Liu Jun, Zhao Donghua, Wang Chenguang, Yang Jiangtao, Guo Xiaoting, Tang Jun, Shen Chong
Key Laboratory of Instrumentation and Science and Dynamic Measurement, Ministry of Education, School of Instrument and Electronics, North University of China, Taiyuan 030051, People's Republic of China.
Rev Sci Instrum. 2019 Jan;90(1):015009. doi: 10.1063/1.5056195.
In the natural world, insects such as bees and sand ants can navigate with the aid of polarized skylight. Inspired by this, bio-inspired navigation systems based on polarized skylight have attracted considerable attention recently. As an important navigation parameter, attitude information is critical for control and navigation of a vehicle. In this paper, the structural characteristics of full-sky atmospheric polarization mode are studied to calculate the attitude of a vehicle relative to the observation point. The heading angle is obtained by subtraction between two angles. One is the angle between the solar meridian and the geographic north. The other is the angle between the solar meridian and the body coordinate system, which can be obtained from the polarization data detected by the sensor. And the solar position can also gain from the polarization data. Then based on the solar position and the coordinates of solar projection point, the zenith point can be determined. With the coordinates of the zenith point in the body and the reference coordinate system, the pitch angle and roll angle are solved. Simulation and practical experiments are conducted to validate the performance of the attitude calculation method. Experiment results with high accuracy show its feasibility and effectiveness.
在自然界中,蜜蜂和沙蚁等昆虫能够借助偏振天空光进行导航。受此启发,基于偏振天空光的仿生导航系统近年来备受关注。姿态信息作为一个重要的导航参数,对于飞行器的控制和导航至关重要。本文研究了全天空大气偏振模式的结构特征,以计算飞行器相对于观测点的姿态。航向角通过两个角度相减得到。一个是太阳子午线与地理北极之间的夹角。另一个是太阳子午线与机体坐标系之间的夹角,可从传感器检测到的偏振数据中获取。并且太阳位置也可从偏振数据中得到。然后基于太阳位置和太阳投影点的坐标,确定天顶位置。利用天顶位置在机体坐标系和参考坐标系中的坐标,求解俯仰角和滚转角。进行了仿真和实际实验以验证姿态计算方法的性能。高精度的实验结果表明了该方法的可行性和有效性。