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采用终端滑模控制实现交会对接逼近段姿态跟踪
引用本文:刘鲁华,汤国建,余梦伦. 采用终端滑模控制实现交会对接逼近段姿态跟踪[J]. 国防科技大学学报, 2008, 30(2): 16-21
作者姓名:刘鲁华  汤国建  余梦伦
作者单位:国防科技大学,航天与材料工程学院,湖南,长沙,410073;中国运载火箭技术研究院,北京,100076
摘    要:针对交会对接逼近段追踪器的姿态控制问题,采用反馈线性化理论推导了非线性姿态动力学方程的相变量模型.基于导出的姿控模型,引入模型误差和随机噪声,结合终端滑模控制理论,给出了能够在有限时间内完成姿态跟踪,并使状态跟踪误差收敛的控制律的设计方法.对具有扰动项的系统,仿真结果仍能满足交会任务对时间的要求,且姿态角跟踪误差趋于0,说明控制律对相变量系统的姿态跟踪控制具有较好的鲁棒性.

关 键 词:交会对接  非线性  姿态控制  微分几何  终端滑模控制
文章编号:1001-2486(2008)02-0016-06
收稿时间:2007-08-17
修稿时间:2007-08-17

Space RVD Terminal Approach to Attitude Tracking by Terminal Sliding Mode Control
LIU Luhu,TANG Guojian and YU Menglun. Space RVD Terminal Approach to Attitude Tracking by Terminal Sliding Mode Control[J]. Journal of National University of Defense Technology, 2008, 30(2): 16-21
Authors:LIU Luhu  TANG Guojian  YU Menglun
Affiliation:LIU Lu-hua1,TANG Guo-jian1,YU Meng-lun2(1.College of Aerospace , Material Engineering,National Univ.of Defense Technology,Changsha 410073,China,2.China Academics of Launch Vehicle Technology,Beijing 100076,China)
Abstract:For the attitude control problem of terminal approach phase of RVD,the feedback linear theory was adopted to linearize nonlinear attitude dynamics,and a phase-variable states space model was deduced.The terminal sliding mode control theory considering the disturbances was used on the basis of the deduced model.Furthermore,this paper introduces a controller which implements the attitude tracking and controls the states tracking errors convergent to zero in the finite time.For the example given,the control re...
Keywords:rendezvous and docking(RVD)  nonlinear  attitude control  geometric theory  terminal sliding mode control  
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