TY - GEN
T1 - Fuel-balanced satellite formation keeping research
AU - Huang, He
AU - Zhou, Jun
AU - Liu, Yingying
PY - 2010
Y1 - 2010
N2 - How to balance each satellite fuel consumption during the period of satellite formation keeping, which can increase the total life span, is of great importance. For the plane circle formation which center was a virtual satellite, a new formation keeping control method was presented considering the fuel equalization constraint. The satellite which remain fuel was the least was chosed to be the reference satellite, and its state relative to the virtual center was considered to be ideal. By optimizing the phasing angle of the reference satellite, the motivation magnitude of the other satellites can be programmed, which made the satellite which remain fuel more consume more fuel. Finally, the impulse of each satellite was calculated by linear programming. Simulation results manifest, with this new method of satellite formation keeping, the fuel consumption of each satellite can be balanced while the total fuel consumption of formation was suboptimal.
AB - How to balance each satellite fuel consumption during the period of satellite formation keeping, which can increase the total life span, is of great importance. For the plane circle formation which center was a virtual satellite, a new formation keeping control method was presented considering the fuel equalization constraint. The satellite which remain fuel was the least was chosed to be the reference satellite, and its state relative to the virtual center was considered to be ideal. By optimizing the phasing angle of the reference satellite, the motivation magnitude of the other satellites can be programmed, which made the satellite which remain fuel more consume more fuel. Finally, the impulse of each satellite was calculated by linear programming. Simulation results manifest, with this new method of satellite formation keeping, the fuel consumption of each satellite can be balanced while the total fuel consumption of formation was suboptimal.
KW - Fuel equalization
KW - Linear programming
KW - Satellite formation keeping
UR - http://www.scopus.com/inward/record.url?scp=78651295115&partnerID=8YFLogxK
U2 - 10.1109/ICICISYS.2010.5658538
DO - 10.1109/ICICISYS.2010.5658538
M3 - 会议稿件
AN - SCOPUS:78651295115
SN - 9781424465835
T3 - Proceedings - 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
SP - 16
EP - 20
BT - Proceedings - 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
T2 - 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
Y2 - 29 October 2010 through 31 October 2010
ER -