[1] 赵炜渝,白保存,金仲和.皮纳卫星应用与特点分析[J].国际太空,2013(8):36-40.ZHAO W Y,BAI B C,JIN Z H.Analysis on application and characteristics of pico-and nano-satellite[J].Space International,2013(8):36-40(in Chinese).
[2] 林来兴.小卫星技术的发展和应用前景[J].中国航天,2006(11):43-47.LIN L X.Development and application prospect of moonlet technology[J].Aerospace China,2006(11):43-47(in Chinese).
[3] YANG C D,SUN Y P.Mixed H2/H∞,state-feedback design for microsatellite attitude control[J].Control Engineering Practice,2002,10(9):951-970.
[4] NEMATI H R,BAHRAMI M,EBRAHIMI B.Sliding mode control of a microsatellite attitude[C]//International Symposium on Systems and Control in Aeronautics and Astronautics.Pisca-taway,NJ:IEEE Press,2010:561-565.
[5] MCDUFFIE J H,SHTESSEL Y B.A de-coupled sliding mode controller and observer for satellite attitude control[C]//Proceedings of the American Control Conference,1997.Pisca-taway,NJ:IEEE Press,1997:564-565.
[6] BANG H,LHO Y.Sliding mode control for spacecraft contain-ing rotating wheels[C]//AIAA Guidance,Navigation,and Control Conference and Exhibit.Reston:AIAA,2001:1-8.
[7] CHEON Y J.Sliding mode control for attitude tracking of thruster-controlled spacecraft[J].Transaction on Control Automation & Systems Engineering,2002,3(3):257-261.
[8] QIAO J,GUO L.Antidisturbance fault tolerant control of attitude control systems for microsatellite with unknown input delay[J].Mathematical Problems in Engineering,2013,2013:804754.
[9] BELLAR A,FELLAH M K,MOHAMMED M A S.A cold gas thruster microsatellite attitude control[J].Revue Roumaine des Sciences Techniques-Serie électrotechnique et énergétique,2013,58(4):395-404.
[10] GRASSI M,PASTENA M.Minimum power optimum control of microsatellite attitude dynamics[J].Journal of Guidance,Control,and Dynamics,2015,23(5):798-804.
[11] QUEEN E M,SILVERBERG L.Optimal control of a rigid body with dissimilar actuators[J].Journal of Guidance,Control,and Dynamics,1971,19(3):738-740.
[12] HALL C,TSIOTRAS P,SHEN H.Tracking rigid body motion using thrusters and momentum wheels[J].Journal of the Astronautical Sciences,2002,50(3):311-323.
[13] SUN Z W,GENG Y,XU G,et al.The combined control algorithm for large-angle maneuver of HITSAT-1 small satellite[J].Acta Astronautica,2004,54(7):463-469.
[14] 孙兆伟,杨旭,杨涤.小卫星磁力矩器与反作用飞轮联合控制算法研究[J].控制理论与应用,2002,19(2):173-177.SUN Z W,YANG X,YANG D.The combined control algorithm for magnetorquer and reaction wheel of small satellite[J].Control Theory and Application,2002,19(2):173-177(in Chinese).
[15] 杨灵芝,魏延明,刘旭辉.MEMS固体微推力器阵列发展研究[J].空间控制技术与应用,2016,42(1):13-19.YANG L Z,WEI Y M,LIU X H.Development of MEMS solid micro thruster array[J].Aerospace Control and Application,2016,42(1):13-19(in Chinese).
[16] CHENG Y,JIANG B,ZHANG X.A micro-satellite attitude system using sliding mode observer and sliding mode controller with perturbation estimation[C]//International Symposium on Systems and Control in Aerospace and Astronautics.Pisca-taway,NJ:IEEE Press,2008:1-4.
[17] AHMED J,COPPOLA V T,BERNSTEIN D S.Adaptive asymptotic tracking of spacecraft attitude motion with inertia matrix identification[C]//IEEE Conference on Decision and Control,1997.Piscatway,NJ:IEEE Press,1998:2471-2476.
[18] ZOU A M,KUMAR K D.Adaptive fuzzy fault-tolerant attitude control of spacecraft[J].Control Engineering Practice,2011,19(1):10-21. |