Spacecraft Recovery & Remote Sensing, Volume. 46, Issue 1, 21(2025)

Parameter Identification of Parachute Inflation Phase Based on YOLO

Ce LU1, Zhuangzhi WU2, Xiaopeng XUE3, Kang LIU1, and Wei RONG1
Author Affiliations
  • 1Beijing Institute of Space Mechanics & Electricity, Beijing 100094, China
  • 2School of Computer Science and Engineering, Beihang University, Beijing 100191, China
  • 3School of Automation Academy, Central South University, Changsha 410083, China
  • show less
    References(11)

    [3] [3] MRIS A, FRAIRE U, BLEDSOE K, et al. Simulating New Test Vehicles Test Techniques f the ion Cev Parachute Assembly System[C]21st AIAA Aerodynamic Decelerat Systems Technology Conference Seminar, May 2326, 2011, Dublin, Irel. [S. l.]: AIAA, 2011: AIAA 20112616. DOI: 10.25146.20112616.

    [4] [4] MOOG R D. Aerodynamic Line Bowing During Parachute Deployment[C]5th Aerodynamic Deceleration Systems Conference, November 1719, 1975, Albuquerque, NM. [S. l.]: AIAA, 2012: AIAA 751381. DOI: 10.25146.19751381.

    [5] [5] PURVIS J W. Prediction of Line Sail During LinesFirst Deployment[C]Prediction of Line Sail During LinesFirst Deployment, January 1013, 1983, Reno, NV. [S. l.]: AIAA, 1983: AIAA 830370. DOI: 10.25146.1983370.

    [7] [7] STRICKERT G, JANN T. Determination of the Relative Motion Between Parafoil Canopy Load Using Advanced Videoimage Processing Techniques[C]15th Aerodynamic Decelerat Systems Technology Conference, June 0811, 1999, Toulouse, France. [S. l.]: AIAA, 1999: AIAA991754. DOI: 10.25146.19991754.

    [8] [8] DECKER R J, YAKIMENKO O A. Automated Canopy Payload Motion Estimation Using Vision Based Methods[C]23rd AIAA Aerodynamic Decelerat Systems Technology Conference, March 30April 2, 2015, Daytona Beach, FL. [S. l.]: AIAA, 2015: 2171. DOI: 10.25146.20152171.

    [9] [9] KUMAR Y, SHARMA A, SHADAAB, et al. Validation of Canopy Payload Relative Motion Estimation f Parafoil Aerial Vehicle using Computer Vision[C]AIAA Atmospheric Flight Mechanics Conference, June 59, 2017, Denver, Colado. [S. l.]: AIAA, 2017: 3728. DOI: 10.25146.20173728.

    [10] [10] RAY E, BRETZ D, MRIS A. Photogrammetric Analysis of CPAS Main Parachutes[C]21st AIAA Aerodynamic Decelerat Systems Technology Conference Seminar, May 2326, 2011, Dublin, Irel. [S. l.]: AIAA, 2011: 2538. DOI: 10.25146.20112538.

    [11] [11] RAY E, BRETZ D R. Improved CPAS Photogrammetric Capabilities f Engineering Development Unit (EDU) Testing[C]AIAA Aerodynamic Decelerat Systems (ADS) Conference, March 2528, 2013, Daytona Beach, Flida. [S. l.]: AIAA, 2013: AIAA 20131258. DOI: 10.25146.20131258.

    [12] [12] HULTGREN E L, COLLINS P, LETTIERI C. Advances in Modeling Clusters of Parachutes f SpaceX Dragon Spacecraft[C]26th AIAA Aerodynamic Decelerat Systems Technology Conference, May 1619, 2022, Toulouse, France. [S. l.]: AIAA, 2022: 2709. DOI: 10.25146.20222709.

    [23] [23] REZATOFIGHI H, TSOI N, GWAK J Y, et al. Generalized Intersection over Union: A Metric a Loss f Bounding Box Regression[C]2019 IEEECVF Conference on Computer Vision Pattern Recognition (CVPR), June 1520, 2019, Long Beach, CA, USA. Piscataway, NJ: IEEE, 2019: 658666. DOI: 10.1109CVPR.2019.00075.

    Tools

    Get Citation

    Copy Citation Text

    Ce LU, Zhuangzhi WU, Xiaopeng XUE, Kang LIU, Wei RONG. Parameter Identification of Parachute Inflation Phase Based on YOLO[J]. Spacecraft Recovery & Remote Sensing, 2025, 46(1): 21

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category:

    Received: Oct. 16, 2024

    Accepted: --

    Published Online: Apr. 2, 2025

    The Author Email:

    DOI:10.3969/j.issn.1009-8518.2025.01.003

    Topics