兵工自动化2024，Vol.43Issue(7)：60-64,68,6.DOI:10.7690/bgzdh.2024.07.013
基于C*准则的最优控制灵敏度设计方法
Sensitivity Design Method of Optimal Control Based on C* Criterion
翟任庆1
作者信息
- 1. 航空工业西安飞行自动控制研究所,西安 710065
- 折叠
摘要
Abstract
In order to optimize the design flow of side link load and control sensitivity characteristics,an optimal control sensitivity design method based on C* criterion is proposed. Based on foreign experience,the parameters were designed according to C* criterion. The influence of pilot ergonomics and side stick performance on flight experience was introduced,and the design method of side stick optimal force feeling characteristics was introduced. Combined with the traditional flying quality specification,the closed-loop model of pilot and pilot was built for verification. The experimental results show that the side stick has different weights of longitudinal angular rate and overload control at different speeds,and the response meets the first-level design requirements of the C* criterion. The simulation verifies the effectiveness of the combined optimization of side stick parameters and flying qualities.关键词
人机工程学/力感特性/控制灵敏度/仿真验证/C*准则Key words
ergonomics/force feeling characteristics/control sensitivity/simulation verification/C* criterion分类
航空航天引用本文复制引用
翟任庆..基于C*准则的最优控制灵敏度设计方法[J].兵工自动化,2024,43(7):60-64,68,6.
