| タイトル | Flight performance of SEASAT-1 attitude control system |
| 著者（英） | Simcox, D. G.; Rodden, J. J.; Beach, S. W.; Hendricks, R. J. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1981-01-01 |
| 言語 | eng |
| 内容記述 | The paper describes the attitude control flight performance of SEASAT-A, (launched in June 1978), until failure of the power subsystem terminated the mission in Oct. 1978. Information provided by the satellite pertained to surface winds and coastal storm activity, currents and wave heights, ocean topography and temperature. The ACS used three-axis momentum exchange and magnetic momentum containment and was set in a nose-down configuration. Attitude control sensing was via horizon sensors and attitude anomalies, resulting from solar interference with the sensors, is covered in detail. Remedial action was taken by reconfiguring the IR scanners, but failure resulted nevertheless. Recommendations for similar future missions include consideration of the effect of light sources and circuit time constants and scan rates. A block diagram of the ACS is included. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 81A32893
AAS PAPER 81-046 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/416825 |
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