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    • 1. 发明授权
    • System for guiding remote-controlled missiles
    • 遥控导弹系统
    • US4313580A
    • 1982-02-02
    • US89961
    • 1979-10-31
    • Hubert Collette
    • Hubert Collette
    • F41G7/24F41G7/00F41G7/30G05D1/12
    • F41G7/308F41G7/30
    • The present invention relates to a system for guiding remote-controlled missiles, enabling these missiles to be fired by bursts, comprising a sighting device, an angular deviation measuring (ADM) device and a device for controlling the path; according to the invention, partial, individual and separate fields are defined in the field of the ADM device, said fields corresponding to various zones where successive missiles may be addressed, and said control device is designed for simultaneously guiding a plurality of missiles on a plurality of distinct predetermined standby courses spaced apart with respect to said line of sight. The invention finds particular application in the guiding of ground-ground, ground-air, or air-ground missiles.
    • 本发明涉及用于引导远程控制导弹的系统,使这些导弹能够通过脉冲串来发射,包括瞄准装置,角度偏差测量装置(ADM)装置和用于控制路径的装置; 根据本发明,在ADM设备的领域中限定了部分的,单独的和分离的场,所述场对应于可以寻址连续导弹的各个区域,并且所述控制设备被设计成同时引导多个导弹的多个导弹 相对于所述视线间隔开的不同的预定待机课程。 本发明特别适用于地面,地面或空地导弹的引导。