基于C*准则的最优控制灵敏度设计方法
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Sensitivity Design Method of Optimal Control Based on C* Criterion
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    摘要:

    为优化侧杆负载及控制灵敏度特性设计流程,提出一种基于C*准则的最优控制灵敏度设计方法。依托国 外相关经验,结合C*准则设计参数;介绍驾驶员人机工程学及侧杆性能对飞行体验的影响,引出侧杆最优力感特性 的设计方法,结合传统的飞行品质规范搭建人机闭环模型验证。实验结果表明:侧杆在不同速度下对纵向角速率和 过载控制权重不同,响应均满足C*准则的一级设计要求,仿真验证了侧杆参数和飞行品质结合优化的有效性。

    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.

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翟任庆.基于C*准则的最优控制灵敏度设计方法[J].,2024,43(07).

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  • 收稿日期:2024-03-15
  • 最后修改日期:2024-04-16
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  • 在线发布日期: 2024-07-08
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