Tethered towing using open-loop input-shaping and discrete thrust levels

被引:43
作者
Jasper, Lee [1 ]
Schaub, Hanspeter [1 ]
机构
[1] Univ Colorado, UCB Colorado Ctr Astrodynam Res 431, Dept Aerosp Engn Sci, ECNT 321, Boulder, CO 80309 USA
关键词
Space debris; Active debris removal; Tether; Input shaping; Bang-off-bang; Posicast; SPACE; DYNAMICS; SHAPERS;
D O I
10.1016/j.actaastro.2014.10.001
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Asteroid retrieval, satellite servicing, and debris removal concepts often rely on a thrusting vehicle to redirect and steer a passive object. One effective way to tow the object is through a tether. This study employs a discretized tether model attached to six degree-of-freedom end bodies. To reduce the risk of a post-burn collision between the end bodies, discrete thrust input shaping profiles are considered including a Posicast input and a bang-off-bang thrust profile. These input shaping techniques attain desirable collision avoidance performance by inducing a tumbling or gravity gradient motion of the tethered formation. Their performance is compared to an earlier frequency notched thruster profile. (C) 2014 IAA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:373 / 384
页数:12
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