基于FPGA的激光测速系统设计
[Abstract]:The initial velocity measurement technology of high speed flying objects has a very important role in promoting the development of modernization, whether in modern industrial production or in the frontier of scientific and technological research. For the study of the important characteristics of high speed flying objects, such as the motion performance, flight trajectory and flight attitude, the initial velocity of the high-speed flying object is measured. In this paper, based on the traditional laser ranging principle, this paper optimizes the traditional method of laser velocity measurement, develops a set of laser velocity measurement scheme with fast reaction time and high measurement precision, and realizes the velocity measurement for the launch of the spacecraft from the launcher. The system uses a high sensitivity, high reaction time photodiode to collect the laser signal. At the same time, through the preamplifier and the high-speed comparator, the signal filtering is adjusted by the preamplifier and the high-speed comparator. Finally, the edge change of the signal can be extracted successfully. Finally, the system using the FPGA+MCU as the core frame is used to signal the signal. In line processing, this not only further optimizes the speed measurement scheme, but also ensures the measurement accuracy of the system. Compared with the current widely used speed measuring system, the design of this system not only improves the accuracy of velocity measurement, but also responds to speed blocks in a relatively short time. The speed meter is easy to adjust, compact and portable, and is very suitable for measuring speed in various occasions. The research content of this subject is described mainly from seven aspects. (1) a simple analysis of various speed measuring methods is carried out, including coil speed measurement, radar velocity measurement, video velocity measurement, and GPS velocity measurement. And laser velocimetry. Two laser velocimetry. (2) based on the method of laser velocity measurement, based on the method of laser velocity measurement, according to the design requirements of the system, the original laser velocity measurement method is optimized. (3) the laser receiving module is designed, the photodiode is selected as the industrial NJL6201R-1, and its response speed Fast, superior performance, through the electric signal converted by photodiode through the preamplifier AD8015 and then through the high speed comparator ADCMP600 to carry out the signal shaping. A simple introduction to the chip is carried out, and the circuit design diagram of the whole module is given. (4) the design of the high precision timing module: the core of the FPGA chip, mining A pulse counting method is used to count the motion time of the spacecraft through a fixed distance. When the counting start pulse is received, the FPGA starts counting with its internal high precision clock until the stop count is received. (5) the design of the data processing module: when the MCU chip receives the interrupt signal at the end of the FPGA count, it begins. Read the value of FPGA, and process the data after receiving the data according to the established communication protocol. (6) the design of the wireless module: using the wireless transmission module of 433MHz, the wireless transmission chip to select Si4463, and transmit the related data to the coordinator through this module after the end of the MCU data processing. (7) the design of the module: on the one hand, through the module design The liquid crystal display screen LCD1602A displays the speed value after the microprocessor processing, and can operate according to the key to display the data stored in the flash; on the other hand, the related data transmitted over the wireless transmission module by the upper computer is displayed to facilitate the view. The speed range of this subject is measured at the speed range of: 0.36km/h~3600 Km/h, system error: less than 0.5%.
【学位授予单位】:成都理工大学
【学位级别】:硕士
【学位授予年份】:2017
【分类号】:TN249
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