDr Guinan and DR Maloney 1989: W= 15/century 1989DR Khailullin and Dr Kozyreva: 1983 W = 14.6 /centuryEinstein: 44.3/ century

    2 - Binary stars System: DI Her Apsidal Motion SolutionDI Her Apsidal motion solution:Data: T=10.55days r(m) = 0.0621 m=5.15M(0) R(m)=2.68R(0)[v(m),v(M)]=[45,45]And = 0.4882; r (M) = 0.0574 M=4.52 M (0) R (M) =2.48; m + M=9.67 M (0)L = 2000 +/- 200 Ly

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    Calculations1- = 0.5118; (1-/4) = 0.94; [ (1-)] / (1-) = 3.33181; 1 + = 1.4882;G=6.673x10-11; M (0) = 1.98892x19^30kg; R (0) = 0.696x109m

    V* (p) = [GM/ (m + M) a (1-/4)] = 99.88 km/secV* (s) = [Gm/ (m + M) a (1-/4)] = 113.8km/sec

    A- Apsidal motion is given by this formula:W (cal) = (-720x36526/T) {[ (1-)]/ (1-) ]} [(v + v*)/c] degrees/100yearsAnd v = - 45 km/s - 45 km/sec = 90km/secNow let us calculate v* (cm) = m v/m = 106.38km/secWith v* = 2 v*(cm) = 212.76 km/secAnd v = -90 km/secThen v* + v = 212.76 - 90 = 122.76 km/sec andW (cal) = (-720x36526/T) {[ (1-)]/ (1-) } sine [Inverse tan122.76/300,000]

    = (-720x36526/10.55) (3.33181) (122.76/300,000)W (cal) = 1.39/centuryWith = { [v* - v* (cm)] /2}

    = {[106.36 - 99.88]/2 + [106.36 - 113.8]/2} = 6.975 km/secThen W (cal) = 1.39/century +/- 0.16Observed 2004: 1.39 +/- 0.3/century; Relativity: 4.27/century

    B - W (cal) = (-720x36526/T) {[ (1-)]/ (1-) ]} [(v + v*)/c] degrees/100yearsWith v = - 45 km/s + 45 km/sec = 0 km/secAnd v* = v* (cm) = m v/m = 106.38km/sec

    W (cal) = (-720x36526/10.55) (106.38.300, 000) degrees/100 yearsW (cal) = 1.044 degrees/centuryC - V* (p) = [GM/ (m + M) a (1-/4)] = 99.88 km/sec

    With v* x (1-/4)/ (1-) = 99.88 (.94)/ (0.5118) = 135.36

    And v* x (1-/4)/ (1+ ) = 99.88 (.94)/ (1.4882) = 79.38K (A) = [(135.36 + 79.38)/2] = 107.37 km/secV* (s) = [Gm/ (m + M) a (1-/4)] = 113.8 km/sec

    With v* x (1-/4)/ (1-) = 113.8 (.94)/ (0.5118) = 154.2254 km/secAnd v* x (1-/4)/ (1+ ) = 113.8 (.94)/ (1.4882) = 90.44312 km/secK (B) = 122.3342 km/sec

    V* = [m K (A) + M K (B)]/ (m + M) = 114.3646 km/secOr v* = [K (A) + K (B)]/2 = 114. 85 km/sec; with v* = 114.85

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    And a = [R (m)/r (m)] R (0) = (1.88/0.0440)0.696x10^9m = 29.73818182x10^9mThen a (1-/4) = 28.03x10^9mAnd v (m) = [GM/ (m + M) a (1-/4)] = 75.5883km/sec; v (m) =24

    And v (M) = [Gm/a (m + M) (1-/4)] = 75.883km/sec; v (M) =24With v=24 + 24= 44km/secAnd v* = 151.1766km/secWith v* + v= 151.1766 - 48 = 103.1766km/secW (ob) = (-720x36526/T) {[ (1-)]/ (1-) ]} {[v* + v]/c} W (ob) = (- 720 x 365226/15.3379) (3.2339) (103.1766/300,000)W (ob) = 0.65Notice: [v (m), v (M)] = [24 2, 24 2]If v (m) = v (M) = 24 + 2 = 26Then v* + v= 151.1766 - 52 = 99.1766km/secAnd W (ob) = (- 720 x 365226/15.3379) (3.2339) (99.1766/300,000)W (ob) = 0.60/centuryObserved is W= 0.60 +/ -0.1/century Lacy = [0.5; 0.7]

