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Volumn , Issue , 2009, Pages

Identification and integration of ornithopter actuator models

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; EQUATIONS OF STATE; FLIGHT DYNAMICS; MAXIMUM LIKELIHOOD; RELIGIOUS BUILDINGS; RESEARCH AIRCRAFT; STATE SPACE METHODS; TIME DOMAIN ANALYSIS;

EID: 77958158611     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-5937     Document Type: Conference Paper
Times cited : (7)

References (14)
  • 1
    • 60349093721 scopus 로고    scopus 로고
    • Inertial measurements from flight data of a flapping-wing ornithopter
    • January-February
    • Grauer, J. and Hubbard, J., "Inertial Measurements from Flight Data of a Flapping-Wing Ornithopter," Journal of Guidance, Control, and Dynamics, Vol. 32, No. 1, January-February 2009, pp. 326-331.
    • (2009) Journal of Guidance, Control, and Dynamics , vol.32 , Issue.1 , pp. 326-331
    • Grauer, J.1    Hubbard, J.2
  • 5
    • 0030105517 scopus 로고    scopus 로고
    • Effect of actuator nonlinearities on aeroservoelasticity
    • March-April
    • Taylor, R., Pratt, R., and Caldwell, B., "Effect of Actuator Nonlinearities on Aeroservoelasticity," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 2, March-April 1996, pp. 309-315.
    • (1996) Journal of Guidance, Control, and Dynamics , vol.19 , Issue.2 , pp. 309-315
    • Taylor, R.1    Pratt, R.2    Caldwell, B.3
  • 6
    • 0026111024 scopus 로고
    • Effect of motor dynamics on nonlinear feedback robot arm control
    • February
    • Tarn, T.-J., Bejczy, A., Yun, X., and Li, Z., "Effect of Motor Dynamics on Nonlinear Feedback Robot Arm Control," IEEE Transactions on Robotics and Automation, Vol. 7, No. 1, February 1991, pp. 114-122.
    • (1991) IEEE Transactions on Robotics and Automation , vol.7 , Issue.1 , pp. 114-122
    • Tarn, T.-J.1    Bejczy, A.2    Yun, X.3    Li, Z.4
  • 10
    • 0022736591 scopus 로고
    • Application of parameter estimation to aircraft stability and control: The output-error approach
    • Maine, R. and Illif, K., "Application of Parameter Estimation to Aircraft Stability and Control: The Output-Error Approach," Tech. Rep. NASA RP 1168, NASA, 1986.
    • (1986) Tech. Rep. NASA RP 1168, NASA
    • Maine, R.1    Illif, K.2
  • 11
    • 29344463548 scopus 로고    scopus 로고
    • Aircraft system idenfication: Theory and practice
    • AIAA
    • Klein, V. and Morelli, E., Aircraft System Idenfication: Theory and Practice, AIAA Education Series, AIAA, 2006.
    • (2006) AIAA Education Series
    • Klein, V.1    Morelli, E.2
  • 12
    • 77958168504 scopus 로고
    • Determination of airplane model structure from flight data by using modified stepwise regression
    • Klein, V., Batterson, J., and Murphy, P., "Determination of Airplane Model Structure From Flight Data by Using Modified Stepwise Regression," Tech. Rep. NASA Technical Paper 1916, NASA, 1986.
    • (1986) Tech. Rep. NASA Technical Paper 1916, NASA
    • Klein, V.1    Batterson, J.2    Murphy, P.3
  • 13
    • 0030833069 scopus 로고    scopus 로고
    • Accuracy of aerodynamic model parameters estimated from flight test data
    • January-February
    • Morelli, E. and Klein, V., "Accuracy of Aerodynamic Model Parameters Estimated from Flight Test Data," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 1, January-February 1997, pp. 74-80.
    • (1997) Journal of Guidance, Control, and Dynamics , vol.20 , Issue.1 , pp. 74-80
    • Morelli, E.1    Klein, V.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.