메뉴 건너뛰기




Volumn 5, Issue 5, 1997, Pages 627-636

Drag coefficient curve identification of projectiles from flight tests via optimal dynamic fitting

Author keywords

curve fitting; data reduction; identification; optimal control

Indexed keywords

COMPUTATIONAL METHODS; CONVERGENCE OF NUMERICAL METHODS; CURVE FITTING; DATA REDUCTION; ITERATIVE METHODS; OPTIMAL CONTROL SYSTEMS; OPTIMIZATION; PARAMETER ESTIMATION; PROJECTILES;

EID: 0031148518     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(97)00044-0     Document Type: Article
Times cited : (14)

References (25)
  • 2
    • 0342635636 scopus 로고
    • A method for determination of aerodynamic drag by doppler data
    • Orlando, USA
    • Bartelson, N. (1975). A method for determination of aerodynamic drag by doppler data. In 'Proc. of the First Int. Ballistics Symp.'. Orlando, USA.
    • (1975) Proc. of the First Int. Ballistics Symp.
    • Bartelson, N.1
  • 3
    • 0014767878 scopus 로고
    • A method for extracting aerodynamic coefficients from free flight data
    • Chapman, G. T. and D. B. Kirk (1970). 'A method for extracting aerodynamic coefficients from free flight data'. AIAA Journal.
    • (1970) AIAA Journal
    • Chapman, G.T.1    Kirk, D.B.2
  • 4
    • 0343941709 scopus 로고
    • Researches on trajectory prediction models and software for spin-stabilized projectiles (I): Automatic model-switching trajectory prediction method
    • in Chinese
    • Chen, Y. (1990a). 'Researches on trajectory prediction models and software for spin-stabilized projectiles (I): Automatic model-switching trajectory prediction method'. Projectile and Rocket Fascicule of Acta Armamentarii 1990(3), 1-7 (in Chinese).
    • (1990) Projectile and Rocket Fascicule of Acta Armamentarii , vol.1990 , Issue.3 , pp. 1-7
    • Chen, Y.1
  • 5
    • 0343941709 scopus 로고
    • Researches on trajectory prediction models and software for spin-stabilized projectiles (II): Studies on trajectory prediction model reduction
    • in Chinese
    • Chen, Y. (19906). 'Researches on trajectory prediction models and software for spin-stabilized projectiles (II): Studies on trajectory prediction model reduction'. Projectile and Rocket Fascicule of Acta Armamentarii 1990(4), 1-11 (in Chinese).
    • (1990) Projectile and Rocket Fascicule of Acta Armamentarii , vol.1990 , Issue.4 , pp. 1-11
    • Chen, Y.1
  • 6
    • 0342635629 scopus 로고
    • Researches on trajectory prediction models and software for spin-stabilized projectiles (III) : A new rigid body 6-dof model for trajectory prediction of unguided spin missiles
    • in Chinese
    • Chen, Y. (1991). 'Researches on trajectory prediction models and software for spin-stabilized projectiles (III) : A new rigid body 6-dof model for trajectory prediction of unguided spin missiles'. Projectile and Rocket Fascicule of Acta Armamentarii 1991(1), 1-10 (in Chinese).
    • (1991) Projectile and Rocket Fascicule of Acta Armamentarii , vol.1991 , Issue.1 , pp. 1-10
    • Chen, Y.1
  • 7
    • 0343505930 scopus 로고
    • Data fitting algorithm and general purpose software by constrained multi-staged polynomials with different orders
    • in Chinese
    • Chen, Y. and H. Dou (1991). 'Data fitting algorithm and general purpose software by constrained multi-staged polynomials with different orders'. Aerodynamic Experiment and Measurement Control 5(3), 78-86 (in Chinese).
    • (1991) Aerodynamic Experiment and Measurement Control , vol.5 , Issue.3 , pp. 78-86
    • Chen, Y.1    Dou, H.2
  • 8
    • 0343505931 scopus 로고
    • Researches on the optimal control solution of identifying fitting drag coefficient curve from radar measured velocity data
    • in Chinese
    • Chen, Y. and H. Dou (1993a). 'Researches on the optimal control solution of identifying fitting drag coefficient curve from radar measured velocity data'. Aerodynamic Experiment and Measurement Control 1993(2), 81-89 (in Chinese).
    • (1993) Aerodynamic Experiment and Measurement Control , vol.1993 , Issue.2 , pp. 81-89
