Airborne motion platform magnetic disturbance compensation method without influence of geomagnetic variation
A motion platform and compensation method technology, applied in the field of aeromagnetic detection, can solve problems such as failure of aeromagnetic interference compensation coefficients
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specific Embodiment approach 1
[0091] Specific Embodiment 1: A magnetic interference compensation method for an aeronautical motion platform that is not affected by geomagnetic changes in this embodiment is implemented according to the following steps: figure 1 :
[0092] Step 1, collecting the total magnetic field data to obtain the geomagnetic field;
[0093] Step 2, using the obtained geomagnetic field to obtain a compensation coefficient φ independent of the geomagnetic field;
[0094] Step 3, use the compensation coefficient irrelevant to the geomagnetic field to obtain the magnetic interference compensation result res=H generated by the aviation motion platform total -Ht, where H Total is the total magnetic field, H t for magnetic interference.
specific Embodiment approach 2
[0095] Embodiment 2: This embodiment is different from Embodiment 1, and it is characterized in that the total magnetic field data in Step 1 is collected by a total field magnetometer and a three-component magnetometer.
specific Embodiment approach 3
[0096] Specific embodiment three: present embodiment is different from specific embodiment one or two, and it is characterized in that described step 1 gathers total magnetic field data, obtains geomagnetic field data as follows:
[0097] The total magnetic field measured by the total field magnetometer is H Total , which mainly includes the geomagnetic field He and the three kinds of magnetic disturbance Ht generated by the aircraft motion platform, specifically including the constant field H per , induction field H induce and eddy current field H eddy ,As follows:
[0098] Ht=H per +H induce +H eddy (10)
[0099] in, H p e r = p 1 p 2 p 3 ...
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