| タイトル | Range Filtering For Navigation By Satellite |
| 著者（英） | Paielli, Russell |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1989-08-01 |
| 言語 | eng |
| 内容記述 | Less processing and storage of data needed. Mathematical basis developed for Kalman filtering of sequential measurements of range from single-channel receiver in Global Positioning System (GPS) to each of several navigation satellites. Range filtering involves separate applications of kinematic Kalman tracking filter to measurements of signal from each satellite in use. State vector consists of pseudorange and time derivatives. Main advantages: simplification of tuning and decreases in required amounts of storage and processing of data for navigation in ships, airplanes, and ground vehicles. |
| NASA分類 | MATHEMATICS AND INFORMATION SCIENCES |
| レポートNO | 89B10423
ARC-12106 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/368039 |
