The research into correction algorithms for aircraft navigation systems

We consider the schemes of correction navigation systems and systems of aircraft complexes. To correct the navigation data, we use the adaptive modification of the linear Kalman filter, a method of self-organization and a genetic algorithm. We propose to carry out the high-precision correction by the nonlinear Kalman filter, modified by a genetic algorithm. Moreover, we present a selective navigation system, allowing us to select the best configuration of measuring systems on board the aircraft. As a result, we prove the efficiency of algorithmic maintenance of navigation systems and complexes.

References

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