Aeromagnetic Gradiometry and Its Application to Navigation


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详细

Modern methods of airborne magnetic field measurements are described. A stochastic algorithm to compensate the deviations between the indications of an aeromagnetometer and an aeromagnetic gradiometer is considered. An integration algorithm for the inertial and correlation-extremal navigation systems is briefly described. An advantage of using magnetic field gradient measurements as navigational data is justified. The performance of the integration algorithm is illustrated by numerical simulation.

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E. Karshakov

Trapeznikov Institute of Control Sciences

编辑信件的主要联系方式.
Email: karshak@mail.ru
俄罗斯联邦, Moscow

M. Tkhorenko

Trapeznikov Institute of Control Sciences

Email: karshak@mail.ru
俄罗斯联邦, Moscow

B. Pavlov

Trapeznikov Institute of Control Sciences

Email: karshak@mail.ru
俄罗斯联邦, Moscow

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