Integrated Guidance and Control with Terminal Impact Angular Constraint for Bank to Turn Flight Vehicle

摘要：

　　An integrated guidance and control (IGC) method for bank to turn (BTT) flight vehicle with impact angle constraint is presented,using multiple sliding surface control theory.Based on missile-target engagement geometry model and BTT control mode,an IGC model is formulated.According to multiple sliding surfaces control theory,IGC laws are designed in pitch channel and roll-yaw channels respectively to satisfy miss distance and impact angle requirements.Numeric simulation results show that the aforementioned method can design IGC law for BTT missile effectively,the miss distance and impact angle constraints are satisfied properly.

关键词： Guidance Angular Constraints Bank to Turn Skip to Turn

作者: CHAO Tao WANG Songyan TIAN Guobing YANG Ming

作者单位: Control and Simulation Center,Harbin Institute of Technology,Harbin 150086,China

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 681-685

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）