Abstract:
An optimal algorithm for pointing a steerable satellite spot beam is described. The optimality criterion considered is maximization of the number of Earth terminals cover...Show MoreMetadata
Abstract:
An optimal algorithm for pointing a steerable satellite spot beam is described. The optimality criterion considered is maximization of the number of Earth terminals covered. The computation time of the algorithm has been compared with a brute force algorithm through a series of Monte Carlo trials.
Published in: IEEE Transactions on Aerospace and Electronic Systems ( Volume: 32, Issue: 3, July 1996)
DOI: 10.1109/7.532284
