南京航空航天大学学报2001，Vol.33Issue(1)：73-77,5.
非线性逆在ASTOVL控制系统中的应用
Application of Non-Linear Inversion for ASTOVL Control System
王健 1王家钦 1赵雁南 1郭锁凤2
作者信息
- 1. 清华大学
- 2. 南京航空航天大学自动化学院
- 折叠
摘要
Abstract
The control law of flight/propulsion control system for advanced short takeoff and vertical landing(ASTOVL) is researched.During the flight from cruising to hovering,based on comprehending and grasping the fighter mathematical model under the control of aerodynamics and thrust vector,the theory of nonlinear dynamic inversion is successfully applied to design a thrust vector controller and a pitching controller.In this case,the force and the moment on the aircraft are reasonably distributed.And the three axis of pitching,longitudinal and normal are made to be linearized and uncoupled approximatively in the performance envelope of the propulsion system.Finally,the digital simulation results for ASTOVL during hovering show that the two controllers designed in the papers are very feasible and the designing aim is basically achieved.关键词
垂直短距起落飞机/推力矢量控制系统/非线性变换/动态逆分类
信息技术与安全科学引用本文复制引用
王健,王家钦,赵雁南,郭锁凤..非线性逆在ASTOVL控制系统中的应用[J].南京航空航天大学学报,2001,33(1):73-77,5.
