Affiliation:
1. Air Force Institute of Technology
2. Gdańsk University of Technology
Abstract
Abstract
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.
Subject
Safety, Risk, Reliability and Quality
Reference9 articles.
1. 1. Camps A.: Nanosatellites and Applications to Commercial and Scientific Missions, Satellites Missions and Technologies Geocsiences, Barcelona 2019.
2. 2. Hajiyev Ch., Cilden Guler D.:Review on gyroless attitude determination methods for small satellites, Progress in Aerospace Sciences, Istambul 2017.
3. 3. Karatas S.: LEO Satellites: Dynamics Modelling, Simulations and some Nonlinear Attitude Control Techniques. Master’s thesis, Middle East Technical University 2006.
4. 4. Kouyama T. Kanemura A., Kato S., Imamoglu N., Fukuhara T.: Satellite Attitude Determination and Map Projection Based on Robust Image Matching, Remote sensing, Tokyo 2017.
5. 5. Kristiansen R.. Attitude Control Of a Microsatellite. Master Thesis, Department of Engineering Cybernetics, NTNU, 2000.