TY  - THES 
AU  - Marchante Arjona, Luis
PY  - 2018
UR  - http://hdl.handle.net/10481/53798
AB  - This Bachelor Thesis introduces a Theoretical Description and Simulink
implementation of di erent ADCS (Attitude Determination and Control
System), a fundamental feature of spacecrafts. As it makes possible to
control the orientation and stabilize...
LA  - eng
PB  - Prof. Andrés Roldán Aranda
KW  - GranaSAT
KW  - ADCS
KW  - simulink
TI  - GranaSAT-I: Kinematic and Dynamic Model for Attitude Determination and Control System
M3  - info:eu-repo/semantics/bachelorThesis
ER  -