Time-Efficient Angular Steering Laws for Rigid Satellites

著录项

• 来源
  《Journal of guidance, control, and dynamics》 |2011年第3期|p.878-892|共15页
• 作者

  Dov Verbin; Vaios J. Lappas; Joseph Z. Ben-Asher;

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• 作者单位

  University of Surrey, Guildford, England GU2 7XH, United Kingdom,Israel Aerospace Industries, MBT Space Division, 56000 Yehud, Israel;

  University of Surrey, Guildford, England GU2 7XH, United Kingdom,Surrey Space Centre;

  Technion-Israel Institute of Technology, 32000 Haifa, Israel,Faculty of Aerospace Engineering;

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• 收录信息
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  BF(B); body frame fixed to the satellite; F_α; ratio between safe and maximum acceleration; 0 Fa 1; F_ω; ratio between safe and maximum angular rate; 0 Fa 1; h_(Wi); angular momentum of ith reaction wheels, N • m • s; H_B~s; total angular momentum of satellite including reaction wheels, as formulated in the body framecoordinates, N • m • s; et al;

  机译：BF（B）;固定在卫星上的车身框架;F_α;安全与最大加速度之比;0 Fa 1;F_ω;安全角与最大角速度之比;0 Fa 1;h_（Wi）;第i个反作用轮的角动量N•m•s;H_B〜s;卫星（包括反作用轮）的总角动量;根据人体坐标系表示;N•m•s;等;