[1] ICAO Doc 9613.Performance Based Navigation (PBN) manual［S］．3rd ed.2008.

[2] Federal Aviation Administration. Roadmap for performance-based navigation［Z］.Federal Aviation Administration Washington DC July 2006.

[3] NIKIFOROV I. Integrity monitoring for multi-sensor integrated navigation systems［C］//Proceedings of the 15th International Technical Meeting of the Satellite Division of Navigation(ION GPS 2002) 2002:579-590.

[5] BRENNER M.Integrated GPS/Inertial fault detection av-ailability［C］//Proceedings of ION GPS-95 Palm Springs Virginia USA 1995:1949-1958.

[6] DIESEL J KING J. Integration of navigation systems for fault detection exclusion and integrity determination with-out WAAS［C］//Proceedings of the 1995 Technical Meeting of Navigation 1995:683-692.

[7] LEE Y C O'LAUGHLIN D G. A performance analysis of atightly coupled GPS/Inertial system for two integrity monitoring methods［J］.Journal of Navigation ION GPS 1999:1187-1200.

[12] DIESEL J LUU S. GPS/IRS AIME:Calculation of thresholds and protection radius using chi-square methods［C］//Proceedings of the 8th International Technical Metting of the Satellite Division of Navigation (ION GPS 1995) 1995:1959-1964.

[13] LIU H ZHENG G WANG H et al. Research on integrity monitoring for integrated GNSS/SINS system［C］//The 2010 IEEE International Conference on Information and Automation Harbin China 2010:1990-1995.

[14] YOUNG R S Y MCGRAW G A.Fault detection and exclusion using normalized solution separation and residual monitoring methods［J］. Navigation 2003 50(3):151-170.