Study on Guidance Approaches of Hypersonic Glide-Cruise Vehicle during Cruise and Attack Phases

摘要：

Hypersonic glide-cruise vehicle is a new concept craft which glides with hypersonic velocity, and can cruise at a constant height apart from the ground recur to the engine. In the paper two guidance approaches of this craft are studied during cruise and attack phases respectively. Based on the established dynamics model, a novel guidance approach for cruise state holding and bank-to-turn control when passing through the waypoints is proposed. The optimal transformative proportion guidance law is adopted during the attack phase. The approaches studied are validated with a three-dimension simulation programme, and all war indexes requirements are meet.

作者: Xu Mingliang Liu Luhua Tang Guojian Chen Kejun

作者单位: College of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410073,China

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 1478-1482

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）