无动力升力体飞行器再入机动方案设计及仿真  

Design and Simulation of Reentry Maneuvering Scheme for No-power Lift-body Vehicle

作　　者：何念念[1] 王鹏[2] 马靖[1] 蒋斌[1] 

机构地区：[1]第二炮兵装备研究院 [2]中国人民解放军96161部队

出　　处：《四川兵工学报》2014年第5期33-35,50,共4页Journal of Sichuan Ordnance

摘　　要：针对无动力升力体飞行器特点,设计了其再入机动方案,包括余弦波形式侧向蛇形机动方案和改进的余弦波形式的纵向跳跃机动方案;并根据再入机动方案,对机动幅度、频率、方向的控制进行了仿真分析;仿真结果表明:设计的机动方案能够很好的实现纵向、侧向机动轨迹的控制。Aiming at no-power lift-body vehicle, the reentry maneuvering scheme was designed, including lateral snake-like scheme with cosine wave form and vertical jumping scheme with improved cosine wave form. Based on this reentry maneuvering scheme, the control of maneuvering latitude, frequency and di- rection were simulated and analyzed. Simulation results show that the maneuvering scheme designed in this paper can well realize the lateral and vertical maneuvering track control.

关 键 词：无动力升力体 再入机动 方案设计 仿真分析 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]