Control moment gyro actuator for small satellite applications

Berner, Reimer (2005-03)

Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005.

Thesis

The aim of the thesis is to design a Control Moment Gyro (CMG) actuator which can be used in small satellite applications. The hardware and software of the CMG has to be designed according to specifications given. A satellite fitted with these CMGs has to be able to do a 30 degree rotation within 10 seconds.

Please refer to this item in SUNScholar by using the following persistent URL: http://hdl.handle.net/10019.1/2144
This item appears in the following collections: