Nonlinear Bank-to-Turn Autopilot Design for Hypersonic Gliding Vehicle

摘要：

This paper presents the design and simulation of a Bank-to-Turn (BTT) autopilot for a hypersonic gliding vehicle. Based on the two-time scale assumption, the flight control system is divided in to two loops: the dynamics of fast state (inner loop) and slow state (outer loop). Autopilot is designed for each loop. The method used to design the autopilot relies on trajectory linearization and is realized through two controller subdesigns. The first design problem involves finding a nonlinear dynamic inverse for the plant. The second design involves designing a trajectory stabilizing controller using a Parallel D-eigenvalue stability concept developed for linear time varying (LTV) systems. Finally, two simulations are given to test the autopilots performance.

关键词： Bank-to-Turn:Hypersonic Gliding Vehicle:Nonlinear Control:Trajectory Linearization Control

作者: Xiaoqing Chen Zhongxi Hou Jianxia Liu

作者单位: College of Aerospace and Material Engineering,NUDT,Changsha,Hunan 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: 1046-1051

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）