    Relativity: W = 0.97/century

    1- Apsidal motion of V541Cgyni Lacy 1989

    5 - AI Hydra apsidal motion puzzle solution

    W (cal) = (-720x36526/T) {[ (1-)]/ (1-) } [(v+ v*)/c] degrees/100 yearsAI Hydra Apsidal motion solution:Data: T=8.29days r(m) = 0.1418 m=2.15M(0) R(m)=3.92R(0)[v(m),v(M)]=[28,27]; and = 0.0.23; r (M) = 0.1002 M=1.98 M (0) R (M)=2.77(0); m + M=4.13 M (0); L = 575 +/- 15 Ly

    Calculations1- = 0.77; (1-/4) = 0.986775; [ (1-)] / (1-) = 1.6414G=6.673x10^-11; M (0) = 1.98892x19^30kg; R (0) = 0.696x10^9mThen a = [R (m)/ r (m)] = 19.24062059 x 10 ^ 9 m

    V (m) = [GM/ (m + M) a (1-/4)] = 81.11439578 km/secV (M) = [Gm/ (m + M) a (1-/4)] = 88.11km/sec

    Apsidal motion is given by this formula:

    W (ob) = (-720x36526/T) {[ (1-)]/ (1-) ]} [(v + v*)/c] degrees/100years

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    With v* = v (m) + v (M) = 81.11439578km/sec + 88.11km/sec =169.2243958km/secAnd v = v (m) + v (M) = 28 + 27 = 55 km/sec

    Then (v* + v) = 224.2243958 km/secW (ob) = (-720x36526/T) {[ (1-)]/ (1-) } sine [Inverse tan224.2243958/300,000]

    = (-720x36526/8.29) (1.6414) (224.2243958/300,000)= 2.90/ century

    W (observed) = 2.90/century as measuredObserved is 2.90/centurySpace-Time Relativity theory 6.8 / centuryNow let us calculate v* (cm) = m v/m= 2.15 x 81.11439578 + 1.98 x88.11= 84.46822 km/secWith v* = 2 v*(cm) = 168.936411 km/sec; And v = 55 km/secThen v* + v = 223.9364411 km/sec and

    W (observed) = (-720x36526/T) {[ (1-)]/ (1-) } sine [Inverse tan 223. 936/300,00= (-720x36526/10.55) (3.33181) (223.9364411/300,000)W (observed) = 2.90/centuryWith = { [v* - v* (cm)] /2}

    = {[88.11 -84.46822]/2 + [81.11439578 - 84.46822]/2}= {[3.64178]/2 + [3.35382422]/2} = 3.5 km/sec

    Then W (ob) = 2.90/century; observed is W = 2.9/per centuryAnd Einstein's 100,000 space-timers 6.8 / centuryReferences: Go to Smithsonian/NASA website SAO/NASA and type:

    1- Apsidal motion of AI Hydra Popper 19852- KH. F. Khaliulullin and V.S Kozyreva 19883- Petrova - Ovlav Apsidal motion catalogue 19996 - V731Cehpei Apsidal Motion Solution

    Primary Secondary

    v(p) v* (p) v (p) v* (p) v (p) v* (p) v (p) V* (p)

    v(s) v* (s) Spin=[,][,]=orbit

    [,][,] [,][,] [,][,]

    Spin results v(p) + v(s) v(p) + v(s) - v(p) + v(s) -v(p) + v(s)Orbit results v*(p) + v*(s) -v*(p) + v*(s) v* (p) + v*(s) -v* (p) + v* (s)Examples

    V731Cepheiv (s) v* (s) [,][,] [,][,] [,][,] [,][,]Spin results v(p) + v(s) v(p) + v(s) -v(p) + v(s) -v(p) + v(s)Orbit results v*(p) - v*(s) -v*(p) - v*(s) v*(p) - v*(s) -v* (p) - v* (s)Examplesv (p) v*(s) [,][,] [,][,] [,][,] [,][,]Spin results v(p) - v(s) v(p) - v(s) -v(p) - v(s) -v(p) - v(s)Orbit results v*(p) + v*(s) -v*(p) + v*(s) v*(p) + v*(s) -v* (p) + v* (s)Examplesv (s) V*(s) [,][,] [,][,] [,][,] [,][,]Spin results v(p) - v(s) v(p) - v(s) -v(p) - v(s) -v(p) - v(s)

    Orbit results v*(p) - v*(s) -v*(p) - v*(s) v*(p) - v*(s) -v* (p) - v* (s)Examples V731Cephei

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    Next the same equation will be used to find the advance of Periastron or "apparent"apsidal motion of V731 binary stars system.

