寻找过器,指导和控制的整合,用于准确的高速目标拦截
Ali Chitsaz1, Abolghasem Naghash1, Farhad Fani Saberi2
1Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran.
Scientific reports
|November 20, 2025
概括
这项研究引入了一种新的综合指导和控制 (IGC) 方案,用于拦截高速弹道目标. 这种新方法通过整合先进的控制和估计技术来提高击中杀死精度,即使寻找者数据不完美.
科学领域:
- 航空航天工程 航空航天工程
- 导航,导航和控制系统 (GNC) 是指导,导航和控制系统.
背景情况:
- 攻击高速弹道目标在终端阶段拦截中带来了重大挑战.
- 实现击中杀死性能需要复杂的硬件和软件解决方案的集成.
研究的目的:
- 提出一个新的三维综合指导和控制 (IGC) 方案,以加强终端阶段的参与.
- 通过解决船上搜索器错误,空气动力学不确定性和目标机动来提高拦截准确性.
主要方法:
- 开发一个三维的IGC方案,使用转向控制系统和花链技术.
- 制定一个扩展的卡尔曼波器与一个准确的动力学模型为一个双轴杆寻找器.
- 实现基于干扰观察者控制 (DOBC) 的实施,使用减少顺序扩展状态观察者 (ROESO) 和精确寻找器过器.
主要成果:
- 拟议的IGC方案实现了对高速目标的击中杀伤性能.
- 准确估计视线速率和目标加速度是没有假设理想的寻找者测量实现的.
- 模拟显示在高海拔和高零力度失误场景中使用联合推进器和翅膀控制的效果.
结论:
- 新的IGC战略为挑战弹道目标拦截提供了一个强有力的解决方案.
- 该方法克服了现有方案的局限性,因为它不假设理想的视线可用性.
- 综合方法在复杂场景中增强了参与能力,并通过广泛的模拟证明了其有效性.
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