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1. 1. Experiment Design for System Identification on Satellite Hardware Demonstrator

   University essay from Luleå tekniska universitet/Institutionen för system- och rymdteknik

   Author : Elias Krantz; [2018]
   Keywords : LTU; Airbus; Attitude; Guidance; Control; AOCS; GNC; Kalman Filter; UKF; System Identification; SysId; Estimation; Determination; CMG;

   Abstract : The subject of this thesis covers the process of online parameter estimation of agile satellites. Accurate knowledge of parameters such as moment of inertia and centre of mass play a crucial role in satellite attitude control and pointing performance. READ MORE