IEEE Transactions on Aerospace and Electronic Systems · 2001 · 75 citations · 3 references
ComputingAerospace EngineeringComputer ScienceAlgorithmsGlobal Navigation Satellite SystemsOptimizationGeometric OptimizationSatellite OrbitsDilution Of PrecisionGeometric DilutionIntegrityOptimality Criteria
The author addresses the problem of selecting an optimum n-satellite subset from m visible satellites (m>n). The optimality criteria is minimum geometric dilution of precision (GDOP) subject to the integrity constraint. To solve this problem an efficient algorithm is developed using a revolving door method and matrix inversion lemma. The revolving door method generates each n-subset from its immediate predecessor by deleting some single element and adjoining some other single element. Then using the matrix inversion lemma, the GDOP for each new n-subset is recursively calculated from the incoming and outgoing elements. The matrix inversion lemma is also used to check the satisfaction of the integrity constraint.
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Jarmo Alanen · Proceedings of the IEEE · 1977 · 258 citations