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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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