基于模糊逻辑的GPS天线跟踪器PID参数自整定控制

Ahmad Riyandi, S. Sumardi, T. Prakoso
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引用次数: 4

摘要

移动车辆需要一个天线进行通信,该天线放置在车辆和地面站(地面控制站,GCS)。一般来说,GCS使用配备有驱动系统的定向天线,该驱动系统具有传统的比例、比例积分或比例积分微分(PID)控制,以及基于接收信号强度指示器(RSSI)的步进跟踪算法。本研究采用基于全球定位系统(GPS)的模糊逻辑整定PID控制方法对地面军事系统的定向天线进行控制。由此产生的天线跟踪器系统能够跟踪方位角和仰角最小误差为0°的物体,对于速度为49公里/小时的物体,最大误差为49°。该系统在方位角处的平均上升时间为0.7秒,在仰角处的平均下降时间为1.08秒。该系统可用于控制移动车辆的天线方向,如无人机和火箭。
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PID Parameters Auto-Tuning on GPS-based Antenna Tracker Control using Fuzzy Logic
The moving vehicles require an antenna to communicate which is placed on the vehicles and at the ground station (ground control station, GCS). Generally, GCS uses a directional antenna equipped with the drive system with the conventional proportional, proportional-integral, or proportional-integral-derivative (PID) control, and step-tracking algorithms based on the received signal strength indicator (RSSI). This research used PID control method tuned with fuzzy logic based on Global Positioning System (GPS) to control a directional antenna at GCS. The resulting antenna tracker system was capable of tracking objects with a minimal error of 0° at azimuth and elevation angle and had a maximal error of 49° for a 49 km/hour speed object. The system had an average rise time of 0.7 seconds at an azimuth angle and 1.08 seconds at an elevation angle. This system can be used to control antenna direction for moving vehicles, such as an unmanned aerial vehicle (UAV) and rocket.
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