Near Space Vehicle Control Based on Back-Stepping Robust Adaptive Dynamic Surface

XU Wen-ying; JIANG Ju; ZHEN Zi-yang; LI Xin

doi:10.3969/j.issn.1671-637x.2018.11.003

[1] HENRY J, PINES D J.A mathematical model for roll dynamics by use of a morphing-span wing［C］//The 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2007:AIAA-2007-1708.

[3] YOUNG M, KEITH S, PANCOTTI A.An overview of advanced concepts for near space systems［C］//The 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, 2009:AIAA-2009-4805.

[9] CHAVEZ R F, SCHMIDT K D.Analytical aeropropulsive/aeroelastic hypersonic vehicle model with dynamic analysis［J］.Journal of Guidance, Control and Dynamics, 1994, 17(6):1308-1319.

[10] PARKER T J, BOLENDER A M, DOMAN B D.Control-oriented modeling of an air-breathing hypersonic vehicle［J］.Journal of Guidance, Control and Dynamics, 2007, 30(3):856-869.

[12] LIU Y, LU Y.Longitudinal inversion flight control based on backstepping for hypersonic vehicle［J］.Control and Decision, 2007, 22(3):313-317.

[13] XU H, MIRMIRANI M, IOANNOU P.Adaptive sliding mode control design for a hypersonic flight vehicle［J］.Journal of Guidance, Control, and Dynamics, 2004, 27(5): 829-838.

[14] GAO D X, SUN Z Q, DU T R.Dynamic surface control for hypersonic aircraft using fuzzy logic system［C］//IEEE International Conference on Automation and Logistics, IEEE, 2007:2314-2319.

[19] WANG Q, STENGLE R F．Robust nonlinear control of a hypersonic aircraft［J］.Journal of Guidance, Control and Dynamics, 2000, 23(4):577-585.

[20] ZHU J, HUIZENGA A.A type two linearization controller for a reusable launch vehicle-a singular perturbation approach［C］//AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2004:1-16.