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

作　　者：杨树兴[1] 

机构地区：[1]北京理工大学宇航学院,北京100081

出　　处：《兵工学报》2016年第7期1299-1305,共7页Acta Armamentarii

基　　金：国家自然科学基金项目(11532002)

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。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 War II are introduced intensively. The features of MLRS are summarized as well, in- cluding 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 con- trol, which should be focused on and solved in the future investigation, are proposed.

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 

分 类 号：TJ393[兵器科学与技术—火炮、自动武器与弹药工程]