南京航空航天大学学报2001，Vol.33Issue(2)：122-125,4.
综合TF/TA飞行的航迹控制与仿真
Control and Simulation of Integrated TF/TA Flight Path Tracking
徐克虎 1沈春林 1李宝莉 2冯根生2
作者信息
- 1. 南京航空航天大学自动化学院
- 2. 蚌埠坦克学院
- 折叠
摘要
Abstract
In the process of low altitude penetration, the algorithm for effective flight track control can guarantee to successfully complete the mission of terrain follow and terrain avoid. Due to the fact that the aircraft has to do some movements of great mobility, and there are severe couplings between the vertical and landscape orientation, the general algorithms are inapplicable in the synthesis flight procession. This paper presents six-freedom aircraft state equations as two subsystems of the related-large system consisted of coupling vertical and landscape orientation subsystem. Some assumptions are made when the coupling of vertical and horizontal is considered as a portion of exterior control input. Using large system variable structure control theory, independent vertical and horizontal orientation path control
laws are derived. The method reduces the difficulty of theory study and engineering realization. Simulational results show the above theory is feasible.
关键词
轨迹跟踪/变结构控制/耦合系统/仿真分类
航空航天引用本文复制引用
徐克虎,沈春林,李宝莉,冯根生..综合TF/TA飞行的航迹控制与仿真[J].南京航空航天大学学报,2001,33(2):122-125,4.
