发明名称 |
Aircraft take off procedure |
摘要 |
<p>A pitch command for aiding aircraft take-off is corrected as a function of speed deviation existing between a rotation speed and a reference speed. The angle of deflection of an adjustable horizontal tail plane is determined as a function of the longitudinal position at the center of gravity of the aircraft.</p> |
申请公布号 |
EP1591854(A1) |
申请公布日期 |
2005.11.02 |
申请号 |
EP20050290678 |
申请日期 |
2005.03.29 |
申请人 |
AIRBUS FRANCE |
发明人 |
DELAPLACE, FRANCK;MATHIEU, GERARD;DANIEL, NICOLAS |
分类号 |
G05D1/00;G05D1/08;(IPC1-7):G05D1/00 |
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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