20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 2009
DOI: 10.2514/6.2009-2933
|View full text |Cite
|
Sign up to set email alerts
|

A High-Glide Ram-Air Parachute for 6,000 Kg Payloads, Tested With the FASTWing CL Test-Vehicle

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2011
2011
2016
2016

Publication Types

Select...
2
1
1

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(2 citation statements)
references
References 5 publications
0
2
0
Order By: Relevance
“…However, testing an actual parafoil was outside the scope of this research. The present model is based on the FASTWing CL parafoil [7]. It is based on the geometry, dimensions, weights, and some aerodynamic properties of the FASTWing CL system, but complete aerodynamic data was not available.…”
Section: Parafoil Modellingmentioning
confidence: 99%
See 1 more Smart Citation
“…However, testing an actual parafoil was outside the scope of this research. The present model is based on the FASTWing CL parafoil [7]. It is based on the geometry, dimensions, weights, and some aerodynamic properties of the FASTWing CL system, but complete aerodynamic data was not available.…”
Section: Parafoil Modellingmentioning
confidence: 99%
“…This study considers a large-scale parafoil for 6000 kg payload modelled using available data on the FASTWing and FASTWing CL parafoils [7]. The research focuses on design of guidance laws for precision landing of the parafoil; then, a behavioural strategy for relative motion control of multiple parafoils is proposed and its effects on the baseline guidance are investigated.…”
Section: Introductionmentioning
confidence: 99%