메뉴 건너뛰기




Volumn 31, Issue 4, 2008, Pages 1166-1176

Simple real-time stabilization of vertical takeoff and landing aircraft with bounded signals

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; AIRCRAFT LANDING; ALTITUDE CONTROL; CLOSED LOOP SYSTEMS; CONTROLLERS; FREE FLIGHT; HELICOPTER ROTORS; STABILIZATION; TAKEOFF;

EID: 48849105346     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.32157     Document Type: Article
Times cited : (21)

References (12)
  • 4
    • 0026896517 scopus 로고
    • Nonlinear Control Design for Slightly Nonminimum Phase Systems: Application to V/STOL Aircraft
    • doi:10.1016/0005-1098(92) 90029-F
    • Hauser, J., Sastry, S., and Meyer, G., "Nonlinear Control Design for Slightly Nonminimum Phase Systems: Application to V/STOL Aircraft," Automatica, Vol. 28, No. 4, 1992, pp. 665-679. doi:10.1016/0005-1098(92) 90029-F
    • (1992) Automatica , vol.28 , Issue.4 , pp. 665-679
    • Hauser, J.1    Sastry, S.2    Meyer, G.3
  • 5
    • 0036027518 scopus 로고    scopus 로고
    • Autonomous Vertical Landing on an Oscillating Platform: An Internal-Model Based Approach
    • Jan, doi:10.1016/S0005- 1098(01)00184-4
    • Marconi, L., Isidori, A., and Serrani, A., "Autonomous Vertical Landing on an Oscillating Platform: An Internal-Model Based Approach," Automatica, Vol. 38, No. 1, Jan. 2002, pp. 21-32. doi:10.1016/S0005- 1098(01)00184-4
    • (2002) Automatica , vol.38 , Issue.1 , pp. 21-32
    • Marconi, L.1    Isidori, A.2    Serrani, A.3
  • 7
    • 0024656129 scopus 로고
    • Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations
    • Wie, B., Weiss, H., and Arapostathis, A., "Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations," Journal of Guidance, Control, and Dynamics, Vol. 12, No. 3, 1989, pp. 375-380.
    • (1989) Journal of Guidance, Control, and Dynamics , vol.12 , Issue.3 , pp. 375-380
    • Wie, B.1    Weiss, H.2    Arapostathis, A.3
  • 8
    • 84977389734 scopus 로고
    • A New Method for Performing Digital Control System Attitude Computations Using Quaternions
    • Ickes, B. P., "A New Method for Performing Digital Control System Attitude Computations Using Quaternions," AIAA Journal, Vol. 8, No. 1, 1970, pp. 13-17.
    • (1970) AIAA Journal , vol.8 , Issue.1 , pp. 13-17
    • Ickes, B.P.1
  • 9
    • 0015599953 scopus 로고
    • Solution of Kinematical Differential Equations for a Rigid Body
    • Kane, T. R., "Solution of Kinematical Differential Equations for a Rigid Body," Journal of Applied Mechanics, Vol. 40, No. 1, 1973, pp. 109-113.
    • (1973) Journal of Applied Mechanics , vol.40 , Issue.1 , pp. 109-113
    • Kane, T.R.1
  • 11
    • 4344615677 scopus 로고    scopus 로고
    • Control of Nonlinear Mechanical Underactuated Systems
    • Springer-Verlag, Berlin/New York/Heidelberg
    • Fantoni, I., and Lozano, R., Control of Nonlinear Mechanical Underactuated Systems, Communications and Control Engineering Series, Springer-Verlag, Berlin/New York/Heidelberg, 2001.
    • (2001) Communications and Control Engineering Series
    • Fantoni, I.1    Lozano, R.2
  • 12
    • 0034438553 scopus 로고    scopus 로고
    • Global Configuration Stabilization for the VTOL Aircraft with Strong Input Coupling
    • Inst. of Electrical and Electronics Engineers, Piscataway, NJ
    • Olfati-Saber, R., "Global Configuration Stabilization for the VTOL Aircraft with Strong Input Coupling," Proceedings of the 39th IEEE Conf. on Decision and Control, Vol. 4, Inst. of Electrical and Electronics Engineers, Piscataway, NJ, 2000, pp. 3588-3589.
    • (2000) Proceedings of the 39th IEEE Conf. on Decision and Control , vol.4 , pp. 3588-3589
    • Olfati-Saber, R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.