Defence of dissertation in the field of Space Science and Technology, M.Sc. (Tech.) Osama Khurshid
The title of thesis is “Attitude estimation of a small spinning satellite using Kalman filter approaches”
The main objective of this thesis is to study more practical solutions for the attitude estimation algorithms of a fast spinning cubesat using Kalman filter approaches. The aim also encompasses the utilisation of a single algorithm for both the 3-axis and spin-stabilised attitude modes while also considering the computational load.
Opponent: Professor Chingiz Hajiyev, Istanbul Technical University, Turkey
Supervisor: Professor Esa Kallio, Aalto University School of Electrical Engineering, Department of Electronics and Nanoengineering.
Osama Khurshid, +358504086131, firstname.lastname@example.org