- Journal Details
- Format
- Journal
- First Published
- 26 Feb 2008
- Publication timeframe
- 4 times per year
- Languages
- English
Nanosatellites, although originally developed for educational purposes, are increasingly being used for commercial sense. Continuous increase in the application and use means that they require continuous improvement of performance to cope with new challenges. An important issue is the control of the position of the satellite sufficiently accurate and fast to enable it to efficiently carry out its mission. This paper includes a project consisting of a modelled test system and a presented method of control with simulation. Then, the obtained results and resulting conclusions are discussed.
Keywords
- nanosatellite
- reaction wheels
- control system
Diagnostics of Turbine Blades, Based on Estimation of Frequency Response Function The Impact of Standard Deviation of Wind on the Bomb Flight in Atmospheric Turbulence Efficiency Analyse of Airport Commercial Area Use of Electric Motors in the Context of Glider Aviation Small UAV SHM System Functional Hazard Analysis Aviation Criminal Law Regulations of the Tokyo Convention and the Penal Code to Counteract Terrorist Acts Preliminary System Safety Hazard Analysis of a Transport Helicopter SHM System Measures Taken by the European Union Agency for Aviation Safety to Ensure Aviation Safety Reaction Wheel Control System for Cubesat Nanosatellite The Impact of Technological Changes of PVC Light Partitions and Glazing on the Risk Connected with the Organization of International Transport Checking Aircraft Engines Adjustment Federated Learning for Spanish Ports as an Aid to Digitization