タイトル | Interplanetary beacon for deep space navigation |
著者(英) | Nicholson, F. T.; Winn, F. B.; Smith, C. B.; Ananda, M. P. |
著者所属(英) | Jet Propulsion Lab., California Inst. of Tech. |
発行日 | 1980-01-01 |
言語 | eng |
内容記述 | The utilization of the Viking lander as a beacon for navigating the Galileo spacecraft for its Mars flyby is investigated. Covariance analyses show that the improvement in the flyby navigation accuracy is significant compared with the conventional radiometric navigation. A validation experiment using Viking lander and orbiter indicates that the expected accuracy can be obtained. |
NASA分類 | SPACE COMMUNICATIONS, SPACECRAFT COMMUNICATIONS, COMMAND AND TRACKING |
レポートNO | 82A18163 |
権利 | Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/412509 |