System and method for aircraft performance predictions for descent and approach phases
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United States of America Patent
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Sep 13, 2016
Grant Date -
Nov 1, 2012
app pub date -
Apr 23, 2012
filing date -
Apr 29, 2011
priority date (Note) -
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Abstract
A system and method for aircraft performance predictions for descent and approach phases are disclosed. In one embodiment, cruise computation is stopped substantially around a default distance from a destination. Further, current predicted aircraft state is determined using a total energy of the aircraft starting from the default distance. Furthermore, descent and approach phase profiles are computed using the determined current predicted aircraft state. In addition, the aircraft performance predictions are obtained using the computed descent and approach phase profiles.
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