GTARG is a computer program used to design orbit maintenance maneuvers for the TOPEX/Poseidon satellite. These maneuvers ensure that the ground track is kept within +/-1 km with of an = 9.9 day exact repeat pattern. Maneuver parameters are determined using either of two targeting strategies: longitude targeting, which maximizes the time between maneuvers, and time targeting, in which maneuvers are targeted to occur at specific intervals. The GTARG algorithm propagates nonsingular mean elements, taking into account anticipated error sigma's in orbit determination, Delta v execution, drag prediction and Delta v quantization. A satellite unique drag model is used which incorporates an approximate mean orbital Jacchia-Roberts atmosphere and a variable mean area model. Maneuver Delta v magnitudes are targeted to precisely maintain either the unbiased ground track itself, or a comfortable (3 sigma) error envelope about the unbiased ground track.
GTARG - The TOPEX/Poseidon ground track maintenance maneuver targeting program
AIAA, AHS, and ASEE, Aerospace Design Conference ; 1993 ; Irvine, CA, United States
1993-02-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
TOPEX/POSEIDON orbit maintenance maneuver design
NTRS | 1990
|TOPEX/POSEIDON Ground Track Maintenance Experience
NTRS | 1993
|Topex/Poseidon Autonomous Maneuver Esperiment (TAME)
NTRS | 1996
|Topex/Poseidon Autonomous Maneuver Experiment (TAME)
British Library Conference Proceedings | 1996
|TOPEX/Poseidon Orbit Acquisition Maneuver Sequence
British Library Conference Proceedings | 1993
|