Design requirements for a small satellite (NPSAT-l) Attitude Determination and Control Subsystem (ADCS) is a three-axis stabilized spacecraft which requires a c

This thesis investigates a new concept for the flexible design and verification of an ADCS for a nanosatellite platform. In order to investigate guidelines for

This book gathers selected research papers presented at the International Conference on Power, Control and Communication Infrastructure 2019 (ICPCCI 2019), orga