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Design of New Attitude Measuring Method of Non-Spinning Projectile Based on Magnetic Sensors

机译:基于磁传感器的非旋转弹丸姿态测量新方法设计

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Because of the requirement of accurate measurement of projectile's flying characteristics and limitations of the traditional attitude measuring methods, a new method based on three pairwise-orthogonal magnetic sensors only is presented for non-spinning projectiles.The characteristic ratio theory proposed in our earlier work is described in detail.In order to get the pitch angle with this theory, the mathematical relationship between magnetic sensors output and the theoretical extreme value is derived in this paper.Based on this relation, the extremum ratio method is expanded to be used in non-spinning projectiles.The measurement error of the attitude measuring method is also analyzed in theoy.At last, the simulation of the method is achieved under the given conditions to prove its effectiveness.The simulation experiment results indicate that the method is feasible and the calculating errors of the attitude angles are within ± 1°.
机译:由于精确测量弹丸飞行特性的要求以及传统姿态测量方法的局限性,提出了一种仅基于三个成对正交磁传感器的非旋转弹丸新方法。为了得到该理论的俯仰角,本文推导了磁传感器输出与理论极值之间的数学关系。最后,在给定条件下对该方法进行了仿真,证明了该方法的有效性。仿真实验结果表明,该方法是可行的,并且计算误差较大。姿态角的误差在±1°之内。

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