南京航空航天大学学报（英文版）2021，Vol.38Issue(2)：237-248,12.
基于二阶锥优化的饱和及禁区约束下的航天器姿态控制
Spacecraft Attitude Control with Saturation and Attitude Forbidden Constraints via Second-Order Cone Programming
摘要
Abstract
This paper investigates the optimal control problem of spacecraft reorientation subject to attitude forbiddenconstraints,angular velocity saturation and actuator saturation simultaneously. A second-order cone programming (SOCP) technology is developed to solve the strong nonlinear and non-convex control problem in real time. Specifically,the nonlinear attitude kinematic and dynamic are transformed and relaxed to a standard affine system, and linearization and L1 penalty technique are adopted to convexify non-convex inequality constraints. With the proposed quadratic performance index of angular velocity,the optimal control solution is obtained with high accuracy using the successive SOCP algorithm. Finally,the effectiveness of the algorithm is validated by numerical simulation.关键词
航天器姿态机动/姿态禁区约束/执行机构饱和/角速度饱和/二阶锥优化Key words
spacecraft reorientation/attitude forbidden constraints/actuator saturation/velocity saturation/second-order cone programming(SOCP)分类
信息技术与安全科学引用本文复制引用
陈曦,曹瑞浩,胡庆雷..基于二阶锥优化的饱和及禁区约束下的航天器姿态控制[J].南京航空航天大学学报（英文版）,2021,38(2):237-248,12.基金项目
This work was supported by the Na-tional Natural Science Foundation of China(Nos.61960206011,61633003),the Beijing Natural Science Foundation(No.JQ19017).The authors would like to ac-knowledge the following people for their assistance:YAO Junyu,YANG Haoyang,CHEN Wei,SHI Yongxia,LIU Yueyang,all with the School of Automation Science and Electrical Engineering,Beihang University. （Nos.61960206011,61633003）
