Coefficient Diagram Robust Control Design for Air-to-Air Missile

doi:10.7652/xjtuxb201311013

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Coefficient Diagram Robust Control Design for Air-to-Air Missile

更新时间：2025-07-09

- Coefficient Diagram Robust Control Design for Air-to-Air Missile
- Vol. 47, Issue 11, Pages: 70-75(2013)
- 作者机构：
  
  西安交通大学机械工程学院,西安,710049
- 作者简介：
- 基金信息：
- DOI：10.7652/xjtuxb201311013
  CLC： TP273
- Online First：10 November 2013，
  
  Published：2013
- 稿件说明：
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Coefficient Diagram Robust Control Design for Air-to-Air Missile[J]. 2013, 47(11): 70-75.
DOI：

Coefficient Diagram Robust Control Design for Air-to-Air Missile[J]. 2013, 47(11): 70-75. DOI： 10.7652/xjtuxb201311013.

摘要

针对空空导弹飞行控制系统中存在的弹体强非线性、参数不确定等问题

提出一种依据系数图鲁棒控制原理和导弹动力学特性的多项式结构空空导弹控制器设计方法。通过导弹系数图分析

获得等效时间常数、稳定性指数和裕度等对控制系统特性的影响参数。采用综合时域响应快速性和频域稳定裕度性能构建评价适应度函数

通过遗传算法优化流程对控制器参数进行优化

使优化后的控制系统得到更好的综合性能。不同特征点模型的仿真实验结果表明

所设计的控制器能够获得更好的响应特性和参数鲁棒性

且控制系统结构简单、易于工程实现。

Abstract

Aiming at the strong nonlinearity and uncertain parameters in flight control of air-to-air missile

a robust controller with coefficient diagram method(CDM)is designed according to the CDM essentiality and dynamic characteristics of air-to-air missiles. The effects of equivalent time constant

stability index and stability limit on the controller designed by CDM standard form is obtained via missile coefficient diagram analysis. The comprehensive evaluation index from response rate in time domain and stability margin in frequency domain is established

and genetic algorithm is chosen to optimize the control parameters. Simulation for various fixed point models verifies that the proposed controller possesses fine response and robust performance in controlling an air-to-air missile

and the control system with simple structure is prone to implementation.

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references

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