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NAVIGATION WITH HIGH-ALTITUDE SATELLITES: A STUDY OF ERRORS IN POSITION DETERMINATION
In this report we investigate the accuracy with which the position of a receiver can be determined by use of a high-altitude satellite navigation system. The navigation system is modelled as a problem of nonlinear estimation in the presence of random disturbances. Equations are derived for describing positioning errors by using linearization and the Kalman-Bucy filtering equations.doi:10.21236/ad0648828 fatcat:yy62hvgwybebtkgalzbi5zq2hq