高精度力促動器控制系統(tǒng)的設(shè)計
[Abstract]:Telescope is an important tool for astronomical observation. The larger the aperture, the stronger the ability of collecting light and the higher the resolution. With the increase of aperture, the primary mirror will be affected by wind, temperature, gravity and other factors, which will produce certain changes in plane shape, which will affect the imaging quality of the telescope. Therefore, it is necessary to control the main mirror shape in real time. Factors such as temperature and gravity influence the mirror surface to improve the imaging quality. In large ground-based telescopes, the real time control of the main mirror can be realized by controlling the force actuators in the active optical system. In recent years, active optics has become one of the most important technologies in large ground-based telescope systems. It belongs to the intersection fields of automatic control, precision machinery, computer and optics. Its principle is to detect the surface distortion of the mirror through the wavefront sensor, and calculate the correction force and its coordinates based on it, and then pass the required correction force value to the corresponding force actuator through the bus. Thus, the force actuator exerts pressure or tension to realize the active adjustment of the supporting force and achieve the purpose of controlling the shape of the plane. The main content of this paper is the hardware and software design of the force actuator control system. The paper is divided into four parts: in the first part, the working principle and mechanical structure of the force actuator are introduced, and the control system scheme of the force actuator is designed, and the expected parameters of the system are given. In the second part, the hardware circuit of the control system is designed, including the system power circuit, the force signal acquisition circuit, the motor driving circuit and the force actuator control circuit, and the system experimental platform is built. In the third part, the advantages and disadvantages of the closed-loop control strategy in the force actuator control system are analyzed, and the design of the variable speed integral PID controller with dead-time is completed. Then, the software design method of force actuator control system is introduced, and the detailed program flow chart is completed. In the fourth part, the performance test of the force actuator control system is completed, and the experimental results are analyzed, including the force actuator control experiment, the force acquisition circuit conversion precision test and calibration, and the force actuator performance test. It can be seen from the experimental results that the system can work according to the expected mode, can meet the precision requirements of the correction force of the main mirror shape, and has better response performance and engineering practical value to a certain extent.
【學(xué)位授予單位】:中國科學(xué)院長春光學(xué)精密機械與物理研究所
【學(xué)位級別】:碩士
【學(xué)位授予年份】:2016
【分類號】:TP273
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