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Six-Degree-of-Freedom Model of a Controlled Circular Parachute

  • Published:2002-06-25 Issue: Volume: Page:
  • ISSN:
  • Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
  • language:
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Author:

Dobrokhodov Vladimir1,Yakimenko Oleg1,Junge Christopher1

Affiliation:

1. Naval Postgraduate School

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

1. Wolf, D.F. "The Dynamic Stability of a Non-Rigid Parachute and Payload System," Ph.D. dissertation,University of Rhode Island, Kingston, RI, 1968.

2. Wolf, D.F. "An Investigation of Parachute Dynamic Stability," M.S. thesis,University of Rhode Island, Kingston, RI, 1965.

3. A theory of three-dimensional parachute dynamic stability.

4. Computer Model of a Fully-Deployed Parachute

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1. An estimation method for parachute parameters;Journal of Physics: Conference Series;2021-02-01

2. Modeling and Simulation Framework for Multi-Objective Identification of a Guided Descending System;AIAA Modeling and Simulation Technologies Conference and Exhibit;2003-06-25

3. On the Development of a Six-Degree-of-Freedom Model of a Low-Aspect-Ratio Parafoil Delivery System;17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2003-05-19

4. Simulink Implementation of the 6DoF Model of Controlled Circular Parachute;AIAA Modeling and Simulation Technologies Conference and Exhibit;2002-06-25

5. On Control of Autonomous Circular Parachutes;AIAA Guidance, Navigation, and Control Conference and Exhibit;2002-06-25
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