航天控制2024,Vol.42Issue(3) :48-53.

采用粒子群优化算法的三回路自动驾驶仪设计优化

Design Optimization of Three-Loop Autopilot with Particle Swarm Optimization

张明恩 李如飞
航天控制2024,Vol.42Issue(3) :48-53.

采用粒子群优化算法的三回路自动驾驶仪设计优化

Design Optimization of Three-Loop Autopilot with Particle Swarm Optimization

张明恩 1李如飞1
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作者信息

  • 1. 上海机电工程研究所,上海 201109
  • 折叠

摘要

提出了一种伪攻角三回路自动驾驶仪的设计方法,从控制系统的开环性能指标出发,在舵控处依次断开增稳回路和过载回路,建立开环参数与伪攻角三回路自动驾驶仪参数的关系式,并以开环性能参数为自变量,闭环性能参数为优化目标,设计粒子群算法结构与边界条件,实现伪攻角三回路自动驾驶仪的快速调参.仿真结果表明,本文提出的设计方法,可使伪攻角三回路自动驾驶仪获得良好的开环性能和闭环性能,具有一定的工程应用价值.

Abstract

A designed method is proposed in this paper for the parameter adjustment of three-loop autopilot with pseudo-angle.Ulteriorly,regarding the open-loop performances indexes of the control system,the sta-bilizing and the overload loops are successively disconnected at the rudder control,and the relationship is es-tablished between open-loop parameters and the three-loop autopilot parameters with pseudo-angle.Then,by taking the open-loop performance parameters as independent variable and the closed-loop performance pa-rameter as optimization goal,particle swarm optimization algorithm structure and boundary conditions are designed,and the quickly parameters adjustment of three-loop autopilot with pseudo-angle is realized.The simulation results show that good open and closed loop performance of three-loop autopilot can be achieved through the designed method based on particle swarm optimization.

关键词

三回路自动驾驶仪/开环分析/粒子群算法/参数优化

Key words

Three-loop autopilot/Open-loop Analysis/Particle Swarm Optimization/Parameter optimization

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基金项目

&&(4140503020350901020201)

出版年

2024
航天控制
北京航天自动控制研究所

航天控制

CSTPCD
影响因子:0.29
ISSN:1006-3242
参考文献量6
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