摘要
简述了结构调控技术在导弹不同飞行阶段中实现可靠飞行的基本工作原理和实现该技术对导弹制导控制系统的基本要求,以美军远程光纤制导导弹为例具体阐述了该技术的优点——实现初始段加速、减速搜索目标、末制导段加速、增大射程和提高对机动目标的打击能力。
The principles for regulation and control technology of structure, realized in different flight stages of missile, and the requirements for missile＇s guidance and control system are introduced. The merits of this technology by analyzing remote fibre optic guidance missile for US Army is also expatiated, which can realize accelerated flight during initial stage, decelerated searching target, accelerated fight during final guidance segment, augmented range and enhanced aggressive capacity to mobile target.
出处
《导弹与航天运载技术》
北大核心
2008年第2期4-6,12,共4页
Missiles and Space Vehicles
关键词
结构调控技术
远程光纤制导导弹
指挥控制系统
飞行弹道
Regulation and control technology of structure
Remote fibre optic guidance missile
Guidance and control system
Flight trajectory
