In the last decade, there has been a significant increase in the use and launch of small satellites. Initially, universities dominated the field, launching small satellites for use in scientific research or as technological demonstrators. However, there has been a gradual increase in the number of small satellites launched for commercial purposes. Consequently, these platforms are now required to deliver increasingly better performance due to the growing number of commercial applications they can serve. Given the current state of the space sector, significant research efforts have been dedicated to the study, simulation, improvement, and utilization of the different subsystems that make up small satellites.
This doctoral thesis focuses on the modelling, study, and simulation of the power subsystem and the attitude determination and control subsystem embedded in small satellites, while exploring the relationship between these subsystems. Although the primary emphasis is on small satellites, the application of the results is not limited to them.
This thesis covers several key studies. First, it investigates the performance comparison between power systems that use Direct Energy Transfer (DET) configurations and those that use Maximum Power Point Tracking (MPPT). Secondly, this work explores the estimation of the solar vector using low-cost solar sensors based on photodiodes, as well as the use of the state of solar panels for this purpose. Additionally, this thesis develops data analysis methodologies related to satellite.
attitude, enabling the determination of the satellite’s angular velocity even in situations with very slow data rates compared to the characteristic period of its motion. Finally, a guidance law is formulated to optimize the pointing of the satellite’s solar panels toward the Sun while respecting the maximum deviation constraint of its instruments from the target direction.
All the studies and analyses conducted in this thesis are derived from the experience with the UPMSat-2 and the development of the UPMSat-3. Data from the UPMSat-2, launched in September 2020, has been used to validate the methodologies described in this work, and specific methods have been implemented to validate experiments carried out on board the UPMSat-2. On the other hand, the UPMSat-3, currently in the development phase, has served as a basis for creating case studies to test and develop, for example, new solar tracking algorithms.