Applying NIORAIM to the solution separation method for inertially-aided aircraft autonomous integrity monitoring

Proceedings of the Institute of Navigation, National Technical Meeting

Volumn , Issue , 2005, Pages 992-1000

  Hwang, Patrick Y ^a  

^a ROCKWELL COLLINS   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT AUTONOMOUS INTEGRITY MONITORING (AAIM); HORIZONTAL INTEGRITY LIMIT (HIL); INERTIALLY-AIDED AIRCRAFT; NON-PRECISION APPROACHES (NPA);

ALGORITHMS; SATELLITE COMMUNICATION SYSTEMS; SENSORS; SIGNAL RECEIVERS; STATISTICAL METHODS;

AIRCRAFT;

EID: 27744574975     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. John Diesel, "A New Approach to GPS Integrity/Availability: Immediate Global Sole Means Without WAAS," Proceedings of the ION Seventh International Technical Meeting (GPS-94), Salt Lake City, UT, 1994, pp. 567-576.
2. Mats Brenner, "Integrated GPS/Inertial Fault Detection Availability," Papers published in NAVIGATION (Red Book Series), Vol. 5, pp. 339-358.
3. Ryan S. Y. Young and Gary A. McGraw, "Fault Detection and Exclusion Using Normalized Solution Separation and Residual Monitoring Methods," NAVIGATION, Journal of the Institute of Navigation, Vol. 50, No. 3 (Fall), 2003.
4. Patrick Y. Hwang and R. Grover Brown, "RAIM FDE Revisited: A New Breakthrough In Availability Performance With NIORAIM (Novel Integrity-Optimized RAIM)," Proceedings of the National Technical Meeting of the ION, San Diego, CA, January 2005.
5. R. Grover Brown and Gerald Y. Chin, "GPS RAIM: Calculation of Threshold and Protection Radius Using Chi-Square Methods - A Geometric Approach," Papers published in NAVIGATION (Red Book Series), Vol. 5, pp.155-178.
6. rd Edition, J.Wiley, New York, 1998.