Optimal Attack Guidance Algorithm for UAV with Net Information Support

摘要：

A new guidance algorithm with threat avoidance ability and missile launch restriction is proposed. Firstly, mathematic model of guidance is established based on relative velocity vector, second, path restriction model for threat avoidance and terminal restriction is given. Performance index is established based on guidance time as well as control energy;attack guidance is constructed as an optimal control model with nonlinear boundary restriction, state restriction and path restriction. Gauss Pseudospectral Method is adopted for model discretization and receding horizon control strategy is introduced for online optimization. Simulation result shows, this new guidance algorithm is effectively for threat avoidance and missile launch requirement could well satisfy at the endpoint.

关键词： guidance Algorithm threat avoidance optimal control path restriction Gauss Pseudospectral Method receding horizon control

作者: Zhaowang Fu Zhongliang Zhou Qingchun Kong Hongqiang Liu

作者单位: Engineering college Air Force Engineering University xian, China

会议类型: 国际会议

会议名称: 2012 Fifth International Symposium on Computational Intelligence and Design 第五届计算智能与设计国际会议 ISCID 2012

会议地点: 杭州

会议语种:英文

页码: 584-587

在线出版日期: 2012-10-28（万方平台首次上网日期，不代表论文的发表时间）