Constrained Attitude Control of a Cubesat with Redundant Reaction Wheel Configurations-Reference-Cited by-同舟云学术

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Constrained Attitude Control of a Cubesat with Redundant Reaction Wheel Configurations

Published:2024-03-02 Issue: Volume:8 Page:1-10
ISSN:
Container-title:2024 IEEE Aerospace Conference
language:
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Author:

wafi Ilyas El¹,Haloua Mohamed²,Guennoun Zouhair¹,Moudden Zakaria³

Affiliation:

1. University Center for Research in Space Technologies Mohammed V University,Mohammadia School of Engineers,Department of Electrical Engineering,Rabat,Morocco,10080

2. Mohammadia School of Engineers Mohammed V University,Department of Electrical Engineering,Rabat,Morocco,10080

3. Royal Center for Space Studies and Research,Rabat,Morocco,10100

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10520981/10520936/10521036.pdf?arnumber=10521036

Reference19 articles.

1. SOC-i: A CubeSat Demonstration of Optimization-Based Real-Time Constrained Attitude Control

2. Quaternion based linear time-varying model predictive attitude control for satellites with two reaction wheels

3. Generic Model of a Satellite Attitude Control System

4. Fuzzy logic microcontroller implementation for DC motor speed control

5. Instantaneous Torque Control of Small Inductance Brushless DC Motor

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