Essays about: "Orbital Control Simulation"
Showing result 6 - 10 of 10 essays containing the words Orbital Control Simulation.
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6. An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit
University essay from Luleå tekniska universitet/Institutionen för system- och rymdteknikAbstract : Cubesats are picosatellites that have a mass of less than 1.3kg and have a shape of acube. As a result of their low cost of development and launch, cubesats are gainingpopularity in industry and academia. These satellites are also a cost-efective way forspace technology demonstrations. READ MORE
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7. Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos
University essay from Luleå tekniska universitet/RymdteknikAbstract : Asteroid missions are gaining interest from the scientific community and many new missions are planned. The Didymos binary asteroid is a Near-Earth Object and the target of the Asteroid Impact and Deflection Assessment (AIDA). READ MORE
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8. Mission Concept for a Satellite Mission to Test Special Relativity
University essay from Luleå tekniska universitet/Institutionen för system- och rymdteknikAbstract : In 1905 Albert Einstein developed the theory of Special Relativity. This theory describes the relation between space and time and revolutionized the understanding of the universe. While the concept is generally accepted new experimental setups are constantly being developed to challenge the theory, but so far no contradictions have been found. READ MORE
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9. Modelling and Simulation ofGNC/AOCS Systemsfor Conceptual Studies
University essay from KTH/MekanikAbstract : The preliminary design of Guidance, Navigation, and Control (GNC) algorithms andAttitude and Orbital Control Systems (AOCS) for spacecraft plays an important rolein the planning of a space mission. Many missions require accurate positioning andattitude control to be able to full the mission objectives. READ MORE
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10. Preliminary Mission Analysis and Design for a Small Satellite SWARM
University essay from KTH/Rymd- och plasmafysikAbstract : The thesis is a preliminary mission analysis and design of a small satellite swarm. The concept of the mission is to probe altitudes between 200 km and 6000 km to study the structures and dynamics of the magnetic field aligned currents. The mission lifetime is about 3 months. READ MORE