Full metadata
Title
Modeling and Testing of a CubeSat Attitude Control System
Description
Accurate pointing is essential for any space mission with an imaging payload. The Phoenix Cubesat mission is being designed to take thermal images of major US cities from Low Earth Orbit in order to study the Urban Heat Island effect. Accurate pointing is vital to ensure mission success, so the satellite's Attitude Determination and Control System, or ADCS, must be properly tested and calibrated on the ground to ensure that it performs to its requirements. A commercial ADCS unit, the MAI-400, has been selected for this mission. The expected environmental disturbances must be characterized and modeled in order to inform planning the operations of this system. Appropriate control gains must also be selected to ensure the optimal satellite response. These gains are derived through a system model in Simulink and its response optimization tool, and these gains are then tested in a supplier provided Dynamic Simulator.
Date Created
2018-05
Contributors
- Wofford, Justin Michael (Author)
- Bowman, Judd (Thesis director)
- Jacobs, Daniel (Committee member)
- School of Earth and Space Exploration (Contributor)
- Mechanical and Aerospace Engineering Program (Contributor)
- Barrett, The Honors College (Contributor)
Topical Subject
Resource Type
Extent
15 pages
Language
eng
Copyright Statement
In Copyright
Primary Member of
Series
Academic Year 2017-2018
Handle
https://hdl.handle.net/2286/R.I.48216
Level of coding
minimal
Cataloging Standards
System Created
- 2018-04-21 12:23:48
System Modified
- 2021-08-11 04:09:57
- 3 years 2 months ago
Additional Formats