| METHOD OF TRAJECTORY CONTROL BY MULTI-POINT MEASURING COMPLEX OF MULTI-PULSE ORBITS OF SPACECRAFT INJECTION INTO HIGH-ELLIPTICAL, GEOSTATIONARY AND GEOSTATIONARY ORBITS USING ACCELERATING UNITS | |
| 2024-02-27 | |
| 专利权人 | 4 CENT SCI RES INST MIN DEFENSE RUS (FOUR-Soviet Institute) |
| 申请日期 | 2024-02-27 |
| 专利号 | RU2834499-C1 |
| 成果简介 | NOVELTY - Method for trajectory control of orbits of spacecraft injection into different orbits using GLONASS/GPS navigation systems. Navigation parameters of the booster unit are determined and transmitted to the ground complex, where statistical estimates of the orbit parameters are determined. Interrogation trajectory signal is conducted and the range and speed of the accelerating unit are measured. Refined estimates of navigation definitions are obtained using navigation systems and a multi-point measuring system. Corrections to measured values at slave ground stations are determined. Obtained data are used to determine parameters of spacecraft orbits. USE - Spacecraft navigation. ADVANTAGE - Increased volume of obtained measurements, accuracy and reliability of navigation determinations. 2 cl, 2 dwg |
| IPC 分类号 | B64G-003/00 ; G01S-019/03 |
| 国家 | 俄罗斯 |
| 专业领域 | 信息技术 |
| 语种 | 英语 |
| 成果类型 | 专利 |
| 文献类型 | 科技成果 |
| 条目标识符 | http://119.78.100.226:8889/handle/3KE4DYBR/17974 |
| 专题 | 中国科学院新疆生态与地理研究所 |
| 作者单位 | 4 CENT SCI RES INST MIN DEFENSE RUS (FOUR-Soviet Institute) |
| 推荐引用方式 GB/T 7714 | KUKUSHKIN S S,BORISKIN S V,SHIGAREVA Z P. METHOD OF TRAJECTORY CONTROL BY MULTI-POINT MEASURING COMPLEX OF MULTI-PULSE ORBITS OF SPACECRAFT INJECTION INTO HIGH-ELLIPTICAL, GEOSTATIONARY AND GEOSTATIONARY ORBITS USING ACCELERATING UNITS. RU2834499-C1[P]. 2024. |
| 条目包含的文件 | 条目无相关文件。 | |||||
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