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Volumn , Issue , 2009, Pages

Aerodynamic hinge moment coefficient estimation using automatic fly-by-wire control inputs

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AILERONS; ELEVATORS; FLIGHT CONTROL SYSTEMS;

EID: 77958188731     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-5692     Document Type: Conference Paper
Times cited : (19)

References (25)
  • 13
    • 29744431933 scopus 로고    scopus 로고
    • Output error method and two step method for aerodynamic model identification
    • Keystone Colorado, No. AIAA-2005-6440, American Institute of Aeronautics and Astronautics
    • Oliveira, J., Chu, Q. P., Mulder, J. A., Balini, H., and Vos, W., "Output Error Method and Two Step Method for Aerodynamic Model Identification, " AIAA Guidance, Navigation and Control conference and Exhibit, Keystone Colorado, No. AIAA-2005-6440, American Institute of Aeronautics and Astronautics, 2005.
    • (2005) AIAA Guidance, Navigation and Control Conference and Exhibit
    • Oliveira, J.1    Chu, Q.P.2    Mulder, J.A.3    Balini, H.4    Vos, W.5
  • 15
    • 0016339217 scopus 로고
    • Optimal input signals for parameter estimation in dynamic systems-Survey and new results
    • IEEE
    • Mehra, R. K., "Optimal input signals for parameter estimation in dynamic systems-Survey and new results, " IEEE Transactions on Automatic Control, Vol. 19, IEEE, 1974, pp. 753-768.
    • (1974) IEEE Transactions on Automatic Control , vol.19 , pp. 753-768
    • Mehra, R.K.1
  • 16
    • 85006385058 scopus 로고
    • Flight investigation of various control inputs intended for parameter estimation
    • Shafer, M. F., "Flight investigation of various control inputs intended for parameter estimation, " Tech. Rep. Technical Memorandum 85901, NASA, 1984.
    • (1984) Tech. Rep. Technical Memorandum 85901, NASA
    • Shafer, M.F.1
  • 17
    • 84983127144 scopus 로고    scopus 로고
    • Flight test validation of imal input design and comparison to conventional inputs
    • New Orleans, Louisiana, No. AIAA-97-3711
    • Morelli, E. A., "Flight Test Validation of imal Input Design and Comparison to Conventional Inputs, " AIAA Atmospheric Flight Mechanics Conference, New Orleans, Louisiana, No. AIAA-97-3711, 1997.
    • (1997) AIAA Atmospheric Flight Mechanics Conference
    • Morelli, E.A.1
  • 20
    • 67651149249 scopus 로고
    • Identification of dynamic systems - Applications to aircraft Part 2: Nonlinear analysis and manoeuvre design
    • North Atlantic Treaty Organization, May
    • Mulder, J. A., Sridhar, J. K., and Breeman, J. H., "Identification of Dynamic Systems - Applications to Aircraft Part 2: Nonlinear Analysis and Manoeuvre Design, " Tech. Rep. AGARD AG-300, Flight Test Techniques Series - Volume 3, North Atlantic Treaty Organization, May 1994.
    • (1994) Tech. Rep. AGARD AG-300, Flight Test Techniques Series , vol.3
    • Mulder, J.A.1    Sridhar, J.K.2    Breeman, J.H.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.