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Ballistic missile trajectory prediction and the solution algorithms for impact point prediction

机译:弹道导弹的弹道预测及冲击点预测的求解算法

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In order to improve the guidance precision of the ballistic missile interception, the target's trajectory prediction and the impact point prediction solution algorithm for interceptor's mid-course guidance are studied. Firstly, in allusion to the drawbacks of current ballistic missile's trajectory predication, the high precision ballistic missile prediction algorithms based on predictor-corrector method considering the radar's measurement noise are designed on the premise of ballistic missile tracking. Then, in allusion to the drawbacks of dead circulation, heavy computation, and engineering unavailability in current impact point prediction solving, the basic strategy of impact point prediction guidance is studied, and the iterative solution algorithm of forecasting impact point based on time series is designed with common applicability, less computation and engineering availability, and then the computing circuit is proposed. Simulations results show that the proposed algorithms of ballistic trajectory prediction and impact point prediction solution have better precision and availability, which could offer some theoretical meaning and some references for engineering application.
机译:为了提高弹道导弹拦截的制导精度,研究了目标的弹道预测和拦截器中段制导的冲击点预测求解算法。首先,针对当前弹道导弹弹道预测的弊端,在弹道导弹跟踪的前提下,设计了一种基于预测校正法的高精度弹道导弹预测算法,该算法考虑了雷达的测量噪声。然后针对当前冲击点预测求解中死循环,计算量大,工程不可用等缺点,研究了冲击点预测指导的基本策略,设计了基于时间序列的迭代预测冲击点求解算法。具有通用性,较少的计算量和工程上的可利用性,提出了计算电路。仿真结果表明,所提出的弹道轨迹预测和碰撞点预测算法具有较高的精度和可用性,可以为工程应用提供一定的理论意义和参考价值。

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