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Flight management system execution of idle-thrust descents in operations

机译:飞行管理系统在运行中执行空推力下降

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To enable arriving aircraft to fly optimized descents computed by the flight management system (FMS) in congested airspace, ground automation must accurately predict descent trajectories. To support development of the trajectory predictor and its error models, commercial flights executed idle-thrust descents, and the recorded data includes the target speed profile and FMS intent trajectories. The FMS computes the intended descent path assuming idle thrust after top of descent (TOD), and any intervention by the controllers that alters the FMS execution of the descent is recorded so that such flights are discarded from the analysis. The horizontal flight path, cruise and meter fix altitudes, and actual TOD location are extracted from the radar data. Using more than 60 descents in Boeing 777 aircraft, the actual speeds are compared to the intended descent speed profile. In addition, three aspects of the accuracy of the FMS intent trajectory are analyzed: the meter fix crossing time, the TOD location, and the altitude at the meter fix. The actual TOD location is within 5 nmi of the intent location for over 95% of the descents. Roughly 90% of the time, the airspeed is within 0.01 of the target Mach number and within 10 KCAS of the target descent CAS, but the meter fix crossing time is only within 50 sec of the time computed by the FMS. Overall, the aircraft seem to be executing the descents as intended by the designers of the onboard automation.
机译:为了使到达的飞机能够在拥挤的空域中飞行由飞行管理系统(FMS)计算的最佳下降,地面自动化必须准确地预测下降轨迹。为了支持轨迹预测器及其误差模型的开发,商业航班执行了空转推力下降,并且记录的数据包括目标速度曲线和FMS意图轨迹。 FMS假定下降后顶部(TOD)后有空转推力,计算预期的下降路径,并记录控制器更改FMS执行下降的任何干预,以便从分析中丢弃此类飞行。从雷达数据中提取水平飞行路径,巡航和仪表固定高度以及实际TOD位置。在波音777飞机上使用60多个下降时,将实际速度与预期的下降速度曲线进行比较。此外,还分析了FMS意图轨迹的准确性的三个方面:仪表固定点穿越时间,TOD位置以及仪表固定点的高度。超过95%的下降位置,实际TOD位置在目标位置的5 nmi以内。大约有90%的时间,空速在目标马赫数的0.01以内,并且在目标下降CAS的10 KCAS以内,但是仪表固定横越时间仅在FMS计算的时间的50秒以内。总体而言,飞机似乎按照机上自动化设计者的意图执行下降任务。

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