Integrated Guidance and Control Design for the Near Space Interceptor

논문상세정보
' Integrated Guidance and Control Design for the Near Space Interceptor' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 항공우주공학, 우주항법학
  • backstepping sliding mode
  • finitetimedisturbanceobserver(ftdo)
  • integratedguidanceandcontrol(igc)
  • robust least-squares weighted control allocation (rlswca)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
468 0

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' Integrated Guidance and Control Design for the Near Space Interceptor' 의 참고문헌

  • Smooth second-order sliding modes: missile guidance application
    Shtessel, Y. Automatica 43 (8) : 1470 ~ 1476 [2007]
  • Robust solutions to least squares problems with uncertain data
    Ghaoui, L. SIAM Journal on Matrix Analysis and Applications 18 (4) : 1035 ~ 1064 [1997]
  • Robust autopilot design for bank-to-turn missiles using disturbance observers
    Li, S. IEEE Transactions on Aerospace and Electronic Systems 49 (1) : 558 ~ 579 [2013]
  • Research of integrated robust high order sliding mode guidance and control for missiles
    Dong, F. Acta Aeronautica et Astronautica Sinica 34 (9) : 2212 ~ 2218 [2013]
  • Partial integrated missile guidance and control with finite time convergence
    Wang, X. AIAA Journal of Guidance, Control and Dynamics 36 (5) : 1399 ~ 1409 [2013]
  • Partial integrated guidance and control for missiles with three-dimensional impact angle constraints
    Wang, X. AIAA Journal of Guidance, Control and Dynamics 37 (2) : 644 ~ 657 [2014]
  • Numerical state-dependent Riccati equation approach for missile integrated guidance control
    Vaddi, S. AIAA Journal of Guidance, Control and Dynamics 32 (2) : 699 ~ 703 [2009]
  • Nonlinear-disturbanceobserver-based robust flight control for airbreathing hypersonic vehicles
    Yang, J. IEEE Transactions on Aerospace and Electronic Systems 49 (2) : 1263 ~ 1275 [2013]
  • Nonlinear disturbance observer-enhanced dynamic inversion control of missiles
    Chen, W. AIAA Journal of Guidance, Control, and Dynamics 26 (1) : 161 ~ 166 [2003]
  • Integrated higherorder sliding mode guidance and autopilot for dual control missiles
    Shtessel, Y. AIAA Journal of Guidance, Control and Dynamics 32 (1) : 79 ~ 94 [2009]
  • Integrated guidance and control of moving-mass actuated kinetic warheads
    Menon, P. AIAA Journal of Guidance, Control and Dynamics 27 (1) : 118 ~ 126 [2004]
  • Integrated guidance and control of missiles with θ-D method
    Xin, M. IEEE Transactions on Control Systems Technology 14 (6) : 981 ~ 992 [2006]
  • Integrated guidance and control for dual-control missiles based on small-gain theorem
    Yan, H. Automatica 48 (10) : 2686 ~ 2692 [2012]
  • Integrated design of agile missile guidance and autopilot systems
    Menon, P. Control Engineering Practice 9 (10) : 1095 ~ 1106 [2001]
  • High-order mismatched disturbance compensation for motion control systems via a continuous dynamic sliding-mode approach
    Yang, J. IEEE Transactions on Industrial Informatics 10 (1) : 604 ~ 614 [2014]
  • Guidance laws with finite time convergence
    Zhou, D. AIAA Journal of Guidance, Control, and Dynamics 32 (6) : 1838 ~ 1846 [2009]
  • Guidance and control of missile interceptor using second-order sliding modes
    Shtessel, Y. IEEE Transactions on Aerospace and Electronic Systems 45 (1) : 110 ~ 124 [2009]
  • Dynamics and autopilot design for endoatmospheric interceptors with dual control systems
    Zhou, D. Aerospace Science and Technology 13 (6) : 291 ~ 300 [2009]
  • Disturbance rejection and robust least-squares control allocation in flight control system
    Cui, L. AIAA Journal of Guidance, Control, and Dynamics 34 (6) : 1632 ~ 1643 [2011]
  • Disturbance observer based control for nonlinear systems
    Chen, W. IEEE/ASME Transactions on Mechatronics 9 (4) : 706 ~ 710 [2004]
  • Design methods for the integrated guidance and control system
    Xue, W. Control Theory & Applications 30 (12) : 1511 ~ 1520 [2013]
  • Control allocation--a survey
    Johansen, T. Automatica 49 (5) : 1087 ~ 1103 [2013]
  • Composite disturbanceobserver-based control and H∞ control for complex continuous models
    Wei, X. International Journal of Robust and Nonlinear Control 20 (1) : 106 ~ 118 [2004]
  • Backstepping design of missile guidance and control based on adaptive fuzzy sliding mode control
    Ran, M. Chinese Journal of Aeronautics 27 (3) : 634 ~ 642 [2014]
  • Adaptive block dynamic surface control for integrated missile guidance and autopilot
    Hou, M. Chinese Journal of Aeronautics 26 (3) : 741 ~ 750 [2013]