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
[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.
Get Citation
Copy Citation Text
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
Category:
Received: Dec. 31, 2024
Accepted: Dec. 31, 2024
Published Online: Jul. 1, 2025
The Author Email: