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Pitch guidance optimization for the orion ascent abort flight tests
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stillwater, Ryan Allanque |
| Copyright Year | 2010 |
| Description | Conference presentation sharing aspects of the pitch guidance optimization for the Orion ascent Abort Flight Test. |
| File Size | 928994 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20100039162 |
| Archival Resource Key | ark:/13960/t45q9x205 |
| Language | English |
| Publisher Date | 2010-08-02 |
| Access Restriction | Open |
| Subject Keyword | Launch Vehicles And Launch Operations Flight Tests Algorithms Ascent P-3 Aircraft Aircraft Guidance Ares 1 Launch Vehicle Crew Exploration Vehicle Aborted Missions Optimization Descent Pitch Inclination Dynamic Pressure Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
