变形翼舵技术在导弹领域的应用需求及技术发展路线  

The Application Requirements and Technological Development Route of Deformable Wing Rudder Technology in Missile Fields

作　　者：姚重阳[1,2] 王晓鹏[2] 张海瑞 雷豹[2] 夏艳 YAO Chongyang;WANG Xiaopeng;ZHANG Hairui;LEI Bao;XIA Yan(National Graduate College for Engineers,Tsinghua University,Beijing,100084;China Academy of Launch Vehicle Technology,Beijing,100076)

机构地区：[1]清华大学国家卓越工程师学院,北京100084 [2]中国运载火箭技术研究院,北京100076

出　　处：《导弹与航天运载技术（中英文）》2024年第3期9-13,28,共6页Missiles and Space Vehicles

基　　金：国家自然科学基金联合基金项目(U20B2028)。

摘　　要：采用变形翼舵技术可解决导弹对发射平台尺寸强约束问题,改善导弹升阻比及弹道末段机动性能,实现飞行全程气动外形最优,适应多任务作战需求。对国内外变形翼舵技术发展进行了概述,介绍了变形翼舵方案组成,分析了导弹对变形翼舵技术的需求,提出了单次阶跃变形、往复伸缩变形、柔性连续变形三阶段技术发展路线以及各阶段的关键技术,为变形翼舵技术在导弹武器领域的深入研究及应用提供了参考。The use of deformable wing rudder technology can solve the problem of strong constraints on the launch platform size of missiles,improve the lift to drag ratio and ballistic maneuverability of missiles,achieve optimal aerodynamic shape throughout the flight,and adapt to the needs of multi mission operations.The development of deformable wing rudder technology at home and abroad is summarized,the composition of deformable wing rudder scheme is briefly introduced.The missile's demand for deformable wing rudder technology is analyzed,and the development path of single step deformation,reciprocating expansion deformation,flexible continuous deformation and the key technologies of each stage are put forward.The research results provide a reference for the in-depth research and application of deformable wing rudder technology in the field of missile weapons.

关 键 词：变形翼舵 导弹 应用需求 发展路线 关键技术 

分 类 号：V19[航空宇航科学与技术—人机与环境工程]