Small Satellite Home Page - Established 1995

Home ] Up ] Amateur satellites ] Attitude and Orbit control ] Military Small sats ] Cancelled missions ] [ GPS Navigation ] On Board Data Handling ] Power Systems ] Remote sensing ] Store and Forward ]

 

Navigation - Small Satellites carrying GPS receivers

gps.gif (12644 bytes)Global Positioning System receivers provide highly accurate time and position information, and use  a constellation of 24 navigation satellites maintained by the US DOD in order to accurately determine their own position. Although designed for Terrestrial geolocation and navigation, the system can be employed in the highly dynamic environment in Low Earth Orbit. Landsat was the first civil spacecraft to carry a GPS receiver into orbit, but the receiver technology has advanced to a stage where GPS receivers can now routinely be carried on smaller platforms. Since Selective Availability has been switched off, accuracies in the order of 10m in all axis are achievable for simple position fixes. 

A space borne GPS receiver is different from a terrestrial receiver, as it travels at great velocity relative to the GPS constellation, and satellites tracked change constantly. As a consequence it has to cope with higher Doppler shifts and Doppler shift rates. In LEO this can be of the order of ±60kHz. Consequently, the receiver only has a short time available to perform a frequency/code search in order to lock onto the spread spectrum GPS signals. In order to predict GPS satellite visibility, the antenna geometry and orbital dynamics of the host satellite must be well known. For more precise applications, differential and double-differential filtering of GPS is proposed for formations of satellites. For greater precision, kinematic GPS employs the basic understanding of the dynamics to further improve accuracy. 

Orbit determination using GPS receivers on small satellites is now well demonstrated, and the next challenge now is to perform attitude determination on a small platform. Several small missions have recently been launched in order to demonstrate this. GPS can also be used in ionospheric research, and this is achieved by monitoring GPS signals as the satellite-to-satellite path skims the upper atmosphere.

GPS can only be effectively used near the Earth's surface, but various experiments have demonstrated that sidelobe signals can be picked up above the GPS constellation at 20,000; e.g. from Geostationary heights. 

Satellite Launch Receiver Channels Antennas Status
ORBComm-X 1991 Trimble Tans II 6 1 Spacecraft not operational
Radcal 1993 2x Trimble Tans Quadrex 6+6, L1 C/A 4 To demonstrate post processing attitude determination
PoSat-1 1993 Trimble Tans II with LEO firmware 6 1 Operational, orbit determination
DarpaSat 1994 Rockwell AST-5 6, L1, L2 2 Operational, orbit determination
Step-0 (TAOS) 1994 Rockwell AST-5 6, L1, L2 ? -
APEX 1994 Trimble TANS II 6 1 -
MICROLAB 1995 JPL/AOA Turbo Rogue(GPS-MET) + Trimble Tans 8+6 1+4 Operational, atmospheric measurements
ORBCOMM-FM1 1995 Trimble Tans II 6 4 To demonstrate real time orbit determination
ORBCOMM-FM2 1995 Trimble Tans II 6 4 To demonstrate real time orbit determination
FASat-alfa 1995 Trimble Tans II with LEO firmware 6 1 Spacecraft not operational
GEMStar 1995 Trimble Tans Vector Launch failure
REX-II 1996 2xTrimble Tans Vector 6 4 Operational, demonstrated orbit and attitude fixes
420-600mm baslines, aligned better than 0.1 degree

Reported 0.3-0.5 degree accuracy

Zeya 1997 GPS and Glonass Launched
Lewis 1997 SS Loral Tensor ? 4 Satellite malfunctioned
Clark 1997 Trimble Tans Vector Programme abandoned. There were plans for real time attitude determination
ØRSTED 1998 Trimble Tans II + modified JPL Turbo Rogue 6+8 2 Launched
SunSat 1998 JPL Turbo Rogue 8 1 Launched
FASat-Bravo 1998 Trimble Tans II with LEO firmware 6 1 Launched
SNOE 1998 JPL MicroGPS no correlator 1 Launched
Phase-3D AMSAT GPS receiver ? 8 Launched
TMSat-1 1998 SSTL SGR-10 12 2 Launched
UoSAT-12 1999 SSTL SGR-20 24 5 Demonstrated simultaneous tracking of 12 satellites and "lost in space" solution within 4 minutes.
SeaStar 1997 Motorola Viceroy ? 2
STRV-1c 2000 JPL MicroGPS no correlator, L1, L2 1 Launched, but can not be operated
Teamsat (/Yes) 1997 Trimble TANS II 2 Launched. Aimed to show GPS use above the GPS constellation.
Equator-S 1998 Aim to show GPS use above the GPS constellation.
SAC-A 1998 4? Differential GPS, aim to measure position to sub-10cm accuracy
Tsinghua-1 2000 SSTL SGR-10 12 2 Operational
SNAP-1 2000 SSTL SGR-05 12 1 Operational
HETE-II 2000 CNES      
SAC-C 2000 Blackbeard      
CHAMP   JPL BlackJack      
SimpleSAT 2001 Trimble Vector     Never operated
PICOSat 2001 JPL Turbo-Rogue     Receiver part of ionospheric occultation experiment
PCSAT 2001       Operational
PROBA 2001 SSTL SGR-20 24   Operational
GRACE 1&2 2002        
ALSAT-1 2002 SSTL SGR-20 24   Operational
Mozhayets 2002        
FedSat 2002 dual frequency      

The Trimble series 6 channel receivers are equipped with LEO firmware, to allow them to operate in the highly dynamic environment of space, with high velocity and high velocity derivatives. The Trimble Tans II employs a 68000 processor. The Quadrex employs antenna switching to commutate between four antennas. The Vector is a Quadrex which includes a coprocessor to permit basic attitude determination.

Further information on space-borne GPS can be found at the Department of Geodesy and Geomatics Engineering, University of New Brunswick.

References
[1] Precise platform positioning with a single GPS receiver, S.B.Bisnath et al, GPS World, April 2002, [http://www.gpsworld.com]
[2]
JPL Press release for BlackJack [http://www.jpl.nasa.gov/releases/2000/blackjackgps.html]

 

sshp_footer.jpg (14290 bytes)