Aeromagnetic compensation method based on non-linear aeromagnetic total field gradient compensation model
A compensation method and field gradient technology, applied in the field of geophysical aeromagnetic exploration, can solve the problems of asynchronous working clock, compensation deviation, difficult to achieve strict synchronization of real-time data, etc., to achieve the effect of improving accuracy and solving the compensation problem of disturbing magnetic field
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[0025] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in further detail below in conjunction with specific embodiments and with reference to the accompanying drawings.
[0026] The aeromagnetic total field gradient compensation model is derived based on the aeromagnetic compensation model. At any position of the optical pump magnetometer probe, the total interference field of the aircraft is represented by the following aeromagnetic compensation model:
[0027]
[0028] In the formula, c i is the magnetic compensation coefficient of the total magnetic field, H d (t) is the total interference field at the optical pump magnetometer probe, H e is the total field modulus of the geomagnetic field, A i (t) is the characteristic element in the aeromagnetic compensation model, and the expression of the characteristic matrix A(t) composed of characteristic elements is as follows:
[0029] A(...
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