简谈中、小型制导弹药舵机的发展现状
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摘要
为实现常规武器的精确制导,依据中、小型制导弹药舵机的发展现状,对舵机系统进行探讨。阐述制导弹药舵机系统主要构成模块,介绍影响舵机在制导弹药制导过程中的因素,结合舵机的国内外发展现状,列举目前典型的舵机和相关参数,得出气动舵机和电动舵机的应用特点及发展趋势。应用结果表明,对弹载舵机在制导弹药领域的研究可以提高制导弹药的精确性。
In order to achieve the accurate guidance of conventional weapon, based on the development status of medium and small guided missile ammunition servo system, the servo system is discussed. Explained the main components of the guided missile servo system, introduced the factors that affect the servo in the guided missile manufacturing.Combine with the development status of the servo at home and abroad, enumerated the typical servos and related parameters, and obtained the application features and development trends of aerodynamic and electric servos. The application results showed that the research on the missile-borne servo in the field of guided missile can improve the accuracy of the guided missiles.
In order to achieve the accurate guidance of conventional weapon, based on the development status of medium and small guided missile ammunition servo system, the servo system is discussed. Explained the main components of the guided missile servo system, introduced the factors that affect the servo in the guided missile manufacturing.Combine with the development status of the servo at home and abroad, enumerated the typical servos and related parameters, and obtained the application features and development trends of aerodynamic and electric servos. The application results showed that the research on the missile-borne servo in the field of guided missile can improve the accuracy of the guided missiles.
引文
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[2]孟秀云.导弹制导与系统控制原理[M].北京:北京理工大学出版社, 2003:84.
[3]张国元.某型舵机改进设计及其仿真分析[D].哈尔滨:哈尔滨工业大学, 2016.
[4]冉红凯.某气动舵机改进设计与研究[D].南京:南京理工大学, 2012.
[5]温清波.滑阀式燃气舵机的仿真与研究[D].昆明:昆明理工大学, 2015.
[6]张爱军.一种筒弹状态下电动舵机自检方法[J].兵工自动, 2018, 37(12):9-11.
[6]王生明.制导炮弹电动舵机控制器设计与分析[D].南京:南京理工大学, 2010.
[7]张伟东.灵巧弹药舵机控制系统研究[D].南京:南京理工大学, 2006.
[8]张皎.制导炮弹可控滚转执行机构关键技术研究[D].北京:北京理工大学, 2015.
[9]苏享,桂成兵,周亚军.制导弹药舵机研究现状及其关键技术分析[J].飞航导弹, 2008(11):48-50.
[10]汪军林,解付强,刘玉浩.导弹电动舵机的研究现状及发展趋势[J].飞航导弹, 2008(3):42-46.