舰载制导火箭弹总体技术的若干问题探讨  

Discussion on Several Issues of Shipborne Guided Rocket Overall Technology

作　　者：欧阳福蕾 李磊[1] 郭洪波[1] 龚春林[2] Ouyang Fu lei;Li Lei;Guo Hongbo;Gong Chunlin(Beijing Institute of Space Long March Vehicle,Beijing 100076,China;School of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China)

机构地区：[1]北京航天长征飞行器研究所,北京100076 [2]西北工业大学航天学院,西安710072

出　　处：《战术导弹技术》2021年第1期1-6,共6页Tactical Missile Technology

摘　　要：针对舰载制导火箭弹相关研究的发展情况,结合近年来总体技术领域的文献,探讨了飞行弹道中的若干关键技术,明确了初始段弹道的发射方式、发射精度影响因素、垂直转弯控制方式的主要特点,分析了滑翔段弹道的滑翔增程技术和控制方法的相关问题、主要方法和研究进展,综述了攻击段弹道的制导方法和具有末端约束的末制导方法,提出了多学科交叉发展的建议,为舰载制导火箭弹的工程应用提供理论参考。In view of the development of related research on shipborne guided rockets, combined with the literature in the overall technical field in recent years, several key technologies in flight trajectory are discussed. The main characteristics of the launch method, launch accuracy factors, and vertical turn control methods of the initial stage ballistic are clarified. The related issues, main methods and research progress of the glide extended range technology and control method of the glide ballistics are analyzed. The guidance method and the terminal guidance method with end restraint of the attack phase ballistics are reviewed. Proposals for interdisciplinary development are put forward. A theoretical reference for the engineering application of shipborne guided rockets is provided.

关 键 词：舰载制导火箭弹 总体技术 弹道 垂直转弯控制 

分 类 号：TJ762.3[兵器科学与技术—武器系统与运用工程]