Small satellite maneuver based on terminal sliding mode control

CHANG Lin; JIN Guang; FAN Guo-wei; XU Kai

doi:10.3788/OPE.20152302.0485

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Small satellite maneuver based on terminal sliding mode control

更新时间：2020-08-13

- Small satellite maneuver based on terminal sliding mode control
- Optics and Precision Engineering Vol. 23, Issue 2, Pages: 485-496(2015)
- 作者机构：
  
  1. 中国科学院大学北京,中国,100049
  2. 中国科学院长春光学精密机械与物理研究所小卫星技术国家地方联合工程研究中心,吉林长春,130033
- 作者简介：
- 基金信息：
- DOI：10.3788/OPE.20152302.0485
  CLC： V474.2
- Received：05 April 2014，
  
  Revised：27 May 2014，
  
  Published：25 February 2015
- 稿件说明：
移动端阅览
常琳, 金光, 范国伟等. 基于terminal滑模控制的小卫星机动方法[J]. 光学精密工程, 2015,23(2): 485-496

CHANG Lin, JIN Guang, FAN Guo-wei etc. Small satellite maneuver based on terminal sliding mode control[J]. Editorial Office of Optics and Precision Engineering, 2015,23(2): 485-496
常琳, 金光, 范国伟等. 基于terminal滑模控制的小卫星机动方法[J]. 光学精密工程, 2015,23(2): 485-496 DOI： 10.3788/OPE.20152302.0485.

CHANG Lin, JIN Guang, FAN Guo-wei etc. Small satellite maneuver based on terminal sliding mode control[J]. Editorial Office of Optics and Precision Engineering, 2015,23(2): 485-496 DOI： 10.3788/OPE.20152302.0485.

摘要

采用terminal滑模控制方法研究了以单框架控制力矩陀螺(SGCMG)为执行机构的小卫星的姿态机动控制。首先

基于修正罗德里格斯(MRP)参数建立了小卫星数学模型

以terminal滑模控制方法进行控制力矩规划。然后

采用SGCMGs作为小卫星执行机构

以非对角奇异鲁棒操纵律跟踪terminal 滑模控制产生的期望力矩;通过仿真分析归纳出terminal滑模控制设计参数的变化规律和选取原则。最后

利用小卫星三轴气浮转台实验验证termianl滑模控制方法的实用性。实验显示:根据参数选取原则设定的参数进行小卫星机动稳定实验得到的姿态角和姿态角速度控制精度和稳态误差分别小于0.1°和0.01(°)/s

满足三轴气浮转台最佳控制精度。结果表明terminal滑模控制方法在小卫星机动稳定任务中具有很高的控制精度和稳定度

能够为小卫星成像任务稳定执行提供良好的基础。

Abstract

The attitude maneuver and stable task of a small satellite by using a Single Gimbal Control Moment Gyro(SGCMG) as an actuator was explored with the terminal sliding mode control method. Firstly

a small satellite mathematical model was established based on the Modified Rodrigues Parameters (MRP)

and the torque planning was made in the terminal sliding mode control method. Then

command torque was given through diagonal singular robust tracking control law using the SGCMG as an actuator. The performance of the control method was studied by mathematical simulation

and the changing law and chosen rule of design parameters of the terminal sliding mode control were presented. Finally

a small satellite three-axis air flotation turntable was used to verify the adaptability of terminal sliding mode control. The experimental results show that the attitude angle and attitude angular velocity control precision and steady state error is less than 0.1 ° and 0.01(°)/s

which is within the scope of the best control precision from the parameter selection principle in the three-axis air flotation turntable for small satellite maneuver stability experiment. It concludes that the terminal sliding mode control method has high control precision and stability and is able to give a good function for small satellite maneuvers.

关键词

Keywords

references

MAN Z H, PAPLINSKI A P, WU H R. A robust MIMO terminal sliding mode control scheme for rigid robot manipulators[J]. IEEE Transactions on Automatic Control, 1994, 39: 2464-2469.

穆朝絮,余星火,孙长银. 非奇异终端滑模控制系统相轨迹和暂态分析[J]. 自动化学报,2013,39(6): 902-908.

MU CH X, YU X H, SUN CH Y. Phase trajectory and transient analysis for nonsingular terminal sliding mode control systems [J]. Acta Automatica Sinica, 2013,39(6): 902-908.(in Chinese)

张巍巍,王京.基于指数趋近律的非奇异Terminal 滑模控制[J].控制与决策,2012, 27(6): 909-913.

