Abstract
This paper summarizes the design and application of a cold gas thruster propulsion system for attitude control of satellites and space tugs. The control algorithm’s development relies on analyzing data collected through several tests intended for system identification. Therefore, the project highlights the importance of performing real time testing on the physical system along with validating the simulation of the mathematical model. The control mainly relies on PWM signal customized under the special constraints defined by the cold gas thruster characteristics.
| Original language | English |
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| Title of host publication | AIAA SciTech Forum and Exposition, 2024 |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624107115 |
| DOIs | |
| Publication status | Published - 2024 |
| Event | AIAA SciTech Forum and Exposition, 2024 - Orlando, United States Duration: 8 Jan 2024 → 12 Jan 2024 |
Publication series
| Name | AIAA SciTech Forum and Exposition, 2024 |
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Conference
| Conference | AIAA SciTech Forum and Exposition, 2024 |
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| Country/Territory | United States |
| City | Orlando |
| Period | 8/01/24 → 12/01/24 |
Bibliographical note
Publisher Copyright:© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.