An accurate positions, attitude and motion estimations of the debris target satellite are required to approaching to the target for its removal. We employed the visual-based sensing approach, that analyzes the image and/or sequence obtained by the chaser satellite, and considered this approach has the advantages of low-resources and low-cost. The experimental equipment that simulated approaching to the debris target under the actual optical environment is built in our laboratory. This equipment can precisely simulate to the debris removal phases in the orbit. In this presentation, our recent activities are introduced with some experimental results.
内容記述
形態: カラー図版あり
内容記述(英)
Physical characteristics: Original contains color illustrations