Simplified Femto-satellite Operations for Disaster Mangement Missions Joshua Tristancho UPC...
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Transcript of Simplified Femto-satellite Operations for Disaster Mangement Missions Joshua Tristancho UPC...
Simplified Femto-satellite Operations
for Disaster Mangement Missions
Joshua Tristancho
UPC Barcelona Tech - SPAIN
Jordi L. Gutiérrez
Applied Physics department (UPC)
October 3rd, 201263rd International Astronautical Congress, Naples, Italy. 10IAC-12-B4.3.12
2
Index
1. Introduction
2. Task analysis for DM
3. Simplified method for femtosat
4. Simulation of a mission
5. Conclusions
License:
Team FREDNET
Creative Commons
http://creativecommons.org/licenses/by-nc-sa/2.5/es/deed.en
Inde
x
3
Introduction (I) – Space Payload Paradigm
Femto-Satellite: New technological limit (<100 grams) The lower the satellite mass, the lower the launcher size
and so, the lower the cost. Swarms. Constellations Very-Low Earth Orbit, short mission life (few weeks) and
more reusable orbits
1. I
ntro
duct
ion
4
Introduction (II) – Femto-satellite specs.
Minimal number of subsystems:High gain and sensitivity modem Microstrip antenna
Attitude control (Magnetorquers) High resolution payload camera
Passive thermal control Electrical power management
Payload separated from the satellite LiPoly battery source
High accuracy attitude and position determination
Optimized on-board computer (Arduino like)
TECHNOLOGIES
- Use of MEMS
- SMD technology
- High G load tolerant
Femto-satellite protoype without
battery.(Less than 8 grams)
Source: www.wikisat.org
1. I
ntro
duct
ion
5
Introduction (III)
Types of disasters that a femto-satellite can address:– Earthquake Changes in the first week– Tsunami Short duration (Except Drought)– Drought Tens of meters per pixel– Cyclone Not very high resolution– Fire– Flood– Landslide– Volcano
1. I
ntro
duct
ion
6
Introduction (IV)
The emergency cycle by Lew Sian Many launch stations aruound the world in the
Preparedness phase Femto-satellites will be used mainly in the Response
phase. First hours are critical for the first responders
1. I
ntro
duct
ion
7
LEO satellite tasks for Disaster Management
Earth Observation– Acquire images from the Disaster Area– Send this images to Decision Makers
Data Relay– Provide basic communications to First Responders
2. T
ask
anal
ysis
for
DM
8
Initial hypotheses (I)
Use of femto-satellite swarm dedicated a single mission
Each femto-satellite will perform a revisit every day
Aerodynamic drag - Femto-satellite life 1 or 2 weeks
Femto-satellite horizon is about 2,000 km (Very-LEO)
Femto-satellite transit could have an angle (Corrections)
2. T
ask
anal
ysis
for
DM
9
Initial hypotheses (II)
Limited energy – Only use energy when– Recording– Communications– Attitude corrections
No solar panels to recharge the battery – Energy budget
2. T
ask
anal
ysis
for
DM
10
Initial hypotheses (III)
High power wireless modem. No huge ground station required
Two download modes:– Slow long range:
200 km footprint– Fast short range:
50 km footprint
Information is not
encrypted (Global interest)2. T
ask
anal
ysis
for
DM
11
Agents
Interest Point = First Responders Ground Stations = Decision Makers
Simplified List:– First coordinate point is the Disaster Area Epicenter– The rest of coordinate points are Ground Stations
2. T
ask
anal
ysis
for
DM
12
Ground Station policy (I)
No priority between Ground Stations
Nearest Ground Station will be kept until it is lost
A change between station is a waste of time
Ground Stations closer than 1,000 km between them are useless
Ground Stations near the Disaster area are useless. The priority is for the First Responders2.
Tas
k an
alys
is f
or D
M
13
Ground Station policy (II)
The less number of Ground Stations the higher life due to both– Battery duration (No solar panels) and– in-orbit time (Aerodynamic drag)
Share the info through a single agency– i.e. UN-SPIDER– Less femto-satellite consumption– Larger life
2. T
ask
anal
ysis
for
DM
14
The Simplified Method (I)
List of coordinates (Up to eight coordinates)
First coordinate is the Interest Point and it has absolute priority. First Responder are there by definition
The rest of coordinates are ground stations without priority. Decision Makers or other agents3.
Sim
plifi
ed m
etho
d fo
r fe
mto
sat
15
The Simplified Method (II)
Aerodynamic attitude only
abandoned when a coordinate
should be follow
The femto-satellite broadcast the information when there is a coordinate to follow (200 km footprint)
It tries to establish a fast download (50 km footprint)
If succeeds, a new coordinate list could be uploaded by the Ground Station if password is provided3.
Sim
plifi
ed m
etho
d fo
r fe
mto
sat
16
The Simplified Method (III)
The femto-satellite always follows the same Ground Station until it is not in view, then follows the nearest Ground Station if not, aerodynamic attitude is kept
The only exception to the previous statement is when the Interest Point coordinate appears; then aerodynamic attitude or previous coordinate is abandoned
It is possible to acquire and establish a link at the same time when First Responder has a Wireless equipment that works as a Ground Station (Optimum case)
3. S
impl
ified
met
hod
for
fem
tosa
t
17
The case of Sri Lanka – Tsunami impact (I)
00:58:53, 26 Dec 2004 (UTC) Magnitude 9.1 to 9.3 Mw Epicenter 3.316 N, 95.854 E Depth 30 km (19 mi) 250,000 deaths
4. S
imul
atio
n of
a m
issi
on
21
The case of Sri Lanka – Tsunami impact (III)
A single femto-satellite launched few hours after the disaster
Coordinate List based on two points– Matara
(Sri Lanka)– Mas Palomas
(Spain)
4. S
imul
atio
n of
a m
issi
on
http://4.bp.blogspot.com/-T3kYiRiDed0/TyZmUR5zlJI/AAAAAAAAG7w/P90Nene0IcY/s1600/tsunami_sri_lanka.gif
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The case of Sri Lanka – Tsunami impact (IV)
Femto-satellite provides coverage during 8 days
4. S
imul
atio
n of
a m
issi
on
23
The case of Sri Lanka – Tsunami impact (V)
2 h and 24 minutes after, First Responders have images
4. S
imul
atio
n of
a m
issi
on
24
The case of Sri Lanka – Tsunami impact (VI)
8 contacts with First Responders (One every day) 30 contacts with Mas Palomas Ground Station
4. S
imul
atio
n of
a m
issi
on
25
Conclusions
Following the Space Payload Paradigm, swarm of femto-satellites will be sent with a low-cost. It will be feasible thanks to a huge reduction of mass through a simple design and operation
Space responsive femto-satellites will be dedicated to Disaster Management (DM) mainly in the Responsive phase. First hours are critical for the First Responders
Real-time pictures are sent to the First Responders via wireless. No large infrastructure is required
The operation of each femto-satellite is simplified using a List of Coordinates. The first is the Interest Point. The rest are scheduled downloads for Decision Makers or others agents
5. C
oncl
usio
ns
26
Thanks for your attention!
This work has been supported by the MITYC under the contract reference TSI-020100-2010-138 as a part of the grant AVANZA competitividad I+D+I 2010