一种无人系统姿态控制PID参数整定动态多目标优化方法

By constructing a dynamic model and multidimensional variable optimization space for unmanned systems, and combining it with a dynamic multi-objective optimization algorithm based on kernel mean matching, the problems of overshoot, settling time, and control error in the dynamic attitude control of unmanned systems are solved. This achieves efficient PID parameter tuning and meets the optimization requirements in dynamic environments.

CN116774573BActive Publication Date: 2026-07-17XIAMEN UNIV

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
XIAMEN UNIV
Filing Date
2023-07-13
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies in the dynamic attitude control of unmanned systems cannot simultaneously meet the requirements of small maximum overshoot, short settling time, and small absolute control error, and the control process is lengthy and ineffective in dynamic environments.

Method used

An optimization space is constructed based on the dynamic model of the unmanned system, and a multi-dimensional variable optimization objective function is built. A dynamic multi-objective optimization algorithm based on kernel mean matching is used, and PID parameters are tuned through matrix description method. Combined with environmental detection and scoring selection mechanism, highly adaptable individuals are selected for transfer learning to optimize and solve the PID control parameters.

Benefits of technology

It accelerates the optimization speed of multi-objective optimization algorithms in dynamic environments, improves the efficiency of attitude control of unmanned systems, meets the optimization objectives under different time scales, and achieves control effects with small overshoot, short settling time and small control error.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN116774573B_ABST
    Figure CN116774573B_ABST
Patent Text Reader

Abstract

本发明公开了一种无人系统姿态控制PID参数整定动态多目标优化方法,包括:S1,构建优化空间;S2,构建优化目标函数模型;S3,采用基于核均值匹配的动态多目标优化算法进行优化求解,得到不同时刻对应的PID控制参数;S4,根据得到的PID控制参数构建解空间,获得最终优化结果。本发明根据动力学模型分析和动态传递函数,通过矩阵描述的方法对无人系统刚体姿态进行描述,建立控制模型;利用基于核均值匹配的新型动态多目标优化算法进行求解,在不同时刻对PID参数进行动态优化,使得无人系统在动态姿态控制中满足最大超调量小、稳定时间短或绝对控制误差值小的要求。
Need to check novelty before this filing date? Find Prior Art