专利名称：HORIZONTAL TAIL LOAD OPTIMIZATION
SYSTEM AND METHOD
发明人：Vedad Mahmulyin申请号：US15797576申请日：20171030
公开号：US20180043992A1公开日：20180215
专利附图：
摘要：A method of controlling an elevator of an aircraft includes selecting a factor forincreasing or decreasing a predetermined horizontal tail load alleviation (HTLA) authoritylimit for an elevator based on at least one aircraft parameter. The HTLA authority limit
decreases with an increase in Mach number and/or airspeed. The method also includescomputing an elevator position limit as a product of the HTLA authority limit and thefactor, and moving the elevator to a commanded elevator position that is no greater thanthe elevator position limit.
申请人：The Boeing Company
地址：Chicago IL US
国籍：US
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