发明名称 Flight management system with integrated tactical commands for use with an aircraft and method of operating same
摘要 <p>A flight management system (24) for use in automatically generating a flight path trajectory (26) for an aircraft (10) is provided. The flight path trajectory including a plurality of waypoints (28) and a plurality of vectors (30) extending between each waypoint of the plurality of waypoints, the flight management system including a processor (302) is configured to calculate a first flight path trajectory (36) including an origin waypoint (40) and a destination waypoint (42), receive a tactical command indicating a change in flight trajectory, and calculate a second flight path trajectory (38) based at least in part on the tactical command, the calculated second flight path trajectory including a departure waypoint along the first flight path trajectory, an intercept waypoint (48) along the first flight path trajectory, and a departure vector from the departure waypoint (46) to the intercept waypoint. </p>
申请公布号 EP2474812(A3) 申请公布日期 2013.08.28
申请号 EP20120150189 申请日期 2012.01.04
申请人 GE AVIATION SYSTEMS LLC 发明人 WALTER, RANDY LYNN
分类号 G01C23/00;G08G5/00 主分类号 G01C23/00
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