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Volumn 28, Issue 4, 1992, Pages 1068-1075

Observability Analysis of Piecewise Constant Systems Part II: Application to Inertial Navigation In-Flight Alignment

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Indexed keywords


EID: 70249083660     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.165368     Document Type: Article
Times cited : (235)

References (13)
  • 2
    • 84912180470 scopus 로고
    • Application of Kalman filtering to the C-5 guidance and control system
    • AGARD, Paris, France, Astia Document 704 306, 1970.
    • Schmidt, S.F., Weinberg, J.D., and Lukesh, J.S. (1970) Application of Kalman filtering to the C-5 guidance and control system. In Theory and Applications of Kalman Filtering, AGARD, Paris, France, Astia Document 704 306, 1970.
    • (1970) Theory and Applications of Kalman Filtering
    • Schmidt, S.F.1    Weinberg, J.D.2    Lukesh, J.S.3
  • 3
    • 84948589864 scopus 로고
    • Engineering technical report KD-73–9, The Singer Company Kearfott Division, 1973.
    • Danik, B. (1973) Gyrocompass alignment of inertial platforms. Engineering technical report KD-73–9, The Singer Company Kearfott Division, 1973.
    • (1973) Gyrocompass alignment of inertial platforms.
    • Danik, B.1
  • 4
    • 85003341560 scopus 로고
    • The Kalman filter in transfer alignment of inertial guidance systems
    • (1968)
    • Sutherland, A.A., Jr. (1968) The Kalman filter in transfer alignment of inertial guidance systems. Journal of Spacecraft and Rockets, 5 (1968), 1175–1180.
    • (1968) Journal of Spacecraft and Rockets , vol.5 , pp. 1175-1180
    • Sutherland, A.A.1
  • 5
    • 0015361176 scopus 로고
    • In-flight alignment and calibration of inertial measurement units-Part I: General formulation
    • (1972)
    • Baziw, J., and Leondes, C.T. (1972) In-flight alignment and calibration of inertial measurement units-Part I: General formulation. IEEE Transactions on Aerospace and Electronic Systems, AES-8 (1972), 440–449.
    • (1972) IEEE Transactions on Aerospace and Electronic Systems , vol.AES-8 , pp. 440-449
    • Baziw, J.1    Leondes, C.T.2
  • 6
    • 0019585124 scopus 로고
    • Effect of acceleration switching during INS in-flight alignment
    • (1981)
    • Porat, B., and Bar-Itzhack, I.Y. (1981) Effect of acceleration switching during INS in-flight alignment. Journal of Guidance and Control, 4 (1981), 385–389.
    • (1981) Journal of Guidance and Control , vol.4 , pp. 385-389
    • Porat, B.1    Bar-Itzhack, I.Y.2
  • 7
    • 0019043994 scopus 로고
    • Azimuth observability enhancement during inertial navigation system in-flight alignment
    • (1981)
    • Bar-Itzhack, I.Y., and Porat, B. (1981) Azimuth observability enhancement during inertial navigation system in-flight alignment. Journal of Guidance and Control, 3 (1981), 337–344.
    • (1981) Journal of Guidance and Control , vol.3 , pp. 337-344
    • Bar-Itzhack, I.Y.1    Porat, B.2
  • 9
    • 0005923245 scopus 로고
    • Inertial guidance of cruise vehicles
    • C.T. Leondes (Ed.), New York: McGraw-Hill, 1963, ch. 4.
    • Pinson, J.C. (1963) Inertial guidance of cruise vehicles. In C.T. Leondes (Ed.), Guidance and Control of Aerospace Vehicles. New York: McGraw-Hill, 1963, ch. 4.
    • (1963) Guidance and Control of Aerospace Vehicles.
    • Pinson, J.C.1
  • 11
    • 0016535817 scopus 로고
    • A comparison of two approaches to pure-inertial and Doppler-inertial error analysis
    • (July 1975)
    • Benson, D.O., Jr. (1975) A comparison of two approaches to pure-inertial and Doppler-inertial error analysis. IEEE Transactions on Aerospace and Electronic Systems, AES-11 (July 1975), 447–455.
    • (1975) IEEE Transactions on Aerospace and Electronic Systems , vol.AES-11 , pp. 447-455
    • Benson, D.O.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.