发明名称 HEURISTIC METHOD FOR COMPUTING PERFORMANCE OF AIRCRAFT
摘要 <P>PROBLEM TO BE SOLVED: To provide a method that can derive reliable values relative to aircraft operating parameters, such as an engine fuel flow rate and a rate of climb of an aircraft, from a smaller amount of aircraft performance data. <P>SOLUTION: The method estimates a vertical airspeed and a fuel flow of an aircraft at a point along a flight plan using other aircraft parameters for that point. More particularly, when vertical airspeed and fuel flow estimates are needed, the method uses a database containing sets of actual values of operating parameters of an aircraft to identify a set of actual values of operating parameters that best matches the other aircraft parameters, and applies the vertical airspeed and fuel flow values obtained from that identified set as the estimates. <P>COPYRIGHT: (C)2013,JPO&INPIT
申请公布号 JP2013014325(A) 申请公布日期 2013.01.24
申请号 JP20120150966 申请日期 2012.07.05
申请人 UNIVERSAL AVIONICS SYSTEMS CORP 发明人 LIEU BRIAN V
分类号 B64D45/00 主分类号 B64D45/00
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