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Volumn 6166, Issue , 2006, Pages

Non-linear controls influence functions in an aircraft dynamics simulator

Author keywords

Aerodynamic coefficients; Dynamics; Influence functions; Morphing; Simulation; Stability derivatives; UAV

Indexed keywords

ALGORITHMS; COMPUTER SIMULATION; FUNCTION EVALUATION; INFORMATION RETRIEVAL; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; UNMANNED VEHICLES; WINGS;

EID: 33745856604     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.658488     Document Type: Conference Paper
Times cited : (3)

References (7)
  • 2
    • 0003673079 scopus 로고    scopus 로고
    • American Institute of Aeronautics and Astronautics, Inc., Reston, VA
    • nd Edition, American Institute of Aeronautics and Astronautics, Inc., Reston, VA, 2004.
    • (2004) nd Edition
    • Pamadi, B.N.1
  • 4
    • 84896840107 scopus 로고    scopus 로고
    • Investigating segmented trailing-edge surfaces for full authority control of a UAV
    • AIAA-2003-5312, Austin, TX, August
    • Abdulrahim, M., and Lind, R., "Investigating Segmented Trailing-Edge Surfaces for Full Authority Control of a UAV," AIAA Atmospheric Flight Mechanics Conference, AIAA-2003-5312, Austin, TX, August 2003.
    • (2003) AIAA Atmospheric Flight Mechanics Conference
    • Abdulrahim, M.1    Lind, R.2
  • 6
    • 2942703856 scopus 로고    scopus 로고
    • Flight dynamics and control of an aircraft with segmented control surfaces
    • AIAA-2004-128, Reno, NV, January
    • Abdulrahim, M., "Flight Dynamics and Control of an Aircraft With Segmented Control Surfaces," 42nd AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2004-128, Reno, NV, January 2004.
    • (2004) 42nd AIAA Aerospace Sciences Meeting and Exhibit
    • Abdulrahim, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.