发明名称 |
Limiting aircraft vertical acceleration response |
摘要 |
The presently-disclosed invention utilizes sensed pitched rate and sensed vertical acceleration to prevent aberrant pitch rate command outputs as a function of lead compensated sensed acceleration, controlling the vertical acceleration by sensing when a maximum is approached. When the lead compensated acceleration exceeds a first predetermined acceleration factor, the presently-sensed pitch rate replaces the pre-programmed maximum pitch rate factor as the temporary maximum rate, to temporarily prevent additional vertical acceleration due to increasing pitch rate. This apparatus requires no airspeed input and does not interfere with flight performance characteristics during normal flight operations, allowing higher torque servos to be used, and thus improves overall performance.
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申请公布号 |
US4787042(A) |
申请公布日期 |
1988.11.22 |
申请号 |
US19850799222 |
申请日期 |
1985.11.18 |
申请人 |
ROCKWELL INTERNATIONAL CORPORATION |
发明人 |
BURNS, ROGER D.;ANSPACH, LARRY A. |
分类号 |
G05D1/00;(IPC1-7):G05D1/06 |
主分类号 |
G05D1/00 |
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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