TY - GEN
T1 - Hayabusa - Final autonomous descent and landing based on target marker tracking
AU - Yoshimitsu, Tetsuo
AU - Kawaguchi, Jun'ichiro
AU - Hashimoto, Tatsuaki
AU - Kubota, Takashi
AU - Uo, Masashi
AU - Morita, Hideo
AU - Shirakawa, Kenichi
PY - 2006
Y1 - 2006
N2 - In November of 2005, Hayabusa performed descent flights to the Itokawa surface five times. The Itokawa surface is full of boulders against expectation and there are few flat areas where the spacecraft can touch down safely. With the reaction wheels lost prior to the events, it was very difficult to control translation motion accurately, since the guidance accuracy of several millimeters per second was requested. The guidance and navigation before launch assumed the autonomous guidance by identifying the illumination center aboard. However, it was not successful due to the highly irregular shape of the asteroid. On the other hand, the scenario based on the terrain recognition in quasi real time well worked. It was anticipated not useful before launch, since such process was conceived to take a lot of time and not effectively useful in real time operation. The Hayabusa project team devised and built the special tool on the ground and had tuned it before the successful three touch downs and one long landing on the surface.
AB - In November of 2005, Hayabusa performed descent flights to the Itokawa surface five times. The Itokawa surface is full of boulders against expectation and there are few flat areas where the spacecraft can touch down safely. With the reaction wheels lost prior to the events, it was very difficult to control translation motion accurately, since the guidance accuracy of several millimeters per second was requested. The guidance and navigation before launch assumed the autonomous guidance by identifying the illumination center aboard. However, it was not successful due to the highly irregular shape of the asteroid. On the other hand, the scenario based on the terrain recognition in quasi real time well worked. It was anticipated not useful before launch, since such process was conceived to take a lot of time and not effectively useful in real time operation. The Hayabusa project team devised and built the special tool on the ground and had tuned it before the successful three touch downs and one long landing on the surface.
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U2 - 10.2514/6.iac-06-c1.7.04
DO - 10.2514/6.iac-06-c1.7.04
M3 - Conference contribution
AN - SCOPUS:40549137811
SN - 9781605600390
T3 - AIAA 57th International Astronautical Congress, IAC 2006
SP - 4588
EP - 4594
BT - AIAA 57th International Astronautical Congress, IAC 2006
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - AIAA 57th International Astronautical Congress, IAC 2006
Y2 - 2 October 2006 through 6 October 2006
ER -