THE HUYGENS MISSION - DESIGN APPROACH FOR AN ATMOSPHERE ENTRY PROBE

被引:3
作者
PATTI, B
机构
[1] European Space Agency, Noordwijk
关键词
INTERPLANETARY SPACECRAFT; MISSION DESIGN; AUTONOMY; PLANETARY ENTRY; PARACHUTE DESCENT;
D O I
10.1016/0967-0661(95)00173-R
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The ESA Huygens probe is part of the NASA/ESA Cassini mission to the Saturnian system, and will make a 2-2.5 h exploratory descent to the surface of Titan. Huygens is designed to enter and brake in Titan's atmosphere in order to parachute a fully instrumented robotic laboratory. The main scientific measurements will be performed during the parachute descent, but some will also be performed during atmospheric entry; in addition, the probe resources are sized to allow measurements after it has impacted Titan's surface for at least a few minutes. This paper describes the control design and optimisation of the Huygens mission, based on an open-loop concept which is one of the keys to minimizing the mission risks induced by the uncertainties in the external environment.
引用
收藏
页码:1621 / 1630
页数:10
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