ZHANG W W, WANG J.Nonsingular Terminal sliding model control based on exponential reaching law [J].Control and Decision, 2012, 27(6) : 909-913.(in Chinese)

张秀华,徐炳林,赵宇.有限时间收敛的Terminal滑模控制设计[J].控制工程,2008, 15(6): 637-639.

ZHANG X H, XU B L, ZHAO Y.Terminal sliding mode control design with finite-time convergence [J].Control Engineering of China, 2008, 15(6):637-639.(in Chinese)

张合新,范金锁,孟飞,等. 一种新型滑模控制双幂次趋近律[J]. 控制与决策,2013,28(2): 289-293.

ZHANG H X, FAN J S, MENG F, et al.. A new double power reaching law for sliding mode control[J]. Control and Decision, 2013,28(2): 289-293. (in Chinese)

王鹏,刘鲁华,吴杰.高超声速飞行器Terminal 滑模控制系统设计[J].航天控制,2012, 30(5): 9-14.

WANG P, LIU L H, WU J.The Terminal sliding mode control system design for hypersonic flight vehicle [J]. Aerospace Control, 2012, 30(5): 9-14.(in Chinese)

曾宪法,王小虎,张晶,等.高超声速飞行器的干扰补偿Terminal 滑模控制[J].北京航空航天大学学报,2012, 38(11): 1454-1458.

ZENG X F, WANG X H, ZHANG J, et al.. Disturbance compensated terminal sliding mode control for hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(11): 1454-1458.(in Chinese)

李迪,陈向坚,续志军. 增益自适应滑模控制器在微型飞行器飞行姿态控制中的应用[J]. 光学精密工程,2013,21(5): 1183-1191.

LI D, CHEN X J, XU ZH J. Gain adaptive sliding mode controller for flight attitude control of MAV[J]. Opt. Precision Eng., 2013,21(5): 1183-1191. (in Chinese)

蒲明,吴庆宪,姜长生,等.基于二阶动态Terminal滑模的近空间飞行器控制[J].宇航学报,2010, 31(4): 1056-1062.

PU M, WU Q X, JIANG CH SH, et al.. Near space vehicle control based on second-order dynamic Terminal sliding mode[J].Journal of Astronautic, 2010, 31(4) :1056-1062.(in Chinese)

SHUSTER M D. A survey of attitude representations [J]. The Journal of the Astronautical Sciences, 1993, 41(4): 439-517.

丛炳龙,刘向东,陈振. 刚体航天器姿态跟踪系统的自适应积分滑模控制[J]. 航空学报,2013,34(3): 620-628.

CONG B L, LIU X D, CHEN ZH. Adaptive integral sliding mode control for rigid spacecraft attitude tracking [J]. Acta Aeronautica et Astronautica Sinica, 2013,34(3): 620-628.(in Chinese)

庄开宇,张克勤,苏宏业,等.高阶非线性系统的Terminal滑模控制[J].浙江大学学报(工学版),2002, 36(5): 482-485.

ZHUANG K Y, ZHANG K Q, SU H Y, et al.. Terminal sliding mode control for high-order nonlinear dynamic systems[J]. Journal of Zhejiang University (Engineering Science), 2002, 36(5): 482-485.(in Chinese)

胡剑波,时满宏,庄开宇,等.一类非线性系统的Terminal滑模控制[J].控制理论与应用,2005, 22(3):495-499.

HU J B, SHI M H, ZHUANG K Y, et al..Terminal sliding mode control for a class of nonlinear systems[J]. Control Theory &Applications, 2005, 22(3): 495-499.(in Chinese)

HE J B, LI G J, CAO F X. Dynamic Terminal sliding mode control method based on backstepping design[J].International Conference on System Science, Engineering Design and Manufacturing Informatization, 2010,42-46.

郭益深,孙富春. 一类具有参数不确定n阶多输入多输出非线性系统的Terminal滑模控制[J]. 控制理论与应用,2013,30(3): 324-329.

GUO Y SH, SUN F CH. Terminal sliding-mode control for a class of nth-order multi-input multi-output nonlinear system with uncertain parameters[J]. Control Theory &Applications, 2013,30(3): 324-329.(in Chinese)

BONG W. New singularity escape/avoidance steering logic for control moment gyro systems[J]. Journal of Guidance, Control and Dynamics, 2005, 28(5):948-956.

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