Closed-Form Solutions for Underactuated Asymmetric Spacecraft Maneuvers Minimizing Torque Input

被引:0
|
作者
Kim, Donghoon [1 ]
Turner, James [2 ]
机构
[1] Univ Cincinnati, Aerosp Engn & Engn Mech, 2850 Campus Way,745 Baldwin Hall, Cincinnati, OH 45221 USA
[2] Amdyn Syst, Syst Engn, 9399 Wade Blvd, Frisco, TX 75035 USA
关键词
RIGID SPACECRAFT; ATTITUDE-CONTROL; STABILIZATION;
D O I
10.2514/1.G004447
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:2493 / 2500
页数:8
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