    V731Cehpei Apsidal Motion Solution

    W (ob) = (-720x36526/T) x{[ (1-)]/ (1-) } [(v+ v*)/c] degrees/100 years

    V731data [see below]

    T= 6.068567days; m= 2.577 M (0); M = 2.577 M (0)And [v (m), v (M)] = [19+/-3, 18+/-3]And = 0.0165 a = 23.27x R (0)

    Calculations

    M + m = 2.738; 1-=0.9835 1-/4=0.9999 R (0) = .696x10^9mWith v [21, 28] = [19 +/- 3] + [18 +/- 3] = 37 +/- 6

    With v* (p) = [GM/ (m + M) a (1-/4)] = 85.6111965km/sec

    And v* (M) = [Gm/ (m + M) a (1-/4)] = 109.38km/sec

    Also, [ (1-)]/ (1-) = 1.033694356

    With v* (cm) = 2m v/m = 96.46688km/sec; 2 v* (cm) = 192.9337619

    And = { [v*-v* (cm)] /2} = {[96.46688 - 85.6] /2} +{[109.38 - 96.46688] /2} = 11.9288422 km/sec

    With v* (p) = 85.6111965km/sec +/- 11.9288422 km/sec

    And v* (s) = 109.38km/sec +/- 11.9288422 km/sec

    Then v* (p) + v* (s) = [192.9337619 +/-] x 2 = 23.8567844 km/sec

    Then v* + v = 229.9288422km/sec +/- 29.8567844 km/secNow: Taking the upper limitThen v* + v = 229.9288422km/sec + 29.8567844 km/sec = 259.7856266km/sec

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    W (obo) = (-720x36526/T) x {[ (1-)]/ (1-) } {[v* + v]/c} W/century= (-720x36526/6.068567) (1.033694356)(259.7856266 /300,000)=2.91/century

    W/century = 3.35914177/century = 0.0335914177/year

    U = 360/0.0335914177 = 10717 years

    Observed values are U = 10000 +/- 2500

    References: 1- Absolute dimensional and apsidal motion of V731CepV. Batkis; M.Zejda; I. Bulut; M.Wolf; S. Bilir; H. Bakis; O.Demircan: J.w.Lee:M.Slechta: B. Kucerova. 2008

    7 - NV CMa Binary stars apsidal motion table

    8 - NV CMa apsidal motion solution:

    Data: T=1.885159 days; = 0; v* (p) = 128.55 km/sec; v* (s) = 130.87 km/sec[ (1-)] / (1-) = 3.33181; v (p) = 51.7 km/sec and v (s) = 52.4 km/secApsidal motion is given by this formula:W (ob) = (-720x36526/T) {[ (1-)]/ (1-) ]} [(v + v*)/c] degrees/100years

    With v* = v* (p) + v*(s) = 259.42 km/sec and v= v (p) + v (s) = 104.1And v* + v = 363.52 km/sec

    W (observed) = (-720x36526/T) {[ (1-)]/ (1-) }sine [Inverse tan 363.52/300,000]

    = (-720x36526/1.885159) (1) (363.52/300,000)= 20.48333818/century = 0.2048333818/year

    U = 360/0.2048333818/year;

    U = 1757. 5 years

    References: Go to Smithsonian/NASA website SAO/NASA and type:Absolute dimensions NV CMa; Kaluzny, J; Pych, W; Rucinski, S. M; Thompson, I.B

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    Relativity theory coffin nail # 8 SW Canis Majoris

    W (cal) = (-720x36526/T) {[ (1-)]/ (1-) ]} [(v + v*)/c] degrees/100years

    T = period = 10.09 days; = eccentricity = 0.3179

    And v = spin velocity effect = v (p) + v(s) = 57km/sec

    And v*= orbital velocity effect = v*(p) + v* (s)= 80.5 + 87.8 = 168.3 km/sec

    For SW Canis Majoris: v* + v = 225.3km/sec

    W (observed) = 2.99565967/century = 0.0299565967

    U = 360/ 0.0299565967= 12017years

    U (observed) = 12,000 yearsEinstein and space-timers 14,000 yearsSW Canis Majoris Binary stars

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    Primary Secondary

    v(p) v* (p) v (p) v* (p) v (p) v* (p) v (p) V* (p)

    v(s) v* (s) Spin=[,][,]=orbit

    [,][,] [,][,] [,][,]

    Spin results v(p) + v(s) v(p) + v(s) - v(p) + v(s) -v(p) + v(s)Orbit results v*(p) + v*(s) -v*(p) + v*(s) v* (p) + v*(s) -v* (p) + v* (s)Examples Sw Canis Majorisv (s) v* (s) [,][,] [,][,] [,][,] [,][,]Spin results v(p) + v(s) v(p) + v(s) -v(p) + v(s) -v(p) + v(s)Orbit results v*(p) - v*(s) -v*(p) - v*(s) v*(p) - v*(s) -v* (p) - v* (s)

    Examplesv (p) v*(s) [,][,] [,][,] [,][,] [,][,]Spin results v(p) - v(s) v(p) - v(s) -v(p) - v(s) -v(p) - v(s)Orbit results v*(p) + v*(s) -v*(p) + v*(s) v*(p) + v*(s) -v* (p)