发明名称 Four-dimensional guidance of an aircraft
摘要 <p>The present invention relates to methods of controlling the flight path of an aircraft to follow as closely as possible a predetermined four-dimensional flight path, such as when flying continuous descent approaches. A method of controlling an aircraft to follow a predetermined four-dimensional flight path is provided that comprises monitoring an actual along-track position and an actual vertical position of the aircraft relative to corresponding desired positions on the predetermined flight path. Throttle commands are generated based on deviations of the actual vertical position of the aircraft from the desired vertical position. Elevator commands are generated based on the deviation of the actual along-track position from the desired along-track position and on the deviation of the actual vertical position from the desired vertical position.</p>
申请公布号 EP2282247(A1) 申请公布日期 2011.02.09
申请号 EP20090382064 申请日期 2009.05.05
申请人 THE BOEING COMPANY 发明人 GOMEZ LEDESMA, RAMON;GARRIDO-LOPEZ, DAVID
分类号 G05D1/10 主分类号 G05D1/10
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