College - Author 1
College of Engineering
Department - Author 1
Aerospace Engineering Department
Advisor
Eric Mehiel - Aerospace Engineering Department
Funding Source
The Aerospace Engineering Department
Date
10-2024
Abstract/Summary
The Spacecraft Attitude Control Simulator is a single-axis attitude control platform which is intended to recreate the frictionless space environment in order to test cold-gas thruster control schemes. The overall goal of this research project was to observe settling data from the platform and compare it to simulated data. In practice, the predicted settling time was only 7% larger than observed settling time.
October 1, 2024.
Included in
Aerodynamics and Fluid Mechanics Commons, Navigation, Guidance, Control and Dynamics Commons, Other Aerospace Engineering Commons, Propulsion and Power Commons
URL: https://digitalcommons.calpoly.edu/ceng_surp/50