Application of Maximum Principle with Final State Constraints in Gliding Control for Guided Bombs
The optimal gliding control problem is studied for guided bombs.Optimal control theory is used to describe the characteristics of continuous variation in gliding control system for guided bombs.The optimal control model of guided bomb is built and solved using maximum principle with final state constraints and shooting method for boundary values.The shooting method is modified to meet desired performance index, final states and temporal constraints.An example for guided bomb optimal gliding is given to validate the effectiveness of proposed method.
guided bomb maximum principle optimal control costate vector shooting method for boundary value
Lina Geng Zhiqiang Zheng
College of Mechatronic Engineering and Automation National University of Defense Technology Changsha,Hunan Province,China
国际会议
2007 IEEE International Conference on Automation and Lofistics
山东济南
英文
2007-08-18（万方平台首次上网日期，不代表论文的发表时间）