메뉴 건너뛰기




Volumn 8, Issue , 2006, Pages 4917-4928

Preliminary modeling, control, and trajectory design for miniature autonomous tailsitters

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MODEL; ATTITUDE CONTROL; FIXED WING AIRCRAFTS; TAILSITTERS;

EID: 33845736448     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (38)

References (18)
  • 1
    • 33845762197 scopus 로고    scopus 로고
    • The single-propeller driven tailsitter is the simplest and most efficient configuration for the VTOL UAV's
    • K. Wernicke. "The single-propeller driven tailsitter is the simplest and most efficient configuration for the VTOL UAV's," in International Powered Lift Conference, 2000.
    • (2000) International Powered Lift Conference
    • Wernicke, K.1
  • 2
    • 33745195256 scopus 로고    scopus 로고
    • Control of a vtol aircraft: Motion planning and trajectory tracking
    • A. Ailon, "Control of a vtol aircraft: Motion planning and trajectory tracking." in Mediterranean Conference on Control and Automation, 2005, pp. 1493-1498.
    • (2005) Mediterranean Conference on Control and Automation , pp. 1493-1498
    • Ailon, A.1
  • 3
    • 0028738687 scopus 로고
    • A different look at output tracking: Control of a VTOL aircraft
    • P. Martin, S. Devasia, and B. Paden. "A different look at output tracking: control of a VTOL aircraft," in Conference on Decision and Control. 1994, pp. 2376-2381.
    • (1994) Conference on Decision and Control , pp. 2376-2381
    • Martin, P.1    Devasia, S.2    Paden, B.3
  • 4
    • 16244422345 scopus 로고    scopus 로고
    • Control architecture for a tail-sitter unmanned air vehicle
    • R. Stone, "Control architecture for a tail-sitter unmanned air vehicle," in 5th Asian Control Conference, 2004, pp. 736-744.
    • (2004) 5th Asian Control Conference , pp. 736-744
    • Stone, R.1
  • 5
    • 11244252131 scopus 로고    scopus 로고
    • The T-wing tail-sitter unmanned air vehicle: From design concept to research flight vehicle
    • _, "The T-wing tail-sitter unmanned air vehicle: from design concept to research flight vehicle," in Proceedings of the I MECH E Part G Journal of Aerospace Engineering, 2004, pp. 417-433.
    • (2004) Proceedings of the I MECH E Part G Journal of Aerospace Engineering , pp. 417-433
  • 6
    • 33845782329 scopus 로고    scopus 로고
    • The T-wing: A VTOL UAV for defense and civilian applications
    • R. Stone and G. Clarke. "The T-wing: A VTOL UAV for defense and civilian applications." in UAV Australia Conference, 2001.
    • (2001) UAV Australia Conference
    • Stone, R.1    Clarke, G.2
  • 7
    • 33845741459 scopus 로고    scopus 로고
    • Optimization of transition maneuvers for a tail-sitter unmanned air vehicle (UAV)
    • _, "Optimization of transition maneuvers for a tail-sitter unmanned air vehicle (UAV)," in Australian International Aerospace Congress, 2001.
    • (2001) Australian International Aerospace Congress
  • 10
    • 0024656129 scopus 로고
    • Quaternion feedback regulator for spacecraft eigenaxis rotations
    • H. W. B.Wei and A. Arapostathis, "Quaternion feedback regulator for spacecraft eigenaxis rotations," AIAA Journal of Guidence and Control, vol. 12, no. 3, 1989.
    • (1989) AIAA Journal of Guidence and Control , vol.12 , Issue.3
    • Wei, H.W.B.1    Arapostathis, A.2
  • 11
    • 0029394180 scopus 로고
    • Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
    • A. G. K. S.M Joshi and J. T.-Y. Wen, "Robust attitude stabilization of spacecraft using nonlinear quaternion feedback," IEEE Transactions on Automatic Control, vol. 40, no. 10, 1995.
    • (1995) IEEE Transactions on Automatic Control , vol.40 , Issue.10
    • Joshi, A.G.K.S.M.1    Wen, J.T.-Y.2
  • 12
    • 0027685020 scopus 로고
    • Linearization of attitude-control error dynamics
    • Oct.
    • R. Bach and R. Paielli, "Linearization of attitude-control error dynamics," IEEE Transactions on Automatic Control, vol. 38, no. 10, Oct. 1993.
    • (1993) IEEE Transactions on Automatic Control , vol.38 , Issue.10
    • Bach, R.1    Paielli, R.2
  • 13
    • 0035389960 scopus 로고    scopus 로고
    • A review of attitude representations used for aircraft kinematics
    • W. Phillips, C. Hailey, and G. Gebert, "A review of attitude representations used for aircraft kinematics," Journal of Aircraft, vol. 38, no. 4, 2001.
    • (2001) Journal of Aircraft , vol.38 , Issue.4
    • Phillips, W.1    Hailey, C.2    Gebert, G.3
  • 16
    • 0013442405 scopus 로고
    • Aerodynamic characteristics of seven symmetrical airfoil sections through 180-degree angle of attack for use in aerodynamic analysis of vertical axis wind turbines
    • R. E. Sheldahl and P. C. Klimas, "Aerodynamic characteristics of seven symmetrical airfoil sections through 180-degree angle of attack for use in aerodynamic analysis of vertical axis wind turbines," Sandia National Laboratories, Tech. Rep. SAND80-2114, 1980.
    • (1980) Sandia National Laboratories, Tech. Rep. , vol.SAND80-2114
    • Sheldahl, R.E.1    Klimas, P.C.2
  • 17
    • 33845746132 scopus 로고    scopus 로고
    • http://www.hobby-lobby.com/pogo.htm.
  • 18
    • 33845783659 scopus 로고    scopus 로고
    • http://procerusuav.com/.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.