Electronics Optics & Control, Volume. 22, Issue 12, 1(2015)
Trajectory Linearization Based Active Disturbance Rejection Control for Hypersonic Vehicle in WideEnvelop Maneuvering Flight
[2] [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] [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] [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] [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] [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] [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] [14] MOOIJ E. The motion of a vehicle in a planetary atmosphere[M]. The Netherlands: Delft University Press, 1997.
[15] [15] IBRIR S. Linear time-derivative trackers[J]. Automatica, 2004, 40(3): 397-405.
[19] [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.
Get Citation
Copy Citation Text
WANG Hong-lun, SHAO Xing-ling, ZHANG Hui-ping, YANG Ye. Trajectory Linearization Based Active Disturbance Rejection Control for Hypersonic Vehicle in WideEnvelop Maneuvering Flight[J]. Electronics Optics & Control, 2015, 22(12): 1
Category:
Received: --
Accepted: --
Published Online: Jan. 28, 2021
The Author Email: