Integer Programming Based Optimal Side Jets Ignition Combination for Advanced Missile Attitude Control
The ignition logic of Reaction Control System(RCS)is one of the core issues of the precision and blended control combined aerodynamic force and reaction force of the advanced guided weapons.Firstly,a side-jet model based on the American Patriot Advanced Capability-3(PAC-3)missile was established,and a calculation method based on the equivalent forces,which convert the positional deviation of the thrusters to the deviation of the equivalent forces,was proposed.Considering the side-jets constraint,the ignition logic is transformed into a mathematical problem based on 0-1 integer programming.To deal with the high complexity of traditional algorithms for 0-1 integer programming model,restrictions of the thruster efficiency,was introduced to reduce the complexity of the algorithm and the computation time.Finally,simulation results indicate that this algorithm can satisfy the requirement and find out a better solution.
Integer Programming Blended Control Reaction Control System (RCS) Ignition Logic
Wang Zhenchao Yang Lingyu Zhang Jing Shen Gongzhang
School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191
国际会议
长沙
英文
3755-3759
2014-05-31（万方平台首次上网日期，不代表论文的发表时间）