小型无人机角参数组合传感器

2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI:10.1109/MSNMC.2014.6979729

M. Filyashkin

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引用次数: 0

摘要

给出了测量角度参数的组合传感器的原理，该传感器可用于补偿法或基于简化卡尔曼滤波的惯性卫星系统。利用该方法研究了飞机在不同机动状态下、加速度和姿态变化情况下的角定向参数测量误差。

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Combined sensor of angular parameters for small unmanned aerial vehicles

Are given principles of the combined sensor which measures the angular parameters and is used in inertial-satellite systems constructed by the method of compensation or based on the reduced Kalman filter. Measurement errors of angular orientation parameters are investigated by the proposed method with aircraft performing various maneuvers and with changing the acceleration and attitude.

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来源期刊

2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)

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