Trim and Stability Analysis of Parafoil/Payload System Using Bifurcation Methods-Reference-Cited by-同舟云学术

Trim and Stability Analysis of Parafoil/Payload System Using Bifurcation Methods

Published:2005-05-23 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
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Author:

Prakash Om¹,Daftary Avani¹,Ananthkrishnan N.¹

Affiliation:

1. Indian Institute of Technology Bombay

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1666

Reference8 articles.

1. Test vehicle ALEX-I for low-cost autonomous parafoil landing experiments

2. Aspects of Control for a Parafoil and Payload System

3. 9 dof Parafoil/Payload Simulator Development and Validation

4. 4Lingard, J. S. "The Performance and Design of Ram-Air Parachutes," Precision Aerial Delivery Seminar, Technical Report, Royal Aircraft Establishment, August 1981.

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