Title :
An attitude control system for the deployment and stabilisation of a tethered dual CubeSat mission
Author :
Kearney, Mike-Alec ; Steyn, W.H.
Author_Institution :
Dept. of Electr. & Electron. Eng., Univ. of Stellenbosch, Stellenbosch, South Africa
Abstract :
The use of electrodynamic tethers on-board satellites is a promising scientific prospect. While the theory describing such systems have been studied by numerous scientists and mathematicians, practical testing of these systems have been relatively unsuccessful and test data concerning the topic is limited. Low-cost CubeSats offer a cheap platform from which practical tests can be done which would contribute to advancements in the field. The design of an attitude determination and control system for such a CubeSat tether mission is discussed in this paper. This includes the design of a sensor capable of measuring the orientation of the tethered CubeSat pair using a CMOS imager. Further, the study includes the design of an active deployment system, mathematical modeling of the system, formulation of control-algorithms for controlling the tether-orientation, and full orbital simulations of the system.
Keywords :
CMOS image sensors; aerospace simulation; artificial satellites; attitude control; control system synthesis; position control; space research; stability; CMOS imager; CubeSat tether mission; active deployment system; attitude control system; control system design; electrodynamic satellite tethers; low-cost CubeSats; mathematical modeling; orbital simulations; stabilisation; system testing; tethered CubeSat pair orientation; tethered dual CubeSat mission deployment; Electrodynamics; Force; Mathematical model; Oscillators; Satellites; Torque; Vectors; Attitude; Control; CubeSat; Tether;
Conference_Titel :
AFRICON, 2013
Conference_Location :
Pointe-Aux-Piments
Print_ISBN :
978-1-4673-5940-5
DOI :
10.1109/AFRCON.2013.6757729