Entry Guidance for Common Aero Vehicle

摘要：

Aiming at the Common Aero Vehicle (CAV) entry guidance problem under various trajectory constraints and terminal conditions, an on-board reference trajectory generation method was proposed, and then linear quadratic regulator (LQR) was designed to track the longitudinal reference trajectory. Lateral guidance was realized by using bank-reversal strategy with the aid of the azimuth error corridor. Finally, the entry trajectory was presented based on the above method.

作者: Zhou Wenya Chen Hongbo Yang Di

作者单位: Department of Astronautics,Harbin Institute of Technology,Harbin,150001,China China Academy of Launch Vehicle Technology,Beijing,100076,China

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 939-944

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）