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Integrity monitoring method and apparatus for GPS and DGPS receivers
   
Document Number
US Patent 5663732
Issued Date
September 2, 1997
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Abstract
A fail safe GPS system for an aircraft moving along a desired trajectory within vertical and horizontal limits using first and second redundant GPS receivers a first of which is connected to the avionics equipment of the aircraft and to an alarm and the second of which is connected only to the alarm so that if a malfunction in the flight management system occurs both GPS's will cause the alarm and if a malfunction in the first GPS system occurs, so that the aircraft exceeds the vertical or horizontal limits, the second GPS system will cause the alarm.
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Integrity monitoring method and apparatus for GPS and DGPS receivers - US Patent 5663732 Drawing
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Number of Claims:
6
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Owner
Honeywell Inc. (Minneapolis, MN)
Published
September 2, 1997
Application Number
08/450,047
Filed
May 25, 1995
US Classification
342/357.06   340/979 701/213
Int'l Classification
G01C   5/00   (20060101)   G01S   1/00   (20060101)   G01S   5/14   (20060101)   G01S   5/00   (20060101)  
Attorney/Law Firm
USPTO Field of Search
342/357   342/457   364/424.06   340/979  
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Description
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