釆用脉冲宽度调制驱动装置的反辐射导弹导引头随动系统设计

杨艳娟;金志华;田蔚风

兵工学报 ›› 2004, Vol. 25 ›› Issue (2) : 214-217.

兵工学报 ›› 2004, Vol. 25 ›› Issue (2) : 214-217. DOI: 10.3969/j.issn.1000-1093.2004.02.022
短文

釆用脉冲宽度调制驱动装置的反辐射导弹导引头随动系统设计

  • 杨艳娟,金志华,田蔚风
作者信息 +

Design of Anti-Radiation Missile Seeker Follow-Up System Driven by Pulse-Width Modulation

  • Yang Yanjuan ,Jin Zhihua, Tian Weifeng
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文章历史 +

摘要

本文简单介绍了现有两种反辐射导弹(ARM)导引头随动系统,液压伺服随动系统和电动平台随动系统。在综合二者优点的基础上,设计了一种性能更优的捷联反辐射导弹(ARM)导引头随动系统。它将惯性姿态测量元件与载体捷联安装,系统采用经典的比例积分微分(PID)控制,伺服机构采用脉冲宽度调制( PWM)驱动的直流力矩电机,引导规律为比例导引。文中详细分析了该种方案的主要性能和特点,仿真表明所设计系统具有良好的性能。

Abstract

Describes briefly two existing anti-radiation missile (ARM) seeker follow-up systems, viz. the hydraulic pressure servo ARM seeker follow-up system and eiectromotion ARM seeker follow-up system. On the basis of retaining their superiority, a new strapdown ARM seeker follow-up system with better per?formances was suggested. In this system the inertial measurement unit is fixed on the vehicle directly. It adopts the classical proportional integral differential control, witn its servomechanism adopting DC moment motor driven by pulse width modulation working on proportion guidance. The paper analyzed the perfor?mance and characteristics of the ARM seeker follow-up system in detail. Theoretical analysis and simulation show that the ARM seeker follow-up system inherits the excellence of the above two ARM seeker follow-up systems that the structure of the system is simple, and that the effect of the missile attitude movement to steady-state response of the ARM seeker follow-up system is eliminated with integral control. Simulation results also show that the designed system has good tracking performance.

关键词

自动控制技术 / 反辐射导弹 / 导引头 / 随动系统 / 比例积分微分控制

Key words

automatic control technique / anti-raidiation missile / seeker / follow-up system / proportion?al-integral-differential control

引用本文

导出引用
杨艳娟,金志华,田蔚风. 釆用脉冲宽度调制驱动装置的反辐射导弹导引头随动系统设计. 兵工学报. 2004, 25(2): 214-217 https://doi.org/10.3969/j.issn.1000-1093.2004.02.022
Yang Yanjuan ,Jin Zhihua, Tian Weifeng. Design of Anti-Radiation Missile Seeker Follow-Up System Driven by Pulse-Width Modulation. Acta Armamentarii. 2004, 25(2): 214-217 https://doi.org/10.3969/j.issn.1000-1093.2004.02.022

参考文献

[1] Nesline F, William J, Mark L N. An analysis of optimal command guidance vs. optimal semiactive homing missile guidance. In: Proc of Amerian Control Conference. Seattle: 1986.1105?1107
[2] Zarchan P. Tactical and strategic missile guidance. Wasmngton DC: AIAA Inc, 1994. 174?180
[3] 杨艳娟,马澍田,黄德鸣.双通道电动ARM导引头随动系统的设 计与分析.哈尔滨工程大学学报,2000,21(2) :85?87

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