发明名称 Target tracking vehicle guidance system - operates in command guidance mode for portion of its flight and then in homing guidance mode
摘要 <p>The vehicle is guided in either a command guidance mode or a homing mode. In the commands guidance mode, the target tracking element, used during the homing guidance mode serves as an inertial reference element. Such element is attitude stabilised in pitch and yaw by a mechanical drive used in both modes. The device drives the reference element w.r.t. the vehicle's body and, in roll, by the vehicle's roll autopilot to aerodynamically control the vehicle's attitude in roll.</p>
申请公布号 IT1102670(B) 申请公布日期 1985.10.07
申请号 IT19780049369 申请日期 1978.05.15
申请人 RAYTHEON CO 发明人
分类号 G01S;(IPC1-7):G01S/ 主分类号 G01S
代理机构 代理人
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