Prediction of attitude motion of ISIS satellites / by F.R. Vigneron, D. Harrison, F. Yip and G.G. Bower.: Co24-3/7-1226-1972E-PDF
"A mathematical model based on an "averaging" technique is developed for the prediction of attitude motion and spin rate of ISIS-I or ISIS-II under the action of the magnetic torquing control system. The derived motion equations are solved numerically on a digital computer. The model is verified by comparison with flight data of the ISIS-I for all modes of operation. In addition, two malfunctions of the control system are demonstrated"--Abstract, page 1.
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| Department/Agency | Communications Research Centre (Canada), issuing body. |
|---|---|
| Title | Prediction of attitude motion of ISIS satellites / by F.R. Vigneron, D. Harrison, F. Yip and G.G. Bower. |
| Series title | CRC report ; no. 1226 |
| Publication type | Series - View Master Record |
| Language | [English] |
| Format | Electronic |
| Electronic document | |
| Note(s) | Digitized edition from print [produced by Innovation, Science and Economic Development Canada]. Includes bibliographical references (pages 26-27). |
| Publishing information | Ottawa : Communications Research Centre, Department of Communications, February 1972. |
| Author / Contributor | Vigneron, F. R., author. |
| Description | 1 online resource (iii, 41 pages) : illustrations. |
| Catalogue number |
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| Subject terms | ISIS-II (Artificial satellite) Artificial satellites -- Attitude control systems -- Mathematical models. ISIS-II (Satellite artificiel) Satellites artificiels -- Systèmes de commande d'orientation -- Modèles mathématiques. |
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