Shell-borne geomagnetic attitude measurement and processing algorithm
A technology for processing algorithm and magnetic attitude, applied in the field of missile-borne geomagnetic attitude measurement and processing algorithm
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[0036] The technical solution of the present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.
[0037] A missile-borne geomagnetic attitude measurement processing algorithm, comprising the following steps: the missile-borne dual-axis geomagnetic sensor is fixed on the missile body, perpendicular to the direction of the missile axis, sensitive to the change of reluctance in the Y and Z directions, and the specific installation is urgently related to the coordinates of the missile body Such as figure 1 shown.
[0038] Taking the Beidongtian navigation coordinate system as a reference, x′ b for x b For the projection on the NOE plane, γ is the roll attitude angle of the projectile, β is the yaw angle (shooting direction), and θ is the pitch angle (shooting angle). According to the coordinate transformation, the geomagnetic output in the Y and Z directions of the projectile is obtained:
[0039]
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