| Citation: | YANG Bo, LI Jiaxing. A high-precision attitude coordinated control method using MEMS thruster for pico- and nano-satellite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(7): 1378-1386. doi: 10.13700/j.bh.1001-5965.2017.0481(in Chinese)
|
To achieve high precision attitude control for the pico- and nano-satellite at low cost, this paper presents a coordinated control method of double actuators using flywheel and solid propellant microthruster (SPM) array. The global fast terminal sliding mode controller is adopted to solve the rapid maneuvering of disturbed pico- and nano-satellite, which is verified by the Lyapunov stability. Meantime, the energy optimal switching strategy is derived, namely, the three sections of individual flywheel control, flywheel and SPM array coordinated control and individual SPM array control. In this way, the dual effects of high attitude stability precision and global minimum consumption of SPM array are realized. In this paper, the Monte Carlo method is used to optimize the allocation matrix in order to arrange the ignition sequence reasonably and minimize the consumption of the SPM array. The results of numerical simulation show that the coordinated control method of double actuators enables the pico- and nano-satellite complete high precision attitude control tasks at low cost, the attitude angle precision is 0.045 7°, and the attitude angular rate precision is 0.006 2 (°)/s.
| [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. http://www.cqvip.com/QK/70785X/201505/666539706.html
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). http://www.cqvip.com/QK/70785X/201505/666539706.html
|
| [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. doi: 10.3969/j.issn.1672-9463.2006.11.017
LIN L X.Development and application prospect of moonlet technology[J].Aerospace China, 2006(11):43-47(in Chinese). doi: 10.3969/j.issn.1672-9463.2006.11.017
|
| [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. doi: 10.1016/S0967-0661(02)00049-7
|
| [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. doi: 10.1016/S0094-5765(03)00223-6
|
| [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. http://cdmd.cnki.com.cn/Article/CDMD-90002-2008098335.htm
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). http://cdmd.cnki.com.cn/Article/CDMD-90002-2008098335.htm
|
| [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. http://www.cqvip.com/QK/93093A/201601/667960347.html
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). http://www.cqvip.com/QK/93093A/201601/667960347.html
|
| [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. doi: 10.1016/j.conengprac.2010.08.005
|
Figures(8) / Tables(3)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
DownLoad:
