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A new attitude pointing design for Venus spacecraft

  • Ming Xu*
  • , Zuopeng Wang
  • *此作品的通讯作者

科研成果: 期刊稿件文章同行评审

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
39
DOI
出版状态已出版 - 12月 2014

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