This paper discusses the design and development of an Attitude Determination and Control
System (ADCS) for the first Uruguayan nanosatellite, AntelSat, which is being built at …

The picosatellite UWE-3 is the third generation of CubeSats at the University Würzburg. It is
equipped with all necessary satellite systems, among them the attitude determination and …

The thesis work presented in this paper has been carried out between January and June
2016 under the scheme of the CubeSat Student Satellite Project MIST at KTH. I did it as a …

Prediction Algorithms for the Attitude Estimator The attitude estimator is an extended Kalman
filter, a recursive algorithm to treat noisy inputs to a dynamical system. The filter is optimal to …

The extended Kalman filter (EKF) algorithm has been applied widely in orbital guidance and
navigations problems for miniand micro-satellites. This paper evaluates the performance …

The attitude determination and control subsystem (ADCS) is a critical part of any satellite
conducting scientific experiments that require accurate positioning (such as Earth …

Un sistema de orientación activo para satélites es prioritario cuando se desea apuntar algún
instrumento, como una cámara para obtener imágenes de la superficie terrestre. Los …

Abstract The CubeSat Project has lowered development time and costs associated with
university satellite missions that conform to their 10 centimeter cube design specification …

In recent years, the industry of miniature satellite based on cubesat standard has been
growing rapidly. This growing industry has changed the direction of miniature satellite from …

This thesis describes the design, analysis and construction of the Attitude Determination and
Control System (ADCS) for the first Uruguayan nanosatellite, the AntelSat. The AntelSat …