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System and method for aircraft performance predictions for descent and approach phases
System and method for aircraft performance predictions for descent and approach phases
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机译:用于下降和进场阶段的飞机性能预测的系统和方法
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摘要
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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