TY - GEN
T1 - GPU accelerated genetic algorithm for in-SAR cluster configuration keeping across-track baseline under the J2 perturbation
AU - Yu, Kai
AU - Xu, Ming
AU - Liu, Shengli
PY - 2013
Y1 - 2013
N2 - In recent years, distributed small satellites interferometer synthetic aperture radar (InSAR) has been attracted many attentions for superior performance and potential application. According to the digital elevation model, the across-track baseline is one of important factors, which determined by the relative height measurement accuracy. The across-track baseline of the InSAR system can't configure to constant unless infinite satellites are employed. Fortunately, we can get the near-constant across-track baseline from 3-satellites formation. The paper present the existence of J2 invariant relative orbits by the parameters of (E, Hz,δr), which based on the arbitrary relative magnitude over the infinite time using the Routh reduction and Poincare techniques in the J2 Hamiltonian problem. It is optimized by the GPU accelerated Genetic Algorithm to have the best J 2 invariant relative orbit, and then it design the configuration form the crafts' magnitudes and phases. Copyright
AB - In recent years, distributed small satellites interferometer synthetic aperture radar (InSAR) has been attracted many attentions for superior performance and potential application. According to the digital elevation model, the across-track baseline is one of important factors, which determined by the relative height measurement accuracy. The across-track baseline of the InSAR system can't configure to constant unless infinite satellites are employed. Fortunately, we can get the near-constant across-track baseline from 3-satellites formation. The paper present the existence of J2 invariant relative orbits by the parameters of (E, Hz,δr), which based on the arbitrary relative magnitude over the infinite time using the Routh reduction and Poincare techniques in the J2 Hamiltonian problem. It is optimized by the GPU accelerated Genetic Algorithm to have the best J 2 invariant relative orbit, and then it design the configuration form the crafts' magnitudes and phases. Copyright
UR - https://www.scopus.com/pages/publications/84904698812
M3 - 会议稿件
AN - SCOPUS:84904698812
SN - 9781629939094
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 4341
EP - 4348
BT - 64th International Astronautical Congress 2013, IAC 2013
PB - International Astronautical Federation, IAF
T2 - 64th International Astronautical Congress 2013, IAC 2013
Y2 - 23 September 2013 through 27 September 2013
ER -