The purpose of this simulation is to determine the accuracy performance capability of an aircraft positioning system based on the triangulation principle when combined with distance measuring equipment (DME), inertial elements and filtering (blending) of data from the various sensors. The simulation also determines how sensitive the overall system accuracy is to changes in certain key sensor parameters. (Author)
Simulation of Precision Aircraft Positioning System Utilizing Triangulation, DME and Inertial Smoothing Techniques
1978
142 pages
Report
No indication
English
Navigation Systems , Air Transportation , Position finding , Navigational aids , Aircraft equipment , Distance measuring equipment , Simulation , Triangulation , Bias , Comparison , Inertial systems , Mathematical filters , Accuracy , Weighting functions , Kalman filtering , Transformations(Mathematics) , Smoothing
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