메뉴 건너뛰기




Volumn 2, Issue , 2004, Pages 1006-1018

Dynamic inversion based control concept with application to an unmanned aerial vehicle

Author keywords

[No Author keywords available]

Indexed keywords

DYNAMIC INVERSION; NONLINEAR SIMULATION; PSEUDO-CONTROL HEDGING; UNMANNED AERIAL VEHICLE;

EID: 19644368255     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (32)

References (12)
  • 1
    • 85087192694 scopus 로고    scopus 로고
    • Flight testing of a reconfigurable flight control law for the X-36 tailless fighter aircraft
    • AIAA-2000-3941, Denver, CO, August
    • Brinker, J. S. and Wise, K. A.: Flight Testing of a Reconfigurable Flight Control Law for the X-36 Tailless Fighter Aircraft. AIAA-2000-3941. AIAA Guidance, Navigation, and Control Conference, Denver, CO, August 2000.
    • (2000) AIAA Guidance, Navigation, and Control Conference
    • Brinker, J.S.1    Wise, K.A.2
  • 2
    • 85078724392 scopus 로고    scopus 로고
    • Adaptive flight control for an autonomous unmanned helicopter
    • AIAA-2002-4439, Monterey, CA, August
    • Johnson, E. N. and Kannan, S. K.: Adaptive Flight Control for an Autonomous Unmanned Helicopter. AIAA-2002-4439. AIAA Guidance, Navigation, and Control Conference, Monterey, CA, August 2002.
    • (2002) AIAA Guidance, Navigation, and Control Conference
    • Johnson, E.N.1    Kannan, S.K.2
  • 3
    • 19644374248 scopus 로고
    • A formal structure for advanced automatic flight-control systems
    • NASA Ames Research Center, Moffet Field, CA, May
    • Meyer, G. and Cicolani, L.: A Formal Structure for Advanced Automatic Flight-Control Systems. NASA Technical Note TN D-7940. NASA Ames Research Center, Moffet Field, CA, May 1975.
    • (1975) NASA Technical Note , vol.TN D-7940
    • Meyer, G.1    Cicolani, L.2
  • 4
    • 19644397818 scopus 로고    scopus 로고
    • The Unmanned Flying Testbed (UFT) - A research vehicle for handling of UAV and the test of novel flight control techniques
    • Ankara, Turkey, October
    • Hertzog, M., Schmitt, D. and Wagner, O.: The Unmanned Flying Testbed (UFT) - A research vehicle for handling of UAV and the test of novel flight control techniques. RTO-Symposium AVT-49. Ankara, Turkey, October 2000.
    • (2000) RTO-symposium , vol.AVT-49
    • Hertzog, M.1    Schmitt, D.2    Wagner, O.3
  • 6
    • 85087593384 scopus 로고    scopus 로고
    • Application of an optimization-based design process for robust autoland control laws
    • AIAA-2001-4206. Montreal, Canada, August
    • Looye, G., Joos, H.-D. and Willemsen, D.: Application of an Optimization-based Design Process for Robust Autoland Control Laws. AIAA-2001-4206. AIAA Guidance, Navigation, and Control Conference. Montreal, Canada, August 2001.
    • (2001) AIAA Guidance, Navigation, and Control Conference
    • Looye, G.1    Joos, H.-D.2    Willemsen, D.3
  • 10
    • 19644400434 scopus 로고
    • Total Energy Based Flight Control System. U.S. Patent No. 4,536,843. August
    • Lambregts, A. A.: Total Energy Based Flight Control System. U.S. Patent No. 4,536,843. August 1985.
    • (1985)
    • Lambregts, A.A.1
  • 12
    • 0142258149 scopus 로고    scopus 로고
    • PhD Thesis. Georgia Institute of Technology, Atlanta, GA
    • Rysdyk, R.: Adaptive Nonlinear Flight Control. PhD Thesis. Georgia Institute of Technology, Atlanta, GA, 1998.
    • (1998) Adaptive Nonlinear Flight Control
    • Rysdyk, R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.