SwissCube: development of an ultra-light and efficient Inertia Wheel Assembly for the attitude control of pico-satellites
- Paper number
IAC-08.B4.6.A2
- Author
Mr. Gavrilo Bozovic, Ecole Polytechnique Fédérale de Lausanne (EPFL), Switzerland
- Coauthor
Mr. Omar Scaglione, Swiss Federal Institute of Technology Lausanne, Switzerland
- Coauthor
Mr. Enrique Guzman, Swiss Federal Institute of Technology Lausanne, Switzerland
- Coauthor
Mr. Christian Koechli, Swiss Federal Institute of Technology Lausanne, Switzerland
- Year
2008
- Abstract
SwissCube is a CubeSat class picosatellite (10 x 10 x 10 [cm3], weight: 1 [kg]), whose aim is to characterize the Night Glow phenomenon, in order to validate its use in a low-cost earth sensor. The satellite is to be launched by the end of 2008 or beginning of 2009.
For this project was developed an ultra-light and efficient Inertia Wheel Assembly (IWA), adapted to the specifications of a CubeSat. This wheel has two purposes: by maintaining a constant speed, it will allow stiffening the corresponding axis by generating a gyroscopic effect. Disturbances can then be compensated by accelerating or decelerating the wheel, which will generate a torque on the satellite. The IWA is designed to be assembled in one side of the satellite, ensuring a maximal space remains available for the payload.
The specifications for the IWA are:
- Operating speed: 5000 – 11000 [rpm]
- Acceleration: 3000 [rpm/orbit] to compensate the worst-case disturbances
- Mean energy consumption: 100 [mW] (wheel and drive electronics)
- Mass: 32 [g] (19 [g] for the wheel and 13 [g] for the electronics)
- Dimensions: 80 [mm] diameter, 7 [mm] thickness, to be integrated in one side of the cube
The main points of this paper are:- Multi-parameter, non-linear optimization of the analytic model of a permanent magnet synchronous drive
- Validation using finite elements
- Key points for the design of an ad-hoc sensorless drive electronics
- Mechanical design, realization and assembly of prototypes
- Testing of the IWA
The focus being set on the use of novel optimization techniques to comply with very strict specifications.
- Abstract document
- Manuscript document
IAC-08.B4.6.A2.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.