메뉴 건너뛰기




Volumn 2, Issue , 2007, Pages 1998-2008

Adaptive control laws for flexible semi-span wind tunnel model of high-aspect ratio flying wing

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DEGREES OF FREEDOM (MECHANICS); FEEDBACK; WIND TUNNELS;

EID: 37249076401     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-6525     Document Type: Conference Paper
Times cited : (16)

References (12)
  • 1
    • 28844460475 scopus 로고    scopus 로고
    • Lucia, D. J., The SensorCraft Configurations: A Nonlinear Aeroservoelastic Challenge for Aviation, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, No. AIAA-2005-1943, Austin, TX, April 2005.
    • Lucia, D. J., "The SensorCraft Configurations: A Nonlinear Aeroservoelastic Challenge for Aviation," 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, No. AIAA-2005-1943, Austin, TX, April 2005.
  • 2
    • 28844465435 scopus 로고    scopus 로고
    • Vartio, E., Shimko, A., Tilmann, C. P., and Flick, P. M., Structural Modal Control and Gust Load Alleviation for a SensorCraft Concept, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, No. AIAA-2005-1946, Austin, TX, April 2005.
    • Vartio, E., Shimko, A., Tilmann, C. P., and Flick, P. M., "Structural Modal Control and Gust Load Alleviation for a SensorCraft Concept," 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, No. AIAA-2005-1946, Austin, TX, April 2005.
  • 4
    • 84959095724 scopus 로고    scopus 로고
    • Modified Dynamic Inversion to Control Large Flexible Aircraft - What's Going On? AIAA Guidance
    • Portland, OR, August 9-11
    • Gregory, I. M. "Modified Dynamic Inversion to Control Large Flexible Aircraft - What's Going On?" AIAA Guidance, Navigation and Control Conference, No. AIAA99-3998, Portland, OR, August 9-11, 1999.
    • (1999) Navigation and Control Conference, No. AIAA99-3998
    • Gregory, I.M.1
  • 5
    • 33845774204 scopus 로고    scopus 로고
    • Design and Stability Analysis of Integrated Flight/Structural Mode Controller for Highly Flexible Advanced Aircraft Utilizing a Novel Nonlinear Dynamic Inversion
    • Ph.D. Thesis, California Institute of Technology
    • Gregory, I. M. "Design and Stability Analysis of Integrated Flight/Structural Mode Controller for Highly Flexible Advanced Aircraft Utilizing a Novel Nonlinear Dynamic Inversion." Ph.D. Thesis, California Institute of Technology, 2004.
    • (2004)
    • Gregory, I.M.1
  • 6
    • 85086351865 scopus 로고    scopus 로고
    • 1 Adaptive Controller, Part I: Control Signal and Asymptotic Stability. In Proc. of American Control Conference, 2006, pp. 3594-3599.
    • 1 Adaptive Controller, Part I: Control Signal and Asymptotic Stability." In Proc. of American Control Conference, 2006, pp. 3594-3599.
  • 7
    • 34047224087 scopus 로고    scopus 로고
    • 1 Adaptive Controller, Part II: Guaranteed Transient Performance. In Proc. of American Control Conference, 2006, pp. 3397-3402.
    • 1 Adaptive Controller, Part II: Guaranteed Transient Performance." In Proc. of American Control Conference, 2006, pp. 3397-3402.
  • 8
    • 46449123646 scopus 로고    scopus 로고
    • 1 Adaptive Controller for Systems with Unknown Time-Varying Parameters and Bounded Disturbances: Part I
    • 1 Adaptive Controller for Systems with Unknown Time-Varying Parameters and Bounded Disturbances: Part I" In Proc. of American Control Conference, 2007, pp. 3925-3930.
    • (2007) Proc. of American Control Conference , pp. 3925-3930
    • Cao, C.1    Hovakimyan, N.2
  • 9
    • 46449087256 scopus 로고    scopus 로고
    • Stability Margins of Lx Adaptive Controller: Part II
    • Cao, C. and Hovakimyan, N. "Stability Margins of Lx Adaptive Controller: Part II" In Proc. of American Control Conference, 2007, pp. 3931-3936.
    • (2007) Proc. of American Control Conference , pp. 3931-3936
    • Cao, C.1    Hovakimyan, N.2
  • 11
    • 0001009830 scopus 로고
    • Airplane Math Modeling and Active Aeroelastic Control Design
    • Roger, K.L., "Airplane Math Modeling and Active Aeroelastic Control Design", AGARD-CP-228, 1977, pp.4.1-4.11.
    • (1977) AGARD-CP-228
    • Roger, K.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.