Modeling and Analysis of Micro-Spacecraft Attitude Sensing with Gyrowheel

Modeling and Analysis of Micro-Spacecraft Attitude Sensing with Gyrowheel

This paper proposes two kinds of approaches of angular rate sensing for micro-spacecraft with a gyrowheel (GW), which can combine attitude sensing with attitude control into one single device to achieve a compact micro-spacecraft design. In this implementation, during the three-dimensional attitude...

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Bibliographic Details
Main Authors: Xiaokun Liu, Hui Zhao, Yu Yao, Fenghua He
Format: Article
Language:English
Published: MDPI AG 2016-08-01
Series:Sensors
Subjects:
gyrowheel
micro-spacecraft angular rate sensing
real-time Lyapunov linearization
complex quantity
static measurement
dynamic measurement
Online Access:http://www.mdpi.com/1424-8220/16/8/1321

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http://www.mdpi.com/1424-8220/16/8/1321

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