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Structural control interaction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Winder, S. W. Worley, H. E. Ryan, R. S. Mowery, D. K. |
| Copyright Year | 1973 |
| Description | The basic guidance and control concepts that lead to structural control interaction and structural dynamic loads are identified. Space vehicle ascent flight load sources and the load relieving mechanism are discussed, along with the the characteristics and special problems of both present and future space vehicles including launch vehicles, orbiting vehicles, and the Space Shuttle flyback vehicle. The special dynamics and control analyses and test problems apparent at this time are summarized. |
| File Size | 2230997 |
| Page Count | 56 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730013107 |
| Archival Resource Key | ark:/13960/t1zd2pp8r |
| Language | English |
| Publisher Date | 1973-01-15 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Structural Design Trajectory Control Space Shuttles Optimal Control Spacecraft Guidance Angle of Attack Optimization Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
