Integrated power and attitude control with two flywheels

被引：28
|
作者：
Kenny, BH
Jansen, R
Kascak, P
Dever, T
Santiago, W
机构：
[1] NASA, Glenn Res Ctr, Cleveland, OH 44135 USA
[2] Univ Toledo, Toledo, OH 43606 USA
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2005年 / 41卷 / 04期
关键词：
D O I：
10.1109/TAES.2005.1561894
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Energy storage and attitude control are two distinct subsystems of the typical satellite. Energy storage is provided using batteries and active attitude control is accomplished with control moment gyroscopes or reaction wheels. A system mass savings can be achieved if these two subsystems are combined using multiple flywheels for simultaneous kinetic energy storage and momentum transfer. This paper develops, simulates, and experimentally demonstrates the control algorithms to accomplish integrated power and single-axis attitude control using two flywheels.
引用
收藏
页码：1431 / 1449
页数：19
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