Small satellite attitude and orbital control for precise pointing missions
CovenanteePolitecnico di Torino
Document typeBachelor thesis
Rights accessOpen Access
Since spacecraft are subject to strict requirements in terms of angular position and actuation limits, advanced control algorithms are usually designed to combine robustness properties and limited control effort, including external disturbances and parametric uncertainties. The main objective of this research is the design of a control system for both orbit and attitude dynamics of a small spacecraft and carry out several simulations to evaluate the effectiveness of the used algorithms.
DegreeGRAU EN ENGINYERIA DE SISTEMES AEROESPACIALS (Pla 2015)