陆军多管火箭武器的发展与思考

doi:10.3969/j.issn.1000-1093.2016.07.019

兵工学报 ›› 2016, Vol. 37 ›› Issue (7): 1299-1305.doi: 10.3969/j.issn.1000-1093.2016.07.019

陆军多管火箭武器的发展与思考

杨树兴

(北京理工大学宇航学院北京 100081)

收稿日期:2016-06-22 修回日期:2016-06-22 上线日期:2016-09-05
作者简介:杨树兴(1962—)，男，教授，博士生导师
基金资助:
国家自然科学基金项目（11532002）

Progress and Key Points for Guidance of Multiple Launch Rocket Systems

YANG Shu-xing

（School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China)

Received:2016-06-22 Revised:2016-06-22 Online:2016-09-05

摘要/Abstract

摘要： 论述了陆军多管火箭武器的发展进程，重点介绍其在第二次世界大战以来所走过的增大射程、提高射击密集度和实现制导化3个主要发展阶段。归纳总结了陆军多管火箭武器在发展过程中形成的多联装发射平台、弹体采用旋转体制、大长径比、短时大推力发动机和曲射弹道、静稳定设计等特点，分析上述特点对其制导化发展中带来的优势和挑战，提出陆军多管火管武器未来发展中应重点关注和解决的若干问题：旋转弹捷联惯性导航、动态稳定性理论、弹道规划与控制方法、大推力比长工作时间的先进动力、单线制发射控制技术等。

关键词: 兵器科学与技术, 多管火箭武器系统, 火箭弹, 制导化, 惯性导航, 稳定性, 控制系统, 火箭发动机

Abstract: The development process of multiple launch rocket systems (MLRSs) is reviewed, and the three development phases of extended range, improved firing dispersion and guidance implementation of MLRS since World WarⅡ are introduced intensively. The features of MLRS are summarized as well, including multiple launch tubes, spinning of projectile body, large length-diameter ratio, short-time and high thrust motor , curved trajectory and static stability design. The advantages and challenges for guided rocket projectiles are discussed. Several issues, such as strapdowninertia navigation, dynamic stability, trajectory programming and control, advanced solid rocket motor and single conductor wire launch control, which should be focused on and solved in the future investigation, are proposed.

Key words: ordnance science and technology, multiple launch rokect system, rocket, guidance, inertial navigation, stability, control system, rocket motor

中图分类号:

TJ393

杨树兴. 陆军多管火箭武器的发展与思考[J]. 兵工学报, 2016, 37(7): 1299-1305.

YANG Shu-xing. Progress and Key Points for Guidance of Multiple Launch Rocket Systems[J]. Acta Armamentarii, 2016, 37(7): 1299-1305.

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陆军多管火箭武器的发展与思考

Progress and Key Points for Guidance of Multiple Launch Rocket Systems

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