A Verification Method of Missile-borne Geomagnetic Attitude Measurement Processing Algorithm
A technology for processing algorithms and verification methods, applied in directions such as ground navigation
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[0035] The technical solution of the present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.
[0036] A verification method for a missile-borne geomagnetic attitude measurement processing algorithm, comprising the following steps: designing a ground simulation turntable debugging device 100, which can carry a load of more than 20kg, and the device is composed of a sensor 101, a reference 102, a gear box 103, a servo motor 104, and a rotating shaft 105. The mechanical platform composed of bearing housing 106, crank handle 107, flat plate 108, base 109, support rod 110, elastic device 111, support seat 112, shift fork 113 and flange plate 114 can carry ≤15kg heavy parts and can be pitched and rolling motion, pitch angle movement range ±45°; roll angular velocity: 0-1800° / s; the shell control cabin with geomagnetic attitude measurement device is connected with flange 114 through bolts, driven by a servo mo...
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