航空兵器Issue(4)：30-35,6.DOI:10.19297/j.cnki.41-1228/tj.2016.04.005
基于前馈补偿的直升机控制律设计与仿真
Helicopter Control Law Design and Simulation Based on Feed-Forward Compensation
刘宇亮 1张琳 1朱亚芬1
作者信息
- 1. 中国空空导弹研究院，河南洛阳 471009
- 折叠
摘要
Abstract
Taking a transport helicopter as the research subject , based on stability augmentation con-trol , feed-forward compensation control law is designed to improve the control system according to the fly-ing qualities specification of ADS -33 E.By fitting the feed-forward control parameters of different flight nodes, parameter adjusting control law in the full scale flight envelop can be realized .The designed sys-tem is simulated and tested , and the results indicate that satisfied control effect is obtained by adopting the proposed control method , which proves the feasibility and effectiveness of the method .关键词
直升机/飞行品质规范/前馈补偿/控制律/系统仿真Key words
helicopter/flying qualities specification/feed-forward compensation/control law/sys-tem simulation分类
航空航天引用本文复制引用
刘宇亮,张琳,朱亚芬..基于前馈补偿的直升机控制律设计与仿真[J].航空兵器,2016,(4):30-35,6.
