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Correction of the inertial navigation system using a genetic algorithm
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The problem of compensating errors for an inertial navigation system with an unstable signal of a satellite navigation system is considered. The error model of the inertial navigation system, with the help of which its errors are predicted is built under the conditions of the signals disappearance from the satellite navigation system. The prediction of inertial navigation system errors are used for correction in the output signal. Predictive models are built using a genetic algorithm. Correction for small unmanned aerial vehicles, it is proposed to carry out using a scalar model of inertial navigation system errors and generated reduced measurements.
Keywords
aircraft, inertial navigation system, satellite navigation system, correction, genetic algorithm, reduced measurements
Title: Correction of the inertial navigation system using a genetic algorithm
Description:
The problem of compensating errors for an inertial navigation system with an unstable signal of a satellite navigation system is considered.
The error model of the inertial navigation system, with the help of which its errors are predicted is built under the conditions of the signals disappearance from the satellite navigation system.
The prediction of inertial navigation system errors are used for correction in the output signal.
Predictive models are built using a genetic algorithm.
Correction for small unmanned aerial vehicles, it is proposed to carry out using a scalar model of inertial navigation system errors and generated reduced measurements.
Keywords
aircraft, inertial navigation system, satellite navigation system, correction, genetic algorithm, reduced measurements.
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