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Method for improving the accuracy of aircraft navigation system using the Kalman filter
| Authors: Hu Yuhui, Ma Deng | Published: 03.10.2019 |
| Published in issue: #9(38)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-9-529 | |
| Category: Informatics, Computer Engineering and Control | Chapter: System Analysis, Control, and Information Processing, Statistics | |
| Keywords: Kalman filter, aircraft, Gaussian white noise, inertial navigation system, GPS, error of navigation systems, forecast, error compensation | |