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Volumn 2005, Issue , 2005, Pages 1749-1759

MMR-centric multisensor integration architecture for civil aviation applications

Author keywords

[No Author keywords available]

Indexed keywords

AVIONIC INTERFACES; MULTI-MODE RECEIVER (MMR); MULTISENSOR INTEGRATION ARCHITECTURE; NAVIGATION SENSORS;

EID: 33646542745     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (1)

References (8)
  • 2
    • 0344941722 scopus 로고    scopus 로고
    • Global Positioning System: Theory and Applications, American Institute of Aeronautics and Astronautics, Washington D.C.
    • Greenspan, R. L., GPS and Inertial Navigation, Global Positioning System: Theory and Applications, Volume II, American Institute of Aeronautics and Astronautics, Washington D.C., 1996.
    • (1996) GPS and Inertial Navigation , vol.2
    • Greenspan, R.L.1
  • 3
    • 33646544319 scopus 로고    scopus 로고
    • Analysis of coast times upon loss of GPS signals for integrated GPS/inertial systems
    • Anaheim, CA, January 22-24
    • Lee, C. Y., Ericson, S. D., "Analysis of Coast Times Upon Loss of GPS Signals for Integrated GPS/Inertial Systems," Proceedings of ION NTM 2003, Anaheim, CA, January 22-24, 2003.
    • (2003) Proceedings of ION NTM 2003
    • Lee, C.Y.1    Ericson, S.D.2
  • 4
    • 71249151219 scopus 로고    scopus 로고
    • Fault detection and exclusion using normalized solution separation and residual monitoring methods
    • Young, R. S-Y, McGraw, G. A., "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, pp. 151-169.
    • (2003) Navigation: Journal of the Institute of Navigation , vol.50 , Issue.3 FALL , pp. 151-169
    • Young, R.S.-Y.1    McGraw, G.A.2
  • 5
    • 0032024190 scopus 로고    scopus 로고
    • Strapdown inertial navigation integration algorithm design part 2: Velocity and position algorithms
    • Savage, P. G., "Strapdown Inertial Navigation Integration Algorithm Design Part 2: Velocity and Position Algorithms," AIAA Journal of Guidance, Control, and Dynamics, Vol. 21, No. 2, March-April, 1998.
    • (1998) AIAA Journal of Guidance, Control, and Dynamics , vol.21 , Issue.2 MARCH-APRIL
    • Savage, P.G.1
  • 6
    • 84858869358 scopus 로고    scopus 로고
    • "Method and System for Deriving Inertial-Aided Deviations for Autoland Systems During GPS Signal Interruptions," U.S. Patent 6845304, January 18
    • Young, S.Y., "Method and System for Deriving Inertial-Aided Deviations for Autoland Systems During GPS Signal Interruptions," U.S. Patent 6845304, January 18, 2005.
    • (2005)
    • Young, S.Y.1
  • 7
    • 33646573606 scopus 로고    scopus 로고
    • Minimum operational performance standards for GPS local area augmentation system airborne equipment
    • January 11
    • "Minimum Operational Performance Standards for GPS Local Area Augmentation System Airborne Equipment", RTCA DO-253, January 11, 2000.
    • (2000) RTCA , vol.DO-253
  • 8
    • 84858882306 scopus 로고    scopus 로고
    • "Inertially Augmented GPS Landing System," U.S. patent No. 6178363
    • McIntyre, M., Anderson, A., "Inertially Augmented GPS Landing System," U.S. patent No. 6178363.
    • McIntyre, M.1    Anderson, A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.