Engineering topics
Publications and source records attributed to Noe, P. S..
Derivation of a satellite in-view procedure and two satellite selection procedures are obtained and comparisons to previous procedures are presented. Two suboptimal satellite selection procedures - Quadrature System (QS) and Flexible Orthogonal System (FOS) - are compared to a suboptimal and optimum procedures, taking into account the execution time and Geometric Dilution of Precision (GDOP) of each.
A sequential navigation algorithm for a navigator using the Global Positioning System satellites is developed and tested for both noise-free and noisy system models. Data from a six-hour flight from California to Hawaii (C5A aircraft) simulates a true user to test the accuracy of the user's position for a sequential navigation system. For error reduction in the user's position in the sequential navigation system (considering 100 m as a maximum average error tolerated by any low-cost GPS user) an analysis of error sources in the sequential system has led to the use of range-ephemeris rate to translate ranges to a common point in time and to use velocity aiding at the time of a satellite disappearance. To reduce the user's position and velocity errors in a noisy navigation system an 'alpha-beta' two-pole filter is implemented whose optimum alpha is obtained experimentally. A user's position error of 73 m at noise range error of 30.48 (1sigma) is achieved.
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