[2] DAVIDSON J, LALLMAN F, MCMINN J D, et al. Flight control laws for NASA's hyper-X research vehicle［R］. AIAA-1999-4124, Reston: AIAA, 1999.
[3] HOU Y Z, WANG Q, DONG C Y. Gain scheduled control: switched polytopic system approach［J］. Journal of Guidance, Control and Dynamics, 2011, 34(2): 623-629．
[4] ZHU J, BANKER B D, HALL C E. X-33 ascent flight control design by trajectory linearization：a singular perturbation approach［R］. AIAA-2000- 4159, Reston：AIAA, 2000.
[5] LIU Y, ZHU J J. Regular perturbation analysis for trajectory linearization control［C］//Proceedings of American Control Conference, New York City, 2007：3053-3058.
[11] SHAO X L, WANG H L. Trajectory linearization control based output tracking method for nonlinear uncertain system using linear extended state observer ［J］. Asian Journal of Control, 2015, 17(6): 1-12.
[13] SHAO X L, WANG H L. Active disturbance rejection based trajectory linearization control for hypersonic reentry vehicle with bounded uncertainties［J］. ISA Transactions, 2015, 54(1): 27-38.
[14] MOOIJ E. The motion of a vehicle in a planetary atmosphere［M］. The Netherlands: Delft University Press, 1997.
[15] IBRIR S. Linear time-derivative trackers［J］. Automatica, 2004, 40（3）: 397-405.
[19] SHAO X L, WANG H L. Back-stepping active disturbance rejection control design for integrated missile guidance and control system via reduced-order ESO［J］. ISA Transactions, 2015, 57(4): 10-22.
