Stability of Guided Parachute-Payload Systems for Planetary Descent-Reference-Cited by-同舟云学术

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Stability of Guided Parachute-Payload Systems for Planetary Descent

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
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Author:

Trovarelli Federico¹,Mooij Erwin¹

Affiliation:

1. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0665

Reference15 articles.

1. 3Helmut, G. H. and Lawrence Jr., W. R.“Dynamic stability of a parachute point-mass load system”, Report FDL-TDR64-126, Department of Aeronautics and Engineering Mechanics, University of Minnesota, Minneapolis, Minnesota, 1965.

2. 4Hume, R. “A Two dimensional Mathematical Model of a Parachute in Steady Descent”, Technical Report 1260, Aeronautical Research Council, 1973.

3. 5Abdulkadir, L. “Stability of Multibody Systems for Mars Descent and Landing”, MSc Thesis,Delft University of Technology, 2011.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Stability Analysis of the Parachute System with a Data-Driven Approach;Journal of Guidance, Control, and Dynamics;2023-01

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