ACSER SEMINAR: The Attitude Determination and Control System for the EC0 Cubesat
This presentation gives an overview of the attitude determination and control system (ADCS) of the EC0 cubesat due to launch in December this year as part of the QB50 mission. EC0's ADCS system comprises UNSW developed hardware and software as well as commercial off the shelf hardware which has been implemented in a way that it can be re-purposed on other satellites in a modular fashion. Additionally, mission operations and the test configuration and verification of the ADCS system is presented along with lessons learned.
Presented by Benjamin Southwell, UNSW ACSER PhD Candidate.
Registrations welcome but not essential.