[1]林来兴.小卫星编队飞行及其轨道构成[J]. 中国空间科学技术, 2001(1):2328.
LIN L X. Formation flying of small satellite and its orbital configuration[J]. Chinese Space Science and Technology, 2001(1):2328.
[2]FERGUSON P, HOW J P. Decentralized estimation algorithms for formation flying spacecraft[C]//AIAA Guidance, Navigation and Control Conference and Exhibit. Austin, Texas, 2003.
[3]ALONSO R, CRASS IDIS J L, JUNKINS J L. Vision based relative navigation for formation flying of spacecraft[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit. Denver: CO, 2000.
[4]CORAZZINI T, HOW J P. Onboard GPS signal augmentation for spacecraft formation flying[C]//Proceedings of the Institute of Navigation GPS, Institute of Navigation. Nashville, 1998, 19371946.
[5]OLSEN E. GPS sensing for formation flying vehicles[D]. Stanford, California: The Stanford University, 1999:118.
[6]KROES R, MONTENBRUCK O, BERTIGER W, et al. Precise GRACE Baseline Determination Using GPS[J]. GPS Solution. 2005(9):2131.
[7]ALFRIEND K T, GIM D W, SCHAUB H. Gravitational perturbations, nonlinearity and circular orbit assumption effects on formation flying control strategies[J]. Guidance and control 2000, 2000:139158.
[8]张洪华,林来兴.卫星编队飞行相对轨道的确定[J].宇航学报, 2002,23(6):7780.
ZHANG H H, LIN L X. The determination of relative orbit for formation flying[J].Journal of Astronautics, 2002,23(6):7780.
[9]秦永元,张洪钺,汪叔华.卡尔曼滤波与组合导航原理[M].西安:西北工业大学出版社,2007:182 |