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Sps attitude control and stationkeeping: requirements and tradeoffs
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Oglevie, R. E. |
| Copyright Year | 1980 |
| Description | The dominant control requirements of solar power satellites change appreciably relative to small contemporary spacecraft. Trade studies and analyses illustrated preferred control approaches. It was found that the geosynchronous equatorial orbit is preferred over the alternative orbits considered, that the solar pressure orbit perturbation dominates stationkeeping propulsion requirements and that a combined AC and SK system using ion electric propulsion can satisfy the attitude control requirements. It was also found that control system/structural dynamic interaction stability can be obtained through frequency separation with reasonable structural dynamic requirements and simplify spacecraft design. |
| File Size | 317330 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820014824 |
| Archival Resource Key | ark:/13960/t7fr4pr4x |
| Language | English |
| Publisher Date | 1980-07-01 |
| Access Restriction | Open |
| Subject Keyword | Energy Production And Conversion Stationkeeping Satellite Attitude Control Tradeoffs Dynamic Stability Feasibility Analysis Geosynchronous Orbits Solar Power Satellites Spacecraft Propulsion Large Space Structures Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |