A TESTBED FOR STUDENT RESEARCH AND DESIGN OF CONTROL-MOMENT GYROSCOPES FOR ROBOTIC APPLICATIONS ASEE...
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Transcript of A TESTBED FOR STUDENT RESEARCH AND DESIGN OF CONTROL-MOMENT GYROSCOPES FOR ROBOTIC APPLICATIONS ASEE...
A TESTBED FOR STUDENT RESEARCH AND DESIGN OF CONTROL-MOMENT GYROSCOPES FOR
ROBOTIC APPLICATIONS
ASEE Annual Conference & Exposition – Austin, Texas
June 15, 2009
Albert Soto,
Daniel Brown, Mason Peck
Space Systems Design Studio at Cornell University
Overview
• Experimental Learning• Space-Robotics• Drive Design• Momentum Actuators• Reactionless Robotics• Specifications & Design• Student Benefits
Space Systems Design Studio ASEE June 2009
Experimental Learning• Fundamentals of Professionals• Research Project-Oriented
Learning– Teamwork– Self-confidence– Opportunity to apply coursework– Experience– Visualize professional career– Retention in engineering
• Limiting Factors of Aerospace Research– Infrequent microgravity flight trips– Risks in spaceflight launch– Limited resources
Space Systems Design Studio ASEE June 2009
NASA Microgravity Research Aircraft
Space-Robotics
• Robotic Arm Technology– Satellite assembly– Massive cargo relocation– Spacecraft repair
Space Systems Design Studio ASEE June 2009
Actuator Design
• What is a Drive Design?• Direct Drives
– Conventional actuators for robotic arm joints
• Control-Moment Gyroscopes (CMGs)– Traditional spacecraft attitude control
• CMGs vs. Direct Drives– Reactionless actuation– Energy advantage?
Space Systems Design Studio ASEE June 2009
Momentum Actuators
• Control-Moment Gyroscope (CMG)– Constant-speed rotor
– Gimbal the rotor about g-axis to change angular-momentum vector h
– 100x less power than RWAs1,2
– CMGs produce greater torque for less energy
0rotorE h
out
h
Space Systems Design Studio ASEE June 2009
1. Carpenter, Peck, 20082. Van Riper, Liden, 1971
Comparison of CMGs to direct drive needed to bring CMGs into robotics
h
gτ
outτ
Space Systems Design Studio ASEE June 2009
Joint motor CMGs
Torque reacted on spacecraft
No actuator torque reacted on spacecraft
Reactionless Robotics
• Actuator reaction torques
• Inertial reaction forces– From D’Alembert’s
principle• Benefits of CMGs
– Reduce disturbances and low frequency vibrations
– Isolate subsystems– Increased agility of
robot– More power efficient
than RWAs1,2
7
R1j
j
-R1
R1
-R1
CMG
1. Carpenter, Peck, 20082. Van Riper, Liden, 1971
Reactionless Robotics in Space• Robotic manipulators
– Space construction and repair
• Pointing tasks– Independently orient
cameras, sensors, transmitters, solar panels, etc.
• Reduced propellant use in attitude control– Reduce launch mass– Extend mission life
DARPA SUMO spacecraft & Cornell CMG team
Space Systems Design Studio ASEE June 2009
Efficient use of limited spacecraft power
Power Requirements
• Power equations of output torques:– in terms of the joint torques and velocities
Power equations do not equal!
22121211 CMGP 2211Joint P
Space Systems Design Studio ASEE June 2009
CMG power has not previously been compared to direct drive for robotics
Testbed Specifications
Space Systems Design Studio ASEE June 2009
• Planar two-link robot– +/- 90 deg range
• Dually actuated – CMGs from robot arm– DC motors at joints
• Air bearing levitation• Wireless control/data
acquisition • Expandable to 3-link robot • Removable base link
The Scissored-Pair CMG Configuration
Space Systems Design Studio ASEE June 2009
DC Motor
Gear
CMG
hr1
hr1+hr2
C1+C2
C2 C1
Benefits
Space Systems Design Studio ASEE June 2009
• Student introduction to:– Reactionless robotics– Momentum actuators– Dynamics of CMGs– Research– Ground testing of space-systems– Mechanical design and fabrication
Experience for excellence in engineering
• Advances faculty and graduate students– New experimental
hardware– Design groups
Future Possibilities
Space Systems Design Studio ASEE June 2009
• Additional Focuses:• Optimizing CMG size• Real-time data collection
and analyses• Control laws for N-link
robotic arm
Single link Two links
Space Systems Design Studio ASEE June 2009
Acknowledgements
• Space Systems Design Studio– Dr. Michele Carpenter
• Cornell Leadership Alliance
• Cornell 2007 CMG team– Mike Nagele– Nicole Monahan
Space Systems Design Studio ASEE June 2009
Momentum Actuators
• CMGs are part of a larger class of actuators
• Internal momentum change provides output torque
• A spinning body resists change – Magnitude or direction of spin
• Reaction Wheel Assembly (RWA)– Rotor fixed to spacecraft– Vary rotor speed magnitude– Large energy change of rotor
t̂
2 22 1
1
2rotor rE I
out
h
h
Space Systems Design Studio ASEE June 2009