    • Chen, Y.1    Dou, H.2
  • 10
    • 0342635628 scopus 로고
    • Optimal dynamic fitting and identification of aerobomb's fitting drag coefficient curve
    • Dayton, Ohio, USA
    • Chen, Y., D. Lu, H. Dou and Y. Qing (1992). Optimal dynamic fitting and identification of aerobomb's fitting drag coefficient curve. In 'Proc. of the First IEEE Conf. on Control Applications'. Dayton, Ohio, USA. pp. 853-858.
    • (1992) Proc. of the First IEEE Conf. on Control Applications , pp. 853-858
    • Chen, Y.1    Lu, D.2    Dou, H.3    Qing, Y.4
  • 12
    • 0020504287 scopus 로고
    • Identification of aerodynamic coefficients using flight testing data
    • Fratter, C. and R. F. Stengel (1983). 'Identification of aerodynamic coefficients using flight testing data'. AIAA Paper No. 83-2099.
    • (1983) AIAA Paper No. 83-2099
    • Fratter, C.1    Stengel, R.F.2
  • 13
    • 84958069581 scopus 로고
    • Identification of aerodynamic indicial functions using flight data
    • Gupta, N. K. and K. W. Illif (1982). 'Identification of aerodynamic indicial functions using flight data'. AIAA Paper 82-1375.
    • (1982) AIAA Paper 82-1375
    • Gupta, N.K.1    Illif, K.W.2
  • 14
    • 0343941704 scopus 로고
    • Extraction of aerodynamic parameters for aircraft at extreme flight conditions
    • Illif, K. W. (1985). 'Extraction of aerodynamic parameters for aircraft at extreme flight conditions'. NASA-TM-86730 H-1290 NAS 1.15:86730 AGARD-PAPER-24 pp. 1-24.
    • (1985) NASA-TM-86730 H-1290 NAS 1.15:86730 AGARD-PAPER-24 , pp. 1-24
    • Illif, K.W.1
  • 15
    • 0024732403 scopus 로고
    • Parameter estimation for flight vehicle
    • Illif, K. W. (1989). 'Parameter estimation for flight vehicle'. AIAA Journal of Guidance and Control 12(5), 609-622.
    • (1989) AIAA Journal of Guidance and Control , vol.12 , Issue.5 , pp. 609-622
    • Illif, K.W.1
  • 16
    • 0343941703 scopus 로고
    • A bibliography for aircraft parameter estimation
    • Illif, K. W. and R. E. Maine (1986). 'A bibliography for aircraft parameter estimation'. NASA TM-86804.
    • (1986) NASA TM-86804
    • Illif, K.W.1    Maine, R.E.2
  • 18
  • 20
    • 0027698329 scopus 로고
    • Identification of aerodynamic coefficients using computational neural networks
    • Linse, D. J. and R. F. Stengel (1994). 'Identification of aerodynamic coefficients using computational neural networks'. Journal of Guidance, Control, and Dynamics 16(6), 1018-1025.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.16 , Issue.6 , pp. 1018-1025
    • Linse, D.J.1    Stengel, R.F.2
  • 22
    • 0024876655 scopus 로고
    • System identification collaboration - the role of AGARD
    • Peter, H. (1989). 'System identification collaboration - the role of AGARD'. Vertica 13(3), 207-212.
    • (1989) Vertica , vol.13 , Issue.3 , pp. 207-212
    • Peter, H.1
  • 23
    • 0343505927 scopus 로고
    • Determination of aerodynamic derivatives from transient responses in manoeuvring flight
    • Ross, A. J. (1975). 'Determination of aerodynamic derivatives from transient responses in manoeuvring flight'. AGARD Methods for Aircraft State and Parameter Identification pp. 1-10.
    • (1975) AGARD Methods for Aircraft State and Parameter Identification , pp. 1-10
    • Ross, A.J.1
  • 24
    • 0003766505 scopus 로고
    • Aerodynamic mathematical modeling basic concepts
    • Tobak, M. and L. B. Schiff (1981). 'Aerodynamic mathematical modeling basic concepts'. AGARD LS-114 paper 1.
    • (1981) AGARD LS-114 Paper 1
    • Tobak, M.1    Schiff, L.B.2
  • 25
    • 85003405733 scopus 로고
    • Instrument modeling for aerodynamic coefficient identification from flight test data
    • Williamson, W. E. J. (1980). 'Instrument modeling for aerodynamic coefficient identification from flight test data'. AIAA Journal of Guidance and Control 3(3), 225-279.
    • (1980) AIAA Journal of Guidance and Control , vol.3 , Issue.3 , pp. 225-279
    • Williamson, W.E.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.