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Steering shells to manoeuvring flying targets - using temporally decoupled measurement and control phases of coincidence computer to eliminate shell oscillation
Steering shells to manoeuvring flying targets - using temporally decoupled measurement and control phases of coincidence computer to eliminate shell oscillation
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机译:操纵炮弹以操纵飞行目标-使用时间相吻合的计算机进行时间分离的测量和控制阶段以消除炮弹振动
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摘要
The method of guiding shells to enable their hit reliability to be increased involves using a guidance rule which steers the shell on a collision course with the target. The desired course of the shell is derived by a guidance computer at each correction time point from the spatial angular deviation of the actual value of the shell/ target line from its desired value. The guidance measurement and control phases are decoupled in time to suppress shell oscillations arising from control action during the subsequent measurement phase. USE/ADVANTAGE - E.g. for guiding shells towards direct impact with manoeuvering flying targets to achieve significantly higher strike accuracy.
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