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Volumn 143, Issue 2, 1996, Pages 209-216

Analysis of stabilised output error methods

Author keywords

Aircraft stability; Output error methods; Simulation

Indexed keywords

AERODYNAMICS; AIRCRAFT; ASYMPTOTIC STABILITY; COMPUTER SIMULATION; DIFFERENTIAL EQUATIONS; ERROR CORRECTION; LINEAR CONTROL SYSTEMS; MATRIX ALGEBRA; REGRESSION ANALYSIS; SYSTEM STABILITY; VECTORS;

EID: 0030109314     PISSN: 13502379     EISSN: None     Source Type: Journal    
DOI: 10.1049/ip-cta:19960195     Document Type: Article
Times cited : (8)

References (15)
  • 5
    • 84962196836 scopus 로고
    • Estimation of aircraft performance and stability characteristics by dynamic manoeuvres using maximum likelihood estimation techniques
    • Pre-prints Budapest, Hungary, 8-12 July
    • GOPALRATNAM, G., PARAMESWARAN, V., RAOL, J.R., and BALAKRISHNA, S.: 'Estimation of aircraft performance and stability characteristics by dynamic manoeuvres using maximum likelihood estimation techniques', Pre-prints of 9th IFAC/IFORS Symposium on Identification and system parameter estimation, Budapest, Hungary, 8-12 July 1991
    • (1991) 9th IFAC/IFORS Symposium on Identification and System Parameter Estimation
    • Gopalratnam, G.1    Parameswaran, V.2    Raol, J.R.3    Balakrishna, S.4
  • 7
    • 0022736591 scopus 로고
    • Application of parameter estimation to aircraft stability and control - The output error approach
    • MAINE, R.E., and ILIFF, K.W.: 'Application of parameter estimation to aircraft stability and control - the output error approach', NASA RP 1168, 1986
    • (1986) NASA RP , vol.1168
    • Maine, R.E.1    Iliff, K.W.2
  • 8
    • 0024000852 scopus 로고
    • Application of parameter estimation to highly unstable aircraft
    • MAINE, R.E., and MURRAY, J.E.: 'Application of parameter estimation to highly unstable aircraft', J. Guid. Control Dyn., 1988, 11, (3), pp. 213-219
    • (1988) J. Guid. Control Dyn. , vol.11 , Issue.3 , pp. 213-219
    • Maine, R.E.1    Murray, J.E.2
  • 9
    • 0026106811 scopus 로고
    • Equation decoupling - A new approach to the aerodynamic identification of unstable aircraft
    • PREISSLER, H., and SCHAUFELE, H.: 'Equation decoupling - a new approach to the aerodynamic identification of unstable aircraft', J. Aircr., 1991, 28, (2), pp. 146-150
    • (1991) J. Aircr. , vol.28 , Issue.2 , pp. 146-150
    • Preissler, H.1    Schaufele, H.2
  • 13
    • 0029369958 scopus 로고
    • Estimation of parameters of unstable, and augmented aircraft system using recursive mixed estimation technique
    • GOPALRATNAM, G., and RAOL, J.R.: 'Estimation of parameters of unstable, and augmented aircraft system using recursive mixed estimation technique', J. Inst. Eng. Aerosp. Div., 1995, 76, pp. 15-22
    • (1995) J. Inst. Eng. Aerosp. Div. , vol.76 , pp. 15-22
    • Gopalratnam, G.1    Raol, J.R.2
  • 14
    • 0024930671 scopus 로고
    • Estimation of aircraft aerodynamic parameters from flight data
    • KLEIN V.: 'Estimation of aircraft aerodynamic parameters from flight data', Prog. Aerosp. Sci., 1989, 26, pp. 1-77
    • (1989) Prog. Aerosp. Sci. , vol.26 , pp. 1-77
    • Klein, V.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.