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Maximum Torque and Momentum Envelopes for Reaction Wheel Arrays

机译:反作用轮阵列的最大扭矩和动量包络

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Spacecraft reaction-wheel maneuvers are limited by the maximum torque and/or angular momentum that thenwheels can provide. The torque or momentum envelope for an n-wheel configuration can be obtained by projectingnthe n-dimensional hypercube, representing the domain boundary of individual wheel torques or momenta, intonthree-dimensional space via the 3 u0001 n matrix of wheel axes. This paper elucidates the properties of the projectednhypercube and presents algorithms for determining this maximal torque or momentum envelope for general wheelnconfigurations and for distributing a prescribed torque or momentum among the n wheels. We show that thesenalgorithms provide 22, 27, and 33% more capability than the more conventional pseudoinverse algorithm fornconfigurations of four, five, and sixwheels, respectively. Analysis of a representative slew using six wheels shows thatnthese algorithms can provide either a 25%reduction inmaximumwheelmomentumor a 30%reduction in slewtimenwhen compared with the pseudoinverse algorithm.
机译:航天器的反作用轮操纵受到飞轮可以提供的最大扭矩和/或角动量的限制。通过投影n维超立方体,可以表示n车轮配置的扭矩或动量包络,该多维数据通过车轮轴的3 u0001 n矩阵表示单个车轮扭矩或动量,无量纲空间的域边界。本文阐明了投影超立方体的特性,并提出了用于确定一般车轮配置的最大扭矩或动量包络以及在n个车轮之间分配规定扭矩或动量的算法。我们证明这些算法比分别针对四个,五个和六个车轮的常规伪逆算法提供了22、27和33%的能力。对使用六个车轮的典型回转的分析表明,与伪逆算法相比,这些算法可以使最大车轮动量减少25%,或者使回转时间减少30%。

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  • 来源
    《Journal of Guidance, Control, and Dynamics》 |2010年第5期|p.1606-1614|共9页
  • 作者单位

    F. Landis Markley∗NASA Goddard Space Flight Center, Greenbelt, Maryland 20771Reid G. Reynolds†Millennium Space Systems, Inc., Torrance, California 90503Frank X. Liu‡Stinger Ghaffarian Technologies, Inc., Greenbelt, Maryland 20770andKenneth L. Lebsock§Orbital Sciences Corporation, Greenbelt, Maryland 20770;

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