发明名称 ROLLING AIRFRAME AUTOPILOT
摘要 <p>ROLLING AIRFRAME AUTOPILOT The autopilot incorporates a single linear accelerometer transducer and a single pitch rate sensor. the outputs of the accelerometer and pitch rate sensor are summed with the command signal in the control circuit. A servo is controlled by the modified control signal to vary the incidence of a single plane control system, in an intentionally rolling airframe.</p>
申请公布号 CA1087714(A) 申请公布日期 1980.10.14
申请号 CA19760267162 申请日期 1976.12.03
申请人 GENERAL DYNAMICS CORPORATION 发明人 COLE, DONALD E.
分类号 B64C13/18;F42B10/62;G05D1/10;(IPC1-7):05D1/08 主分类号 B64C13/18
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