Open Access
Volume 37, Number 3, June 2019
Page(s) 532 - 540
Published online 20 September 2019
  1. Shertzer R H, Zimpfer D J, Brown P D. Control Allocation for the Next Generation of Entry Vehicles[C]//Proc of the AIAA Guidance, Navigation, and Control Conference, 2002: 5-8 [Google Scholar]
  2. Min B M, Kim E T, Tahk M J. Application of Control Allocation Methods to SAT-IIUAV[C]//AIAA Guidance, Navigation, and Control Conference, 2005: 5651-5660 [Google Scholar]
  3. YuJing, ChenMo, JiangChangsheng Adaptive Sliding Mode Control for Nonlinear Uncertain Systems Based on Disturbance Observer[J]. Control Theory & Applications, 2014, 31(8): 993-999 [Article] [Google Scholar]
  4. ZhangQiang, WuQingxian, JiangChangsheng, et al. Robust Reconfigurable Tracking Control of Near Space Vehicle with Actuator Dynamic and Input Constraints[J]. Control Theory & Applications, 2012, 29(10): 1263-1271 [Article] [Google Scholar]
  5. WangFang, ZongQun, TianNiling, et al. Robust Adaptive Back-Stepping Flight Control Design for Reentry RLV[J]. Control and Decision, 2014, 29(1): 12-18 [Article] [Google Scholar]
  6. ZhouLi, JiangChangsheng, QianChengshan. A Fast Adaptive Back-Stepping Method Based on Neural Networks[J]. Journal of Astronautics, 2008, 29(6): 1888-1894 [Article] [Google Scholar]
  7. ChenMo, ZouQingyuan, JiangChangsheng. Dynamical Inversion Flight Control Based on Neural Network Disturbance Observer[J]. Control and Decision, 2008, 23(3): 283-287 [Article] [Google Scholar]
  8. LeeT, KimY. Nonlinear Adaptive Flight Control Using Back-Stepping and Neural Networks Controller[J]. Journal of Guidance, Control, and Dynamics, 2012, 24(4): 675-682 [Article] [NASA ADS] [Google Scholar]
  9. DingShihong LiShihua. A Survey for Finite-Time Control Problems[J]. Control and Decision, 2011, 26(2): 161-169 [Article] [Google Scholar]
  10. Liu C, Dong C Y, Jiang W L. Finite-Time Adaptive Terminal Sliding Mode Controller Design for Reusable Launch Vehicle in Reentry Phase[C]//Guidance, Navigation & Control Conference, 2016 [Google Scholar]
  11. Dong Q, Zong Q. Integrated Finite-Time Disturbance Observer and Controller Design for Reusable Launch Vehicle in Reentry Phase[C]//Journal of Aerospace Engineering, 2016, 30(1): 04016076 [CrossRef] [Google Scholar]
  12. ZhouYu, HuangYimin, SunChunzhen. Control Technology Based on Pulse Width Modulation of RCS[J]. Journal of Terahertz Science and Electronic Information Technology, 2012, 10(4): 446-450 [Article] [Google Scholar]
  13. BolenderM A, DomanD B. Nonlinear Control Allocation Using Piecewise Linear Functions[J]. Journal of Guidance, Control, and Dynamics, 2004, 27(6): 1017-1027 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  14. HuW J, ZhouJ. Design of Neural Network Variable Structure Reentry Control System for Reusable Launch Vehicle[J]. Journal of China Ordnance, 2008, 4(3): 191-197 [Article] [Google Scholar]
  15. QianChengshan, WuQingxian, JiangChangsheng, et al. Flight Control for an Aerospace Vehicle's Reentry Attitude Based on Thrust of Reaction Jets[J]. Journal of Aerospace Power, 2008, 23(8): 1546-1552 [Article] [Google Scholar]
  16. HeChenglong, ChenXin, YangYidong. Mixed Programming Control Allocation for Reusable Launch Vehicles Using Dynamic Inverse Calculating[J]. Systems Engineering and Electronics, 2010, 32(9): 1973-1976 [Article] [Google Scholar]
  17. DongQ, ZongQ, TianB, et al. Integrated Finite-Time Disturbance Observer and Controller Design for Reusable Launch Vehicle in Reentry Phase[J]. Journal of Aerospace Engineering, 2016, 30(1): 04016076 [Article] [CrossRef] [Google Scholar]
  18. GengJ, ShengY Z, LiuX D. Finite-Time Sliding Mode Attitude Control for a Reentry Vehicle with Blended Aerodynamic Surfaces and a Reaction Control System[J]. Chinese Journal of Aeronautics, 2014, 27(4): 964-976 [Article] [CrossRef] [Google Scholar]
  19. HuQ, JiangB, FriswellM I. Robust Saturated Finite Time Output Feedback Attitude Stabilization for Rigid Spacecraft[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(6): 1914-1929 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  20. ParkJ H, SandbergI W. Universal Approximation Using Radial-Basis-Function Networks[J]. Neural Computation, 2008, 3(2): 246-257 [Article] [Google Scholar]
  21. Doman D B, Gamble B J, Ngo A D. Control Allocation of Reaction Control Jets and Aerodynamic Surfaces for Entry Vehicles[R]. AIAA-2007-6778 [Google Scholar]

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