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 |
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代理人 |
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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 |