基于时至时的三维多导弹时空合作指导法:用于操控目标拦截的新方法
Yiao Zhan1, Siyuan Li1, Di Zhou1
1School of Astronautics, Harbin Institute of Technology, Harbin 150001, China.
ISA transactions
|May 7, 2024
概括
本研究介绍了基于时间到目标的多导弹指导,用于同时拦截机动目标. 这种新的方法通过协调不同角度的导弹攻击来最大限度地损害,同时优化燃料消耗.
科学领域:
- 航空航天工程 航空航天工程
- 控制系统 控制系统
- 导航,导航和控制系统 (GNC) 是指导,导航和控制系统.
背景情况:
- 对多枚导弹的合作指导对于接触机动目标至关重要.
- 现有的方法可能无法充分解决从不同角度同时拦截或优化燃料效率的问题.
研究的目的:
- 开发一种新的基于时间到目标的多导弹空间-时间合作指导方法.
- 为了使不同终端角度同时拦截机动目标,以最大限度地损坏.
- 为了优化导弹发动机负载和燃料消耗在视线 (LOS) 方向.
主要方法:
- 引入有限时间最佳合作指导技术.
- 由剩余飞行时间进行参数化的时间变化的滑动模式指导方案的建议.
- 将该方案应用于纵向和横向LOS方向,以管理加速度并满足交叉角度约束.
主要成果:
- 拟议的时间变化的合作指导法方便在终端时刻以不同的拦截角度同时拦截.
- 数字模拟证实了多导弹时空合作指导方法的有效性,优越性和稳定性.
- 该方法确保多个导弹在不同的终端角度达到最低可接受的拦截距离,同时优化LOS燃料使用量.
结论:
- 开发的指导策略有效地实现了对机动目标的同时,多角度拦截.
- 这种方法通过最大限度地减少损害和优化资源利用 (燃料) 来提高任务的成功.
- 该方法为复杂的多导弹交战场景提供了强大的解决方案.
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