公开(公告)号：US3807660A

公开(公告)日：1974-04-30

申请号：US30384072

申请日：1972-11-06

Applicant: AEROSPATIALE

Inventor： LE CORVIGER P ,  MONTASTIER M

IPC: B64G1/24 ,  B64G1/28 ,  B64G1/36 ,  G05D1/10 ,  H03K19/173 ,  F41G7/00

CPC classification number: G05D1/107 ,  B64G1/24 ,  B64G1/288 ,  B64G1/36 ,  H03K19/173

Abstract: Logic system for controlling a missile in flight comprising four deflecting surfaces actuated between two positions, by the means of three binary signals, the eight arrangements of said binary signals, on an electric or electronic circuit, including OR and AND gates and NOR gates, determining the order in yaw or pitch in association with possible roll control for fetching a reference plane.

Abstract translation: 用于控制飞行中的导弹的逻辑系统包括通过三个二进制信号在两个位置之间致动的四个偏转表面，所述二进制信号的八个布置在包括OR和AND门和NOR门的电或电子电路上，确定 与用于提取参考平面的可能的滚动控制相关联的偏航或俯仰的顺序。