Reaction Wheel Design for CubeSat

被引：0

作者：

Oland, Espen ^{[1
]}

Schlanbusch, Rune ^{[1
]}

机构：

[1] Narvik Univ Coll, Dept Sci Comp Elect Engn & Space Technol, Narvik, Norway

来源：

RAST 2009: PROCEEDINGS OF THE 4TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES | 2009年

关键词：

Attitude Control; Reaction Wheel Design; CubeSat; Magnetic Torquers; Sliding Surface Controller; ROBOT MANIPULATORS; CONTROLLER;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents a reaction wheel design for CubeSats where it takes the limitation of size and mass into consideration. It presents an overview of which altitudes it is feasible to use magnetic torquers for momentum dumping as well as presenting equations for customizing reaction wheels for a CubeSat mission. The reaction wheels are then simulated for different CubeSat sizes and proved capable of performing attitude maneuvers. During these simulations a non-linear passivity-based sliding surface controller is used which through Lyapunov stability theory has been shown to be uniformly asymptotically stable.

引用

页码：778 / 783

页数：6

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