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METHOD OF ADVANCING THE POINT OF IMPACT FOR PASSIVE-LOCATION MISSILES GUIDED BY MEANS OF PROPORTIONAL NAVIGATION IN THE SELF-GUIDE PHASE
METHOD OF ADVANCING THE POINT OF IMPACT FOR PASSIVE-LOCATION MISSILES GUIDED BY MEANS OF PROPORTIONAL NAVIGATION IN THE SELF-GUIDE PHASE
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机译:在自导相中按比例导航的方式提前预测被动定位导弹的冲击点的方法
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1506840 Navigational calculators LICENTIA PATENT-VERWALTUNGS-GmbH 23 Aug 1968 [12 Sept 1967] 40541/68 Heading G4G [Also in Division B7] In an acoustic, proportional navigation, self-guidance system for a torpedo, to prevent, the torpedo aiming directly at the noise source (i.e. the propeller wake) the point of impact with the target ship is advanced from the stern by injecting a disturbance parameter into the torpedo control circuit at a predetermined range from the target. The target distance from the torpedo is measured by observing the change in noise level which occurs during a given track length, and when the predetermined range is reached the disturbance parameter is fed into the control circuit.
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