发明名称 An aircraft system and method for improving navigation performance
摘要 A high integrity navigation system and method are provided. The method comprises performing a cyclic redundancy check (CRC) of a desired flight path of an aircraft, for example an approach to an airport, and comparing the CRC with a stored CRC performed on the identified flight path. If the comparison exceeds a first threshold, a first alert is provided wherein the pilot is to perform a published missed approach. A second alert, also requiring a missed approach, is provided when one or more comparisons are performed of a sensor position of the aircraft with the high integrity flight path; a defined flight path with the high integrity flight path; and the sensor position with an aircraft position determined by a flight management system, and thresholds are exceeded.
申请公布号 EP2685218(A3) 申请公布日期 2016.03.23
申请号 EP20130173676 申请日期 2013.06.25
申请人 HONEYWELL INTERNATIONAL INC. 发明人 SHEHI, CHRISTOPHER JOHN;CROCKER, REGINALD;TENPASSBELL, KIMBERLY;JOHNSON, JAMES
分类号 G01C23/00 主分类号 G01C23/00
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