Wallsgrove R J, Akella M R.Globally stabilizing saturated attitude control in the presence of bounded unknown disturbances[J].Journal of Guidance, Control and Dynamics, 2005, 28(5):957-963
[2]
Wang W, Li J F, Wang T S.Study on sloshing damping in a container of spacecraft(part 2):numerical method[J].Journal of Astronautics, 2006, 27(2):177-180
[3]
Jing W X, Xia X W, Gao C S, et al.Attitude control for spacecraft with swinging large scale payload[J].Chinese Journal of Aeronautics, 2011, 24(3):309-317
[4]
Zhang J R, Rachid A, Zhang Y.Attitude control for part actuator failure of agile small satellite[J].Acta Mechanica Sinica, 2008, 24(4):463-468
[5]
卢松涛, 王磊, 赵育善.双框架控制力矩陀螺奇异性分析[J].北京航空航天大学学报, 2008, 34(9):1096-1100 Lu Songtao, Wang Lei, Zhao Yushan.Double gimbal control moment gyroscopes singularity analysis[J].Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(9):1096-1100(in Chinese)
[6]
Wang W, Li J F, Wang T S.Study on sloshing damping in a container of spacecraft(part 1):theory[J].Journal of Astronautics, 2005, 26(6):687-692
[7]
Bryce A R, Jeffrey W K, Thomas B A, et al.Three-axis attitude control with two reaction wheels and magnetic torquer bars[R].AIAA 2004-5245, 2004
[8]
张尧, 黄庭轩, 徐世杰.星上控制力矩陀螺群隔振平台的动力学特性[J].北京航空航天大学学报, 2012, 38(1):80-85 Zhang Yao, Huang Tingxuan, Xu Shijie.Dynamic characteristic of vibration isolation platform of control moment gyroscopes on satellites[J].Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(1):80-85(in Chinese)
[9]
Kelly A, McChesney C, Smith P, et al.A performance test of fluidic momentum controller in three axes[D].Texas:The University of Texas, 2004
[10]
Wang W, Li J F, Wang T S.Study on sloshing damping in a container of spacecraft(part 2):numerical method[J].Journal of Astronautics, 2006, 27(2):177-180
[11]
Kumar K D.Satellite attitude stabilization using fluid rings[J].Acta Mechanic, 2009, 208(1/2):117-131
[12]
Zhang J R, Rachid A, Zhang Y.Attitude control for part actuator failure of agile small satellite[J].Acta Mechanica Sinica, 2008, 24(4):463-468
[13]
卢松涛, 王磊, 赵育善.双框架控制力矩陀螺奇异性分析[J].北京航空航天大学学报, 2008, 34(9):1096-1100 Lu Songtao, Wang Lei, Zhao Yushan.Double gimbal control moment gyroscopes singularity analysis[J].Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(9):1096-1100(in Chinese)
[14]
Nobari N A, Misra A.Satellite attitude stabilization using four fluid rings in a pyramidal configuration[C]//AIAA/AAS Astrodynamics Conference.Reston, VA:AIAA, 2010:7652-1-7652-13
[15]
Bryce A R, Jeffrey W K, Thomas B A, et al.Three-axis attitude control with two reaction wheels and magnetic torquer bars[R].AIAA 2004-5245, 2004
[16]
张尧, 黄庭轩, 徐世杰.星上控制力矩陀螺群隔振平台的动力学特性[J].北京航空航天大学学报, 2012, 38(1):80-85 Zhang Yao, Huang Tingxuan, Xu Shijie.Dynamic characteristic of vibration isolation platform of control moment gyroscopes on satellites[J].Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(1):80-85(in Chinese)
[17]
田林.考虑执行机构非线性的航天器姿态控制研究[D].北京:北京航空航天大学, 2012 Tian Lin.Study on spacecraft attitude control considering the nonlinearity of actuator[D].Beijing:Beijing University of Aeronautics and Astronautics, 2012(in Chinese)
[18]
Kelly A, McChesney C, Smith P, et al.A performance test of fluidic momentum controller in three axes[D].Texas:The University of Texas, 2004
[19]
Kumar K D.Satellite attitude stabilization using fluid rings[J].Acta Mechanic, 2009, 208(1/2):117-131
[20]
Nobari N A, Misra A.Satellite attitude stabilization using four fluid rings in a pyramidal configuration[C]//AIAA/AAS Astrodynamics Conference.Reston, VA:AIAA, 2010:7652-1-7652-13
[21]
田林.考虑执行机构非线性的航天器姿态控制研究[D].北京:北京航空航天大学, 2012 Tian Lin.Study on spacecraft attitude control considering the nonlinearity of actuator[D].Beijing:Beijing University of Aeronautics and Astronautics, 2012(in Chinese)
