兵工自动化2012，Vol.31Issue(5)：1-4,8,5.DOI:10.3969/j.issn.1006-1576.2012.05.001
基于动态逆的无人机飞行控制律设计
Design of UAV Maneuvering Control Law Based on Dynamic Inversion
李春涛 1胡盛华1
作者信息
- 1. 南京航空航天大学自动化学院,南京210016
- 折叠
摘要
Abstract
According to the properties such as nonlinear and coupling in UAV flight maneuver, the inner-loop consisted of pitch rate and roll rate controller based on dynamic inversion method is proposed. Directly calculate inversion model through mathematics analysis method to cancel the system nonlinearity and realize path coupling. Combination with the requirements of frequency and time domain, the normal acceleration and roll angle outer-loop controller is designed by root locus method. UVA nonlinear simulation results show that the roll angle based on dynamic inversion and time frequency quality of overload controller meets flight control requirements of UAV.关键词
动态逆/过载控制/无人机/控制律Key words
dynamic inversion/ overload control/ UAV/ control law分类
军事科技引用本文复制引用
李春涛,胡盛华..基于动态逆的无人机飞行控制律设计[J].兵工自动化,2012,31(5):1-4,8,5.
