BTT 控制弹体线性模型及传函推导

张頔; 林德福; 崔晓曦; 徐平

doi:10.15892/j.cnki.djzdxb.2013.06.022

弹箭与制导学报 >

2013 , Vol. 33 >Issue 6: 34 - 37

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2013.06.022

导弹与制导技术

BTT 控制弹体线性模型及传函推导

张頔 ,
林德福 ,
崔晓曦 ,
徐平

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1 北京理工大学宇航学院,北京 100081
2 中国兵器工业导航与控制技术研究所,北京 100089
3 北京航天自动控制研究所,北京 100854

张頔(1989-),女,黑龙江哈尔滨人,硕士研究生,研究方向:飞行器总体设计、制导与控制。

收稿日期: 2013-03-18

网络出版日期: 2025-05-26

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Linear Model and Transfer Function of Bank-to-turn Missile

ZHANG Di ,
LIN Defu ,
CUI Xiaoxi ,
XU Ping

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1 School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
2 China Weapon Industry Navigation and Control Technology Reserach Institute, Beijing 100089, China
3 Benjing Aerospace Automatic Control Institute, Benjing 100854, China

Received date: 2013-03-18

Online published: 2025-05-26

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摘要

利用状态空间与传递函数关系,推导偏航-滚转通道耦合传递函数表达式。基于倾斜转弯导弹的运动学和动力学特性,建立倾斜转弯导弹的弹体模型,根据弹体耦合特点进行解耦分析。通过MATLAB符号推导功能和引入算例进行数值求解两种方法,对比验证传递函数正确性。以单位阶跃响应为输入进行仿真,仿真结果表明传递函数表达式正确,为以后的控制系统设计提供便利。

关键词： 倾斜转弯导弹; 线性模型; 传递函数; MATLAB

本文引用格式

张頔 , 林德福 , 崔晓曦 , 徐平 . BTT 控制弹体线性模型及传函推导[J]. 弹箭与制导学报, 2013 , 33(6) : 34 -37 . DOI: 10.15892/j.cnki.djzdxb.2013.06.022

Abstract

According to the relation between state space expression and transfer function, the transfer functions of roll/yaw channel were derived. According to the kinematics and dynamics characters of bank-to-turn missile, the mathematical model of bank-to-turn missile was build, and the coupling model was decoupled. There are two ways to verify the validity of the transfer functions, one is derived by state space in MATLAB, the other is the numerical model which is used to simulate by taking the unit step as input. Simulation results show that the transfer functions are valid and useful for control system design in the future.

Key words： bank-to-turn missile; linear model; transfer function; MATLAB

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