タイトル | The determination of the interplanetary orbits of Vikings 1 and 2 |
著者(英) | Rinker, G. C.; Donegan, A. J.; Christensen, C. S.; Mottinger, N. A.; Acton, C. H.; Campbell, J. K.; Rourke, K. H.; Winn, F. B.; Jerath, N.; Breckenridge, W. G. |
著者所属(英) | Jet Propulsion Lab., California Inst. of Tech. |
発行日 | 1977-01-01 |
言語 | eng |
内容記述 | A description is presented of the navigation-related events of the Viking Mars mission. Orbit determination system fundamentals are discussed, taking into account the trajectory models, observation models, radio data models, range considerations, optical data models, filter models, the orbit determination process, critical orbit determination inputs, and orbit determination errors. Attention is also given to questions of orbit determination strategy, orbit determination results, optical measurements processing, aspects of approach orbit determination evaluation, and the orbit determination software system. |
NASA分類 | SPACE COMMUNICATIONS, SPACECRAFT COMMUNICATIONS, COMMAND AND TRACKING |
レポートNO | 77A22220 AIAA PAPER 77-71 |
権利 | Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/439203 |
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