Accurate ins transfer alignment using a monitor gyro and external navigation measurements

IEEE Transactions on Aerospace and Electronic Systems

Volumn AES-16, Issue 1, 1980, Pages 53-65

  Bar Itzhack, Itzhack Y ^a   Mallove, Eugene F ^a  

^a Analytic Sciences Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NAVIGATION;

EID: 0018919924     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.1980.308876     Document Type: Article

References (13)

1. A.A. Sutherland, Jr., “The Kalman filter in transfer alignment of inertial guidance systems”, J. Space. Rockets, vol. 5, pp. 1175-1180, Oct. 1968.
2. R.L. Doty and R.F. Nease, “Initial condition and alignment”, in Inertial Guidance, G.R. Pitman, Ed. New York: Wiley, 1962, pp. 176-209.
3. J.C. Pinson, “Inertial guidance for cruise vehicles”, in Guidance and Control of Aerospace Vehicles, C.T. Leondes, Ed. New York: McGraw-Hill, 1963, pp. 113-187.
4. F.D. Jurenka and C.T. Leondes, “Optimum alignment of an inertial autonavigator”, IEEE Trans. Aerosp. Electron. Syst., vol. AES-3, pp. 880-888, Nov. 1967.
5. B. Danik, “Gyrocompass alignment of inertial platforms”, The Singer Company Kearfott Division, Engineering Tech. Rep. KD-73-9, Feb. 1973.
6. J.J. Deyst, Jr. and A.A. Sutherland, Jr., “Strapdown inertial system alignment using statistical filters: A simplified formulation”, AIAA J., vol. 11, pp. 452-456, Apr. 1973.
7. J. Baziw and C.T. Leondes, “In-flight alignment and calibration of inertial measurement units-Part I: General formulation”, IEEE Trans. Aerosp. Electron. Syst., vol. AES-8, pp. 439-449, July 1972.
8. C.M. Venegas, “Alignment performance of an inertial navigation system in a low level seismic environment”, in AIAA Guidance and Control Conf. Proc, Aug. 1977, pp. 316-322.
9. L.L. Rosen, “Concepts of gyro monitoring as applied to long term inertial navigation”, Proc. Internal. Conf. Military Electronics, Sept. 1964, pp. 193-197.
10. A. Gelb, “Synthesis of a very accurate inertial navigation system”, IEEE Trans. Aerosp. Navig. Electron., vol. 12, pp. 119-128, June 1965.
11. C. Broxmeyer, Inertial Navigation Systems. New York: McGraw-Hill, 1964.
12. A.A. Sutherland, Jr. and A. Gelb, “Application of the Kalman filter to aided inertial systems”, The Analytic Sciences Corporation (TASC), Reading, MA, Tech. Rep. TR-134-1, Oct. 1967.
13. D.O. Benson, Jr., “A comparison of two approaches to pure-inertial and Doppler-inertial error analysis”, IEEE Trans. Aerosp. Electron. Syst., vol. AES-11, pp. 447-455, July 1975.