Electronics Optics & Control, Volume. 22, Issue 12, 1(2015)

Trajectory Linearization Based Active Disturbance Rejection Control for Hypersonic Vehicle in WideEnvelop Maneuvering Flight

WANG Hong-lun1...2, SHAO Xing-ling1,2, ZHANG Hui-ping3 and YANG Ye4 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
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    References(9)

    [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.

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    [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.

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    WANG Hong-lun, SHAO Xing-ling, ZHANG Hui-ping, YANG Ye. Trajectory Linearization Based Active Disturbance Rejection Control for Hypersonic Vehicle in WideEnvelop Maneuvering Flight[J]. Electronics Optics & Control, 2015, 22(12): 1

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    Paper Information

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    Received: --

    Accepted: --

    Published Online: Jan. 28, 2021

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    DOI:10.3969/j.issn.1671-637x.2015.12.001

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