Doman D B, Gamble B J, Ngo A D. Quantized control allocation of reaction control jets and aerodynamic control surfaces[J]. J of Guidance, Control, and Dynamics, 2009, 32(1): 13-24.
(Zhang B, Wu H X. Complete configuration of unidirectional actuator system[J]. Acta Automatica Sinica, 2000, 26(3): 392-395.)
[4]
Peter J W. Minimum control authority plot: A tool for designing thruster systems[J]. J of Guidance, Control, and Dynamics, 1994, 17(5): 998-1006.
[5]
Crawford B S. Configuration design and efficient operation of redundant multi-jet systems[C]. Proc of AIAA Guidance Control and Flight Mechanics Conf. Princeton: AIAA Press, 1969.
(Zhang B. Study on the fault-tolerant control method for the reaction control system[D]. Beijing: Doctoral Dissertation of China Academy of Space Technology, 1998: 42-51.)
[8]
Ankersen F, Wu S F. Optimization of spacecraft thruster management function[J]. J of Guidance, Control, and Dynamics, 2005, 28(6): 1283-1290.
[9]
Pablo A S. Control allocation for gimbaled/fixed thrusters[J]. Acta Astronautica, 2010, 66(3/4): 587-594.
[10]
Jin H P, Wiktor P, DeBra D B. An optimal thruster configuration design and evaluation for quick step[J]. Control Engineering Practice, 1995, 3(8): 1113-1118.
[11]
Hwang T W. Upper-stage launch vehicle servo controller design considering optimal thruster configuration[C]. Proc of AIAA Guidance, Navigation, and Control Conf and Exhibit. Austin: AIAA Press, 2003.
[12]
Bard S C. Configuration design and efficient operation of redundant multi-jet systems[C]. Proc of AIAA Guidance Control and Flight Mechanics Conf. Princeton: AIAA Press, 1969.
[13]
Pablo A S, Ricardo S S P. Thruster design for position/attitude control of spacecraft[J]. IEEE Trans on Aerospace and Electronic Systems, 2002, 38(4): 1172-1179.
(Zhang B, Wu H X. Complete configuration of unidirectional actuator system[J]. Control Engineering of China, 1998, 1(4): 6-13.)
[16]
张贤达. 矩阵分析与应用[M]. 北京: 清华大学出版社, 2004.
[17]
(Zhang X D. Matrix analysis and application[M]. Beijing: Tsinghua University Press, 2004.)
[18]
Richard H S. Control allocation for the next generation of entry vehicle[C]. Proc of AIAA Guidance, Navigation, and Control Conf and Exhibit. Monterey: AIAA Press, 2002.
(Guo F. The research on fast route planning of lift bodytype vehicle for reentry segment[D]. Harbin: Research Center of Satellite Technology, Master Dissertation of Harbin Institute of Technology, 2008.)