发明名称 |
Method and apparatus for an aircraft inner loop elevator control system |
摘要 |
An improved inner loop control is disclosed for use in an aircraft pitch axis control system. Signals representative of vertical acceleration and pitch rate are complementary filtered and summed to produce an "inner loop" damping signal which is combined with "outer loop" command signals to produce an elevator control signal. The improved approach provides higher outer loop control law gains and better system stability, resulting in higher control bandwidth and tighter command tracking, especially in turbulence.
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申请公布号 |
US4419732(A) |
申请公布日期 |
1983.12.06 |
申请号 |
US19810301911 |
申请日期 |
1981.09.14 |
申请人 |
THE BOEING COMPANY |
发明人 |
LAMBREGTS, ANTONIUS A.;HANSEN, ROLF |
分类号 |
G05D1/06;(IPC1-7):G06G7/78;G05D1/12 |
主分类号 |
G05D1/06 |
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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