国防科技大学学报2017，Vol.39Issue(1)：51-57,7.DOI:10.11887/j.cn.201701009
伺服机构故障下基于线性规划的运载火箭姿控系统重构控制
Reconstruction of attitude control system of launch vehicle based on linear programming under servo mechanism fault
摘要
Abstract
Servo mechanism fault of engine brings challenge to the reliability and safety of attitude control system for the new generation launch vehicle, a research on control reconstruction strategy is needed urgently.Aiming at this problem, a control allocation method for the deflection angle reconstruction was proposed.The problem of deflection angle allocation under servo mechanism fault was transformed into the problem of 1-norm single objective constrained optimization, and then it was translated into the standardized linear programming model solved by simplex algorithm finally.Simulation results show that the attitude control system can be completely reconstructed by the proposed method under servo mechanism fault, each deflection angle does not reach its saturation value, so the validity of the method is proved.关键词
运载火箭/姿态控制/控制分配/线性规划/单纯形法Key words
launch vehicle/attitude control/control allocation/linear programming/simplex algorithm分类
信息技术与安全科学引用本文复制引用
程堂明,李家文,唐国金..伺服机构故障下基于线性规划的运载火箭姿控系统重构控制[J].国防科技大学学报,2017,39(1):51-57,7.基金项目
装备预先研究资助项目(51320120111) （51320120111）
