Title: Aircraft Positioning with INS/GNSS Integrated System
Abstract: The paper describes methods of INS/GNSS integration and rules of designing Kalman filters. An example of INS/GPS positioning system is presented. The system employs a Complementary Linearized Kalman Filter, estimating INS position, velocity and attitude errors, as well as GPS clock bias and drift. Chosen simulation results, comparing accuracy of INS, GPS and INS/GPS are included.
Publication Year: 2006
Publication Date: 2006-01-01
Language: en
Type: article
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Cited By Count: 10
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