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Frequency-Modulated Pulse-Jet Control of an Artillery Rocket

机译:炮弹的调频脉冲喷射控制

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摘要

Long- and medium-range artillery rockets are used for indirect fire on distant targets. As they have a large impact-point dispersion, they are considered to be area weapons. Nevertheless, a control system is required in order to reduce the dispersion and increase hit probability. The pulse-jet control system is simple and efficient enough to produce acceptable impact-point dispersion. However, it is necessary to perform an optimization of the control logic in order to obtain a satisfactory performance with the minimum number and intensity of control pulses. A new two-phase guidance scheme named trajectory tracking with pulse-frequency modulation is presented, considering the fact that an artillery rocket flies through different atmospheric environments. Simulation studies have been conducted in order to perform parametric and performance analyses. It is shown that the presented guidance scheme achieves excellent accuracy even in the case of a small number of pulse jets. In the case of a large number, it tends to nullify the impact-point dispersion. It is also shown that in comparison with the window-based trajectory-tracking guidance, the proposed method achieves significantly better results.
机译:中远程火炮火箭用于对远距离目标进行间接射击。由于它们的冲击点分散很大,因此被认为是区域武器。然而,需要控制系统以减少分散并增加命中概率。脉冲喷射控制系统非常简单有效,足以产生可接受的冲击点色散。但是,有必要对控制逻辑进行优化,以便以最少的控制脉冲数量和强度获得令人满意的性能。考虑到火炮在不同的大气环境中飞行的事实,提出了一种新的两阶段制导方案,即脉冲频率调制的轨迹跟踪。为了进行参数和性能分析,已经进行了仿真研究。结果表明,即使在脉冲喷射数量较少的情况下,所提出的制导方案也能达到极好的精度。在大量情况下,它倾向于使冲击点分散消失。还表明,与基于窗口的轨迹跟踪引导相比,该方法取得了明显更好的效果。

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