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
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