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这篇文章分析六自由度的 SDI 天基动能武器的拦截过程装订方案,装订方案主要包括从雷达平台至发射平台的目标信息传递、发射平台的初始参数至拦截器的参数传递、预测遭遇点的算法、发射架的瞄准以及拦截器本身的卡尔曼滤波器和目标预测器启动方法。确定了这些概念的模型并考虑了与之有关的误差源。正象六自由度仿真所验证的,主要对装订误差对天基动能武器系统性能影响作了讨论。
This article analyzes the six-degree-of-freedom (SDI) space-based kinematic weapon intercept binding process, which includes target information transfer from the radar platform to the launch platform, the initial parameters of the launch platform to the interceptor parameter transfer, Algorithm, the aiming of the launcher and the Kalman filter of the interceptor itself and the method of starting the target predictor. The models for these concepts were identified and the sources of error associated with them were taken into account. As verified by the six-degree-of-freedom simulation, the effects of stapling errors on the performance of space-based kinetic energy weapon systems are discussed.