初始对准误差对导弹自控终点误差影响分析
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Analysis for Calculating Influence of Initial Alignment Error on Auto-Control Termination Error of Sub-Launched Missile
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    摘要:

    潜射导弹初始对准误差会产生导弹自控终点误差,通过理论分析,建立了由初始对准误差对自控终点误差的影响模型,并对该模型进行简化,最后,依据潜射反舰导弹初始对准结果了进行仿真计算,结果表明,该模型能避免烦琐的运动学建模和编程计算过程,为在项目论证阶段不具备完备的总体数据的支持条件下,进行初始对准精度指标分配提供理论依据。

    Abstract:

    The initial alignment error would produce the auto-control termination of sub-launched missile. Based on the theoretical analysis, deduces a simplified algorithm to calculate the impact of the initial alignment errors on auto-control termination errors of sub-launched missile weapons. Finally, the numerical results calculated by the simulation with the initial alignment data of the sub-launched missile. The simulation results show that the model is simple, pellucid and wieldy, avoids fussy calculation and provides academic foundation of allotting the initial alignment error index without enough missile data support in the project verification phase.

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程明文,刘勇志,徐显强.初始对准误差对导弹自控终点误差影响分析[J].,2010,29(04):82-84.

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  • 收稿日期:2010-06-12
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