基于有限时间收敛干扰观测器的探导控一体化设计

doi:10.12305/j.issn.1001-506X.2021.05.21

系统工程与电子技术 ›› 2021, Vol. 43 ›› Issue (5): 1326-1334.doi: 10.12305/j.issn.1001-506X.2021.05.21

基于有限时间收敛干扰观测器的探导控一体化设计

张跃坤^1,*(), 贾晓洪¹(), 张晓阳¹(), 王炜强^1,²()

1. 中国空空导弹研究院, 河南洛阳 471009
2. 航空制导武器航空科技重点实验室, 河南洛阳 471009

收稿日期:2020-07-15 出版日期:2021-05-01 发布日期:2021-04-27
通讯作者: 张跃坤 E-mail:2432877604@qq.com;jia_xh@139.com;fieldzhang@tom.com;alecwong@zju.edu.cn
作者简介:张跃坤(1993—), 男, 博士研究生, 主要研究方向为红外成像制导, 导航、制导与控制。E-mail: 2432877604@qq.com|贾晓洪(1968—), 男, 研究员, 博士, 主要研究方向为红外成像制导, 导航、制导与控制。E-mail: jia_xh@139.com|张晓阳(1975—), 男, 高级工程师, 博士, 主要研究方向为红外图像处理、红外导引头总体。E-mail: fieldzhang@tom.com|王炜强(1985—), 男, 工程师, 博士, 主要研究方向为红外图像处理、红外导引头总体。E-mail: alecwong@zju.edu.cn
基金资助:
国家安全重大基础科研计划(973计划)(6132710302)

Integrated design of detection guidance and control based on finite time disturbance observer

Yuekun ZHANG^1,*(), Xiaohong JIA¹(), Xiaoyang ZHANG¹(), Weiqiang WANG^1,²()

1. China Airborne Missile Academy, Luoyang 471009, China
2. Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons, Luoyang 471009, China

Received:2020-07-15 Online:2021-05-01 Published:2021-04-27
Contact: Yuekun ZHANG E-mail:2432877604@qq.com;jia_xh@139.com;fieldzhang@tom.com;alecwong@zju.edu.cn

摘要/Abstract

摘要：

针对滚仰式半捷联寻的制导导弹, 提出一种基于有限时间干扰观测器(finite time disturbance observer, FTDO)的探导控一体化滑模控制器设计方法。首先基于滚仰式半捷联导引头动力学模型和导弹制导控制模型, 建立了全状态耦合探测、制导、控制一体化控制模型。在模型中将不确定项和误差视为干扰, 通过有限时间收敛干扰观测器对干扰进行估计。对探导控一体化模型进行分块反演滑模控制律设计, 并验证了控制器的稳定性。仿真结果表明, 一体化控制方法提高了导弹对目标机动的响应能力和目标跟踪的稳定性, 并实现了比传统级联控制方法更小的脱靶量。

关键词: 干扰观测器, 滑模控制, 探导控一体化, 滚仰, 半捷联

Abstract:

Aiming at the roll-pitch semi strapdown homing missile, a sliding mode controller for integrated design of detection guidance and control based on finite time disturbance observer (FTDO) is proposed. Firstly, based on the dynamic model of roll-pitch semi strapdown seeker and guidance and control model of the missile, the whole state coupling integrated control model of detection guidance and control is established. In the model, the uncertainty and error are regarded as disturbance, and the disturbance is estimated by finite time disturbance observer. The block backstepping sliding mode control law is designed for the integrated model of detection guidance and control, and the stability of controller is verified. Simulation results show that the integrated control method improves the response ability of missile to target maneuver and the stability of target tracking, which achieves a smaller miss distance than the traditional cascade control method.

Key words: disturbance observer, sliding mode control, integrated detection guidance and control, roll-pitch, semi stapdown

中图分类号:

TP273
TJ765

张跃坤, 贾晓洪, 张晓阳, 王炜强. 基于有限时间收敛干扰观测器的探导控一体化设计[J]. 系统工程与电子技术, 2021, 43(5): 1326-1334.

Yuekun ZHANG, Xiaohong JIA, Xiaoyang ZHANG, Weiqiang WANG. Integrated design of detection guidance and control based on finite time disturbance observer[J]. Systems Engineering and Electronics, 2021, 43(5): 1326-1334.

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仿真条件	设置数值
导弹速度/(m/s)	800
导弹弹道倾角/(°)	5
导弹弹道偏角/(°)	0
弹体俯仰角/(°)	0
弹体偏航角/(°)	0
弹体滚转角/(°)	0
导弹攻角/(°)	5
导弹侧滑角/(°)	0
目标速度/(m/s)	400
目标弹道倾角/(°)	180
目标弹道偏角/(°)	0
相对距离/km	10
视线倾角/(°)	5
视线偏角/(°)	0
目标机动	幅值为3g的方波机动

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基于有限时间收敛干扰观测器的探导控一体化设计

Integrated design of detection guidance and control based on finite time disturbance observer

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