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Antenna for precise orbit determination
Authors:Johan Wettergren  Magnus Bonnedal  Per Ingvarson  Bo Wstberg
Institution:aRUAG Aerospace Sweden, SE-405 15 Göteborg, Sweden;bEFIELD AB, Box 87, SE-164 94 Kista, Sweden
Abstract:The ESA SWARM mission will consist of three satellites that will measure the Earth magnetic field. The system calls for metre accuracy knowledge of the measurement locations. To achieve this a GPS receiver is used. At least four GPS signals are tracked to determine the code and carrier ranges, from which the position can be derived. The accuracy improves when using more GPS satellites and by averaging over many measurements. The latter is achieved in ground processing with a model-based orbit prediction, resulting in cm accuracy. The main error contributions in the processing are often measurement errors due to satellite multi-path effects. The multipath effects are characterized by measuring the antenna on a 1.5 m mock-up, representing the 9 m long satellite. In order to verify that the mock-up is representative, extensive electromagnetic simulations were made. The simulations included the antenna and the complete satellite and were then reduced to the antenna and a section of the satellite. The actual design of the antenna was performed with several levels of software. First, a fast bodies-of-revolution simulation found a geometry with the right coverage. Then, a finite element method simulation allowed us to match the antenna at two frequencies simultaneously.
Keywords:Antenna  Space  GPS  SWARM  ESA  Design  Simulation  RUAG
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