Approach Planning and Guidance for Uncontrolled Rotating Satellite Capture Considering Collision Avoidance
نویسندگان
چکیده
The problem of planning safe kinematic approach trajectories for robotic capture of an uncontrolled rotating satellite is addressed, and two methods of trajectory planning are presented. The first method uses equations of orbital mechanics to plan a passive fly-by approach path for certain conditions of target satellite motion. The second method uses optimization techniques to plan an approach trajectory that is optimized with respect to a set of performance metrics. Results of these methods for representative scenarios are presented, and the relative merits of each method are discussed.
منابع مشابه
Fly-by Approach and Guidance for Uncontrolled Rotating Satellite Capture
Fig. 1 V-bar, R-bar and Fly-by Approach Existing orbital transfer vehicles such as US Space Shuttles, Progress and Japanese H-IIA Transfer Vehicle (HTV) use a straight path approach to the International Space Station (ISS). The straight path approach has many advantages and is suitable for stable targets such as ISS and three-axis attitude-controlled satellites. However, for satellite capture m...
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تاریخ انتشار 2003