COLLISION DETECTION FOR SPACECRAFT PROXIMITY OPERATIONS

被引:0
|
作者
VAUGHAN, RM
BERGMANN, EV
WALKER, BK
机构
[1] CHARLES STARK DRAPER LAB INC,FLIGHT SYST,CAMBRIDGE,MA 02139
[2] UNIV CINCINNATI,AEROSP ENGN & ENGN MECH,CINCINNATI,OH 45221
关键词
D O I
10.2514/3.20631
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A new collision detection algorithm has been developed for use when two spacecraft are operating in the same vicinity. The two spacecraft are modeled as unions of convex polyhedra, where the resulting polyhedron may be either convex or nonconvex. The relative motion of the two spacecraft is assumed to be such that one vehicle is moving with constant linear and angular velocity with respect to the other. Contacts between the vertices, faces, and edges of the polyhedra representing the two spacecraft are shown to occur when the value of one or more of a set of functions is zero. The collision detection algorithm is then formulated as a search for the zeros (roots) of these functions. Special properties of the functions for the assumed relative trajectory are exploited to expedite the zero search. The new algorithm is the first algorithm that can solve the collision detection problem exactly for relative motion with constant angular velocity. This is a significant improvement over models of rotational motion used in previous collision detection algorithms.
引用
收藏
页码:225 / 229
页数:5
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