发明名称 SYSTEMS AND METHODS FOR REDUCING ERROR DETECTION LATENCY IN LPV APPROACHES
摘要 Systems and methods for reducing error detection latency in LPV approaches are provided. In certain embodiments, a method for navigational guidance includes calibrating inertial measurements acquired from an inertial navigation system with satellite-based augmentation system position measurements acquired from a satellite-based augmentation system to create corrected inertial navigation system positions. The method also includes determining whether the satellite-based augmentation system experienced a fault when the inertial measurements were calibrated with the satellite-based augmentation system position measurements. Further, when the satellite-based augmentation system did not experience a fault, the method includes monitoring the satellite-based augmentation system navigation position measurements based on the corrected inertial navigation system positions.
申请公布号 US2014288733(A1) 申请公布日期 2014.09.25
申请号 US201313847151 申请日期 2013.03.19
申请人 HONEYWELL INTERNATIONAL INC. 发明人 He Gang;Wyatt Ivan Sandy
分类号 G08G5/02;G01C21/00 主分类号 G08G5/02
代理机构 代理人
主权项 1. An aircraft landing system on an aircraft, the system comprising: an inertial navigation system configured to make inertial measurements of motion for the aircraft; a satellite-based augmentation system configured to provide satellite-based augmentation system position measurements of the aircraft; and a processor configured to receive the inertial measurements from the inertial navigation system and receive the satellite-based augmentation system position measurements from the satellite-based augmentation system, wherein the processor executes instructions that cause the processor to: calibrate the inertial measurements to the satellite-based augmentation system position measurements;determine whether the satellite-based augmentation system experienced a fault when the inertial measurements were calibrated with the satellite-based augmentation system position measurements; andwhen the satellite-based augmentation system did not experience a fault, monitor the satellite-based augmentation system navigation position measurements based on the calibrated inertial measurements.
地址 Morristown NJ US