DocumentCode
3173187
Title
Collision Dynamics of Target Maker for Visual Navigation in Small Body Exploration
Author
Kubota, Takashi ; Sawai, Shujiro ; Hashimoto, Tatsuaki ; Kawaguchi, Junichiro
Author_Institution
Inst. of Space & Astronautical Sci., Japan Aerosp. Exploration Agency, Kanagawa
fYear
2006
fDate
Oct. 2006
Firstpage
657
Lastpage
662
Abstract
The MUSES-C mission is the world first sample and return attempt to or from the near Earth asteroid. In deep space, it is hard to navigate, guide, and control a spacecraft on a real-time basis remotely from the earth mainly due to the communication delay. So autonomy is required for final approach and landing to an unknown body. It is important to navigate and guide a spacecraft to the landing point without hitting rocks or big stones. In the final descent phase, cancellation of the horizontal speed relative to the surface of the landing site is essential. This paper describes various kinds of robotics technologies applied for MUSES-C mission. An autonomous descent scheme and a novel visual navigation system are proposed and presented in detail. The validity and the effectiveness of the proposed methods are confirmed and evaluated by numerical simulations and flight results
Keywords
aerospace robotics; collision avoidance; mobile robots; telerobotics; MUSES-C mission; autonomous descent scheme; collision dynamics; near Earth asteroid; target maker; visual navigation system; Aerodynamics; Communication system control; Delay; Earth; Navigation; Optical sensors; Orbital robotics; Sampling methods; Space technology; Space vehicles; Artificial Target Marker; Autonomous Landing System; Collision Dynamics; Robotic Exploration; Visual Navigation;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Robots and Systems, 2006 IEEE/RSJ International Conference on
Conference_Location
Beijing
Print_ISBN
1-4244-0259-X
Electronic_ISBN
1-4244-0259-X
Type
conf
DOI
10.1109/IROS.2006.282550
Filename
4058432
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