Spacecraft Recovery & Remote Sensing, Volume. 45, Issue 2, 19(2024)

Aerodynamic Parameter Estimation of Parachute Based on BP Neural Network

Fei CHANG1 and He JIA1,2
Author Affiliations
  • 1Beijing Institute of Space Mechanics & Electricity, Beijing 100094, China
  • 2College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
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    References(6)

    [5] [5] JANN T. Aerodynamic Model Identification GNC Design f the Parafoilload System ALEX[COL]16th AIAA Aerodynamic Decelerat Systems Technology Conference Seminar, 2124 May, 2001, Boston, MA. https:doi.g10.25146.20012015.

    [7] [7] ROGERS R. Aerodynamic Parameter Estimation f Controlled Parachutes[C]AIAA Guidance, Navigation, Control Conference Exhibit, August 58, 2002, Monterey, Califnia. [S.l.]: AIAA, 2002: 4708.

    [15] [15] COCKRELL D J, DOHERR K F. Preliminary Consideration of Parameter Identification Analysis from Parachute Aerodynamic Flight Test Data[COL]7th Aerodynamic Decelerat Balloon Technology Conference, 21 October—23 October 1981, San Diego, CA. https:doi.g10.25146.19811940.

    [17] [17] IBRAHIM S K, ENGDAHL R A. Parachute Dynamics Stability Analysis: NASACR120326[R]. [S.l.: s.n.], 1974.

    [18] [18] KINGMA D P, BA J. Adam: A Method f Stochastic Optimization[C]International Conference on Learning Representations Conferences: Computer Science, Mathematics, 22 December, 2014. [S.l.: s.n.], 2014.

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    Fei CHANG, He JIA. Aerodynamic Parameter Estimation of Parachute Based on BP Neural Network[J]. Spacecraft Recovery & Remote Sensing, 2024, 45(2): 19

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    Paper Information

    Category:

    Received: Sep. 30, 2023

    Accepted: --

    Published Online: May. 29, 2024

    The Author Email:

    DOI:10.3969/j.issn.1009-8518.2024.02.002

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