Identification of powered parafoil-vehicle dynamics from modelling and flight test data
During the final approach and landing phase of the X-38/Crew Return Vehicle, a steerable parafoil is used to maneuver and land at a targeted ground base under autonomous control. To simulate and verify performance of the onboard Parafoil Guidance, Navigation and Control system (PGNC), a commercial p...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
Texas A&M University
2006
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/1969.1/3859 |