Electronics Optics & Control, Volume. 28, Issue 5, 14(2021)

Gliding Phase Trajectory Planning of Interceptor in Near Space Under Multiple Constraints

LI Wanli1、*, LI Jiong2, CHEN Wenyu1, LI Mingjie1, and LUO Changxin1
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  • 1[in Chinese]
  • 2[in Chinese]
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    References(3)

    [4] [4] IMADO F, KURODA T, SUSUMU M.Optimal midcourse guidance for medium-range air-to-air missiles[J].Journal of Guidance, Control, and Dynamics, 1990, 13(4): 603-608.

    [8] [8] OMKAR H, GANESHRAJA R, PADHI R.Robust reentry guidance of a reusable launch vehicle using model predictive static programming[J].Journal of Guidance, Control, and Dynamics, 2014, 37(1): 134-148.

    [13] [13] BARRON R L.Costate approximation and comparisons between improved and classical indirect trajectory optimization[J].Journal of Guidance, Control, and Dynamics, 2011, 34(2): 629-635.

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    LI Wanli, LI Jiong, CHEN Wenyu, LI Mingjie, LUO Changxin. Gliding Phase Trajectory Planning of Interceptor in Near Space Under Multiple Constraints[J]. Electronics Optics & Control, 2021, 28(5): 14

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    Paper Information

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    Received: Oct. 19, 2020

    Accepted: --

    Published Online: May. 14, 2021

    The Author Email: Wanli LI (liwl170@163.com)

    DOI:10.3969/j.issn.1671-637x.2021.05.004

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