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Optimal large angle maneuvers with simultaneous shape control/vibration arrest
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Turner, J. D. Junkins, J. L. |
| Copyright Year | 1980 |
| Description | A relaxation method is demonstrated which reliably solves the nonlinear two point boundary value problem which arises when optimal control theory is applied to determination of large angle maneuvers of flexible spacecraft. The basic ideas are summarized and several idealized maneuvers are determined. The emphasis is upon demonstrating the basic ideas and practical aspects of the methodology. |
| File Size | 311814 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800019897 |
| Archival Resource Key | ark:/13960/t3906xs3m |
| Language | English |
| Publisher Date | 1980-01-01 |
| Access Restriction | Open |
| Subject Keyword | Astrodynamics Spacecraft Maneuvers Boundary Value Problems Relaxation Method Mathematics Algorithms Satellite Attitude Control Optimal Control Differential Equations Orbital Maneuvers Large Space Structures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
