发明名称 |
CLOSED LOOP CONTROL OF AIRCRAFT CONTROL SURFACES |
摘要 |
Closed loop control method for control surfaces includes measuring a flight metric of an aircraft during flight and calculating, using a processor, a deflection of a control surface of the aircraft based on the flight metric.
The disclosed method also includes adjusting the deflection to an effective deflection level based on the calculated deflection to reduce a drag coefficient of the aircraft. |
申请公布号 |
EP2974955(A2) |
申请公布日期 |
2016.01.20 |
申请号 |
EP20150170142 |
申请日期 |
2015.06.01 |
申请人 |
THE BOEING COMPANY |
发明人 |
PACHIKARA, ABRAHAM J.;MOSER, MATTHEW A.;CARPENTER, PAUL H.;FINN, MICHAEL R.;KOCH, THOMAS S.;BIENIAWSKI, STEFAN R.;WHITEHEAD, BRIAN T. |
分类号 |
B64C13/16;B64C9/12;G05D1/00 |
主分类号 |
B64C13/16 |
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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