智能系统学报2016，Vol.11Issue(6)：818-826,9.DOI:10.11992/tis.201611022
航天器绕飞逼近翻滚目标运动再现的姿轨控制
Attitude and orbit control of spacecrafts for motion reconstruction of flying around and approaching the tumbling target
摘要
Abstract
This paper deals with the attitude and orbit control problem for motion reconstruction of spacecrafts flying around and approaching the tumbling target during ground experiments.Firstly, a 6-DOF similarity model is established to describe the integrated attitude and orbit motion, which is suitable for the experimental verification with the practical constraints on the space size, running velocity and time involved.Secondly, the polynomial approach is used to design the motion reference trajectory that can ensure finite-time convergence and good dynamic performances, based on which, an integrated attitude and orbit control law is proposed by the back-stepping method and the corresponding closed-loop stability is proved.Finally, a numerical example is included to illustrate the effectiveness of the obtained results.关键词
运动再现/相似理论/绕飞/翻滚/姿轨控制/航天器Key words
motion reconstruction/similarity/flying around/tumbling/attitude and orbit control/spacecrafts分类
信息技术与安全科学引用本文复制引用
孙施浩,贾英民..航天器绕飞逼近翻滚目标运动再现的姿轨控制[J].智能系统学报,2016,11(6):818-826,9.基金项目
国家"973"计划项目(2012CB821200,2012CB821201) （2012CB821200,2012CB821201）
国家自然科学基金项目(61134005,61327807,61520106010). （61134005,61327807,61520106010）
