Author: Oosthuizen, Gert Adriaan
Similar Items: Resource efficient process chain development of a modular CubeSat spaceframe
- Development of an autonomous deorbiting device for a CubeSat
- Design of an aerodynamic attitude control system for a CubeSat
- An attitude control system for the deployment and stabilisation of a tethered dual CubeSat mission
- An FPGA-based adaptive forward error correction protocol for cubeSats
- An investigation into the imager pointing accuracy and stability for a CubeSat Using a CubeADCS in sun-synchronous low earth orbits
- Design and implementation of generic flight software for a CubeSat