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Volumn 26, Issue 2, 2003, Pages 354-362

Low-order equivalent system identification for the Tu-144LL supersonic transport aircraft

Author keywords

[No Author keywords available]

Indexed keywords

BODE DIAGRAMS; ERROR ANALYSIS; FLIGHT DYNAMICS; FOURIER TRANSFORMS; FREQUENCY DOMAIN ANALYSIS; FREQUENCY RESPONSE; LAPLACE TRANSFORMS; LEAST SQUARES APPROXIMATIONS; MATHEMATICAL MODELS; SPECTRUM ANALYSIS; SUPERSONIC AIRCRAFT; TRANSPORT AIRCRAFT;

EID: 0037352177     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.5053     Document Type: Article
Times cited : (33)

References (17)
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    • (2000)
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  • 2
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    • Identification of low order equivalent system models from flight test data
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    • Morelli, E.A.1
  • 3
    • 0003409960 scopus 로고
    • Aircraft parameter estimation in frequency domain
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    • (1978)
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  • 4
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    • Military standard - Flying qualities of piloted aircraft
    • MIL-STD-1797A, Jan.
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  • 5
    • 0016917683 scopus 로고
    • Handling qualities of aircraft with stability and control augmentation systems - A fundamental approach
    • Feb.
    • Hodgkinson, J., LaManna, W. J., and Heyde, J. L., "Handling Qualities of Aircraft with Stability and Control Augmentation Systems - A Fundamental Approach," Aeronautical Journal, Vol. 80, No. 782, Feb. 1976, pp. 75-81.
    • (1976) Aeronautical Journal , vol.80 , Issue.782 , pp. 75-81
    • Hodgkinson, J.1    Lamanna, W.J.2    Heyde, J.L.3
  • 6
    • 0020175515 scopus 로고
    • Low-order approaches to high-order systems: Problems and promises
    • Mitchell, D. G., and Hoh, R. H., "Low-Order Approaches to High-Order Systems: Problems and Promises," Journal of Guidance, Control, and Dynamics, Vol. 5, No. 5, 1982, pp. 482-489.
    • (1982) Journal of Guidance, Control, and Dynamics , vol.5 , Issue.5 , pp. 482-489
    • Mitchell, D.G.1    Hoh, R.H.2
  • 7
    • 22944455835 scopus 로고
    • Equivalent system verification and evaluation of augmentation effects on fighter approach and landing flying qualities
    • AFWAL-TR-81-3116, Sept.
    • Hodgkinson, J., Snyder, R. C., and Smith, R. E., "Equivalent System Verification and Evaluation of Augmentation Effects on Fighter Approach and Landing Flying Qualities," AFWAL-TR-81-3116, Sept. 1981.
    • (1981)
    • Hodgkinson, J.1    Snyder, R.C.2    Smith, R.E.3
  • 8
    • 13344275882 scopus 로고    scopus 로고
    • A qualitative piloted evaluation of the tupolev Tu-144 supersonic transport
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    • (2000)
    • Rivers, R.A.1    Jackson, E.B.2    Fullerton, C.G.3    Cox, T.H.4    Princen, N.H.5
  • 9
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    • High accuracy evaluation of the finite fourier transform using sampled data
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    • Morelli, E. A., "High Accuracy Evaluation of the Finite Fourier Transform Using Sampled Data," NASA TM 110340, June 1997.
    • (1997)
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  • 10
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    • Frequency-response method for rotorcraft system identification: Flight applications to BO-105 coupled rotor/Fuselage dynamics
    • Tischler, M. B., and Cauffman, M. G., "Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO-105 Coupled Rotor/Fuselage Dynamics," Journal of the American Helicopter Society, Vol. 37, No. 3, 1992, pp. 3-17.
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  • 13
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    • Application of parameter estimation to aircraft stability and control - The output-error approach
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  • 14
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    • NASA CR 194893, March
    • Morelli, E. A., and Klein, V., "Determining the Accuracy of Maximum Likelihood Parameter Estimates with Colored Residuals," NASA CR 194893, March 1994.
    • (1994)
    • Morelli, E.A.1    Klein, V.2
  • 15
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    • NASA TM 89059, Jan.
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    • (1987)
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  • 16
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    • (2002)
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  • 17
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.