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空天飞行器再入制导的预测控制
引用本文:方炜,姜长生,朱亮.空天飞行器再入制导的预测控制[J].宇航学报,2006,27(6):1216-1222.
作者姓名:方炜  姜长生  朱亮
作者单位:南京航空航天大学自动化学院,南京,210016
摘    要:研究了空天飞行器的再人制导预测律的设计问题。根据飞行器再人飞行所受的约束条件确定再人参考轨迹,设计非线性预测控制控制律使得飞行器跟踪参考轨迹,通过在性能指标中加入末端项,以及基于末端项设计局部非线性控制律来保证非线性预测控制律的稳定性。最后给出的仿真实例表明了本文所设计的控制律具有较好的跟踪性能。

关 键 词:再入  约束条件  性能指标  预测控制律
文章编号:1000-1328(2006)06-1216-07
收稿时间:11 22 2005 12:00AM
修稿时间:2005-11-222006-03-07

Design of an Predictive Control Law for Re-entry Aerospace Vehicle
FANG Wei,JIANG Chang-sheng,ZHU Liang.Design of an Predictive Control Law for Re-entry Aerospace Vehicle[J].Journal of Astronautics,2006,27(6):1216-1222.
Authors:FANG Wei  JIANG Chang-sheng  ZHU Liang
Institution:Department of Automatic Control Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:In this paper,the design of the aerospace vehicle's re-entry predictive/tracking law is considered,the reference trajectory of RLV is decided by the constraints,and tracked under the nonlinear predictive control law.The stability is guaranteed by adding a terminal-state penalty in the cost function and using a local terminal-state controller which is based on the terminal cost function.Results of the simulation indicate the acceptable performance of the designed law to track the reference trajectory.
Keywords:Re-entry  Constraints  Cost function  Predictive control law
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