深空天线方位位置控制的模糊pid控制器

Halima S. Yakubu, S. Hussein, Gokhan Koyunlu, E. Ewang, S. Abubakar
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摘要

摘要:深空天线是实现超远距离通信的关键。然而,该天线的指向精度需要尽可能精确,以实现与卫星的有效通信。因此,本文采用模糊pid控制技术,通过改善系统的性能目标(稳定时间、超调上升时间百分比和主要的稳态误差)来解决深空天线的指向精度问题。本文首先对系统的PID控制器进行了设计和仿真,然后分别利用MATLAB和Simulink对模糊控制器进行了设计和仿真,与模糊-PID控制器进行了比较。然后,利用MATLAB和Simulink对系统的模糊PID控制器进行了设计和仿真,其性能目标(上升时间1.0057s,稳定时间1.6019s,超调率1.8013,稳态误差2.195 -6)分别优于PID控制器和模糊控制器。因此,稳态误差表明指向精度提高到2.195 -6。关键字/
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fuzzy-PID Controller for Azimuth Position Control of Deep Space Antenna
Abstract: The Deep Space Antennas are essential in achieving communication over very large distances. However, the pointing accuracy of this antenna needs to be as precise as possible to enable effective communication with the satellite. Therefore, this work addressed the pointing accuracy for a Deep Space Antenna using Fuzzy-PID control technique by improving the performance objectives (settling time, percentage overshoot rise time and mainly steady-state error) of the system. In this work, the PID controller for the system was first of all designed and simulated after which, a fuzzy controller was also designed and simulated using MATLAB and Simulink respectively for the sake of comparison with the fuzzy-PID controller. Then, the fuzzy-PID controller for the system was also designed and simulated using MATLAB and Simulink and it gives a better performance objective (rise time of 1.0057s, settling time of 1.6019s, percentage overshoot of 1.8013, and steady-state error of 2.195e-6) over the PID and fuzzy controllers respectively. Therefore, the steady state error shows improved pointing accuracy of  2.195e-6. Keywords/
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