摘要
For Venus exploration, a Venus spacecraft is expected to keep its digital transmission antenna pointing towards the Earth for ultra-long-distance and low-bit-rate transmission. Fixed heat-dispersing surfaces are also expected to maintain the temperature inside the spacecraft, which iscloser to the Sun than the Earth's orbiter. This paper addresses a new attitude pointing design scheme for Venus spacecraft just by placing the antenna irregularly on the spacecraft, which is beneficial to transmitting data from Venus to Earth and holding the temperature against the Sun. Unlike other Venus spacecrafts employing two or three antennas to transmitting data, such as Venus Express (ESA) and AKATSUKI (JAXA), the present scheme aims to reduce the number of transmission antennas to only one and to set the fixed surfaces as thermal radiators. Two detailed strategies during the flight operation are proposed in this paper to drive the attitude manoeuvres to keep the only antenna pointing to the Earth all the time and t switch the radiator to the suitable surface in specified intervals.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 325-330 |
| 页数 | 6 |
| 期刊 | Aerospace Science and Technology |
| 卷 | 39 |
| DOI | |
| 出版状态 | 已出版 - 12月 2014 |
指纹
探究 'A new attitude pointing design for Venus spacecraft' 的科研主题。它们共同构成独一无二的指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver