发明名称 |
ROLL ATTITUDE-DEPENDENT ROLL RATE LIMIT |
摘要 |
Systems and methods are provided for a roll attitude dependent roll rate limit that may limit an aircraft to a lower roll rate limit under normal flight conditions. The systems and methods may detect situations where a higher roll rate limit may be desirable and allow the aircraft to exceed the lower roll rate limit, to either a higher roll rate limit or a roll rate between the lower and higher roll rate limit. |
申请公布号 |
EP3141976(A1) |
申请公布日期 |
2017.03.15 |
申请号 |
EP20160179216 |
申请日期 |
2016.07.13 |
申请人 |
The Boeing Company |
发明人 |
WILSON, Douglas L;GRUBB, David W;MOREL, Mark R. |
分类号 |
G05D1/00;G05D1/08 |
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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