发明名称 Vertical required navigation performance containment with radio altitude
摘要 A monitor on-board an aircraft which uses radio altitude measurements as the basic observable altitude during runway approach. The basic concept utilizes the aircraft's navigation system, which includes means to store and retrieve radio altitude thresholds as a function of the distance along the desired path from the runway thresholds. These threshold functions are determined in advance based on a radio altitude reference which is defined as the expected radio altimeter measurement that would be made if the airplane were exactly on the desired reference path. Vertical containment monitoring is achieved by comparing the radio altitude measurement to computed thresholds for both too high and too low. During the approach, an annunciation message can be generated if the radio altitude measurement is above or below the threshold limits.
申请公布号 US8798819(B2) 申请公布日期 2014.08.05
申请号 US201313920355 申请日期 2013.06.18
申请人 The Boeing Company 发明人 Murphy Timothy Allen
分类号 G06F19/00;G06G7/70 主分类号 G06F19/00
代理机构 Ostrager Chong Flaherty & Broitman P.C. 代理人 Ostrager Chong Flaherty & Broitman P.C.
主权项 1. An onboard system for detecting deviation of true airplane vertical position from a desired reference path, comprising: a database storing high and low radio altitude thresholds which vary as a function of horizontal distance from a runway threshold; a GNSS receiver for acquiring horizontal position measurements as the aircraft approaches the runway threshold; a radio altimeter for acquiring radio altitude measurements as the aircraft approaches the runway threshold; and a processor for computing a horizontal distance from the runway threshold using the horizontal position measurements and comparing each radio altitude measurement to a respective pair of said high and low radio altitude thresholds as the aircraft approaches the runway threshold.
地址 Chicago IL US