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Aeronautical Holding Pattern Calculation for Solving High Wind and Protected Airspace Issues

机译:解决强风和保护空域问题的航空保持模式计算

摘要

An apparatus comprising a memory and a processor coupled to the memory, wherein the processor is configured to receive holding instructions for an aircraft, wherein the holding instructions comprise a holding fix, a holding direction, and an inbound leg course, obtain an airspeed for the aircraft, obtain a wind speed and a wind direction affecting the aircraft, calculate a holding pattern for the aircraft using the holding instructions, the wind speed, the wind direction, an inbound leg duration, and the airspeed, obtain Federal Aviation Administration (FAA) protected airspace limits associated with the holding fix, and present the holding pattern and the FAA protected airspace limits to a flight crew member on the aircraft.
机译:一种设备,包括存储器和耦合到该存储器的处理器,其中处理器被配置为接收飞机的保持指令,其中该保持指令包括保持固定点,保持方向和向内的航向,从而获得飞机的空速。飞机,获取影响飞机的风速和风向,使用保持指令,风速,风向,入站航程和空速计算飞机的保持模式,并获得联邦航空管理局(FAA)与保持架相关的受保护空域限制,并向飞机上的飞行机组人员提供保持模式和FAA受保护空域限制。

著录项

  • 公开/公告号US2014257684A1

    专利类型

  • 公开/公告日2014-09-11

    原文格式PDF

  • 申请/专利权人 EPOCH FLIGHT SYSTEMS LLC;

    申请/专利号US201414193542

  • 发明设计人 BRUCE GARY WILDER;OTTO CHARLES WILKE;

    申请日2014-02-28

  • 分类号G08G5/00;

  • 国家 US

  • 入库时间 2022-08-21 16:10:31

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