首页> 外文会议>58th International Astronautical Congress 2007 >THE DESIGN OF 'INTERCEPTOR' AND INTEGRATED GUIDANCE AND NAVIGATION STRATEGY FOR FLYBY
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THE DESIGN OF 'INTERCEPTOR' AND INTEGRATED GUIDANCE AND NAVIGATION STRATEGY FOR FLYBY

机译:Flyby的“拦截器”设计与综合制导导航策略。

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interceptor and asteroid is estimated. The strategy of autonomous orbit control is also proposed. These are verified by the ground experiment using robotics simulator, which consists of a 6 DOF chaser and a 3 DOF target. In this experiment, on-board camera of the chaser takes images of a pebble attached on the target. The guidance and navigation of the chaser with respect to the target is demonstrated in various conditions, changing the small bodies shape and the lighting angle.
机译:估计有拦截器和小行星。还提出了自主轨道控制策略。这些已通过使用机器人模拟器的地面实验进行了验证,该模拟器由6个自由度的追赶者和3个自由度的目标组成。在该实验中,追赶者的机载摄像头拍摄了附着在目标上的小卵石的图像。在各种条件下演示了追赶者相对于目标的引导和导航,这些条件改变了小物体的形状和照明角度。

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