Essays about: "NetSat"
Found 4 essays containing the word NetSat.
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1. Further Development of a Distributed Robust Control Approach towards a Nanosatellite Formation Flying Application
University essay from Luleå tekniska universitet/RymdteknikAbstract : This thesis proposes a distributed robust control approach for low-thrust nanosatellite formation flying. The presented control approach is the further development of an already existing approach which combines robust control and distributed control using the consensus approach. READ MORE
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2. Design and analysis of mission and system requirements for 'NetSat' mission with respect to structural and thermal limitations
University essay from Luleå tekniska universitet/RymdteknikAbstract : In the scope of this master thesis work, the proposed design for NetSat was analyzed for mission and system requirements with respect to structural and thermal limitations. Different load case scenarios for structural and thermal analysis were considered during the process which have been discussed. READ MORE
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3. Constrained Low-Thrust Satellite Formation-Flying Using Relative Orbit Elements : Autonomous Guidance and Control for the NetSat Satellite Formation-Flying Mission
University essay from Luleå tekniska universitet/Institutionen för system- och rymdteknikAbstract : This thesis proposes a continuous low-thrust guidance and control strategy for satellite formation-flying. Stabilizing feedback based on mean relative orbit elements and Lyapunov theory is used. A novel feedback gain matrix inspired by the fuel-optimal impulsive solution is designed to achieve near-optimal fuel consumption. READ MORE
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4. Relative Orbit Propagation and Control for Satellite Formation Flying using Continuous Low-thrust
University essay from Luleå tekniska universitet/Institutionen för system- och rymdteknikAbstract : For the upcoming formation flying technology demonstration mission NetSat a relative orbit propagator as well as a relative orbit controller were developed. The formation will consist of four equal nano-satellites with an electric propulsion system for orbit correction manoeuvres. READ MORE