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Volumn , Issue , 1998, Pages 1911-1918

Design, implementation, testing, and flight results of the TRMM Kalman filter

Author keywords

[No Author keywords available]

Indexed keywords

BANDPASS FILTERS; KALMAN FILTERS; ORBITS; RAIN; SOFTWARE TESTING; SPACE FLIGHT; SPACECRAFT; VERIFICATION;

EID: 60349123856     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (5)

References (9)
  • 7
    • 85003406366 scopus 로고
    • Analytical steady-state accuracy solution for two common spacecraft attitude estimators
    • July-Aug
    • Farrenkopf, R. L., "Analytical Steady-State Accuracy Solution for Two Common Spacecraft Attitude Estimators", Journal of Guidance and Control, Vol. 1, No. 4, July-Aug, 1978. pp. 282-284.
    • (1978) Journal of Guidance and Control , vol.1 , Issue.4 , pp. 282-284
    • Farrenkopf, R.L.1
  • 9
    • 0346098488 scopus 로고    scopus 로고
    • Development, implementation, and testing of the TRMM kalman filter
    • Andrews, S. F., D'Agostino, J. M., "Development, Implementation, and Testing of the TRMM Kalman Filter", Flight Mechanics Symposium, 1997.
    • (1997) Flight Mechanics Symposium
    • Andrews, S.F.1    D'Agostino, J.M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.