大空域机动滑翔弹控制方案研究  

Study on the Engineering Application of Bank-to-Turn Technology

作　　者：宋锦[1] 

机构地区：[1]海军装备部驻天津地区军事代表局,北京100076

出　　处：《战术导弹技术》2012年第3期98-102,共5页Tactical Missile Technology

摘　　要：针对导弹大空域作战大机动、高过载的要求,对BTT控制技术的工程化进行了研究,提出了BTT制导方案和姿态控制方案:在导弹初始调姿段采用STT控制方式,在导引飞行段采用BTT控制方式的BTT/STT混合控制模式,并开展了工程化设计工作;以某滑翔弹为例,开展了六自由度仿真试验。仿真试验结果验证了设计方案的可行性,BTT/STT混合控制模式能够发挥两种控制方式的优点,并可实现切换过程的姿态稳定性。采用该方案的滑翔弹可以适应不同的射程范围,具有较强的弹道机动能力。In order to meet the requirements of missile maneuverability and high overload in large airspace combat, the BTT control technology engineering were studied, BTT guidance scheme and the attitude control scheme are put forward. The STr control mode is adopted in the initial missile posture adjusting section, BTT / STT hybrid control mode of BTT control mode is adopted in guiding flight machine, and the engineering design work is carried out. Simulation test in six degree of freedom is carried out based on a gliding missile. The results prove the feasibility of the design scheme, BTT / STT hybrid control modes can play two ways to control, and the switching process stability can be realized. The glide missile using the scheme can be adapted to different range, strong maneuver capability.

关 键 词：倾斜转弯 大空域机动 姿态控制 混合控制 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计] TJ765[兵器科学与技术—武器系统与运用工程]