Spacecraft Recovery & Remote Sensing, Volume. 46, Issue 3, 12(2025)

Research on Attitude Stability Control of Parachute Cabin Combination under the Action of Supersonic Deceleration Parachute

Boyi TAN1,2, Liuxin QU2, Zhi LIU2, Hexi BAOYIN1, and Yao LI2
Author Affiliations
  • 1School of Aerospace Engineering, Tsinghua University, Beijing 100084, China
  • 2The System Design Institute of Mechanical-Electrical Engineering, Beijing 100854, China
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    References(6)

    [4] [4] DEVIN K, MIGUEL S M, JOHN E, et al. Mars Science Labaty Entry, Descent, Ling Triggers[C]2007 IEEE Aerospace Conference. Big Sky, MT, USA: IEEE, 2007: 110. DOI: 10.1109AERO.2007.352825.

    [12] [12] FALLON I E. Parachute Dynamics Stability Analysis of the Queen Match Recovery System[C]11th Aerodynamic Decelerat Systems Technology Conference. San Diego, CA, USA: AIAA, 2012: AIAA910879CP. DOI: 10.25146.1991879.

    [14] [14] MOULIN J. Recovery System SimulationLink Modelization[C]Aerospace Design Conference. Irvine, CA, USA: AIAA, 1993: AIAA931249, DOI: 10.25146.19931249.

    [15] [15] GONYEA K, BRAUN R, CHRISTOPHER L, et al. Aerodynamic Stability Perfmance of NextGeneration Parachutes f Mars Descent[C]AIAA Aerodynamic Decelerat Systems (ADS) Conference. Daytona Beach, Flida: AIAA, 2013: AIAA20131356. DOI: 10.25146.20131356.

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    Boyi TAN, Liuxin QU, Zhi LIU, Hexi BAOYIN, Yao LI. Research on Attitude Stability Control of Parachute Cabin Combination under the Action of Supersonic Deceleration Parachute[J]. Spacecraft Recovery & Remote Sensing, 2025, 46(3): 12

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    Paper Information

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    Received: Dec. 31, 2024

    Accepted: Dec. 31, 2024

    Published Online: Jul. 1, 2025

    The Author Email:

    DOI:10.3969/j.issn.1009-8518.2025.03.002

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