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Control System Development And Response Analysis Of An Electronically Actuated Variable-Orifice Nozzle For Agricultural Pesticide Applications

机译:控制系统开发与响应分析 电子驱动可变孔的研究 农业杀虫剂应用的喷嘴

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摘要

The goal of this research project was to further the development of an electromechanically controlled variable-orifice nozzle by creating an electronic control system and then evaluating that system based on step and ramp inputs. The control system was developed in a programming environment that combined an electronic data acquisition system and actuator with pressure and flow sensors. A proportional, variable-gain (based on system pressure) control system was developed to adjust nozzle flow rates to meet target application rates. The constraints were to achieve settling time of less than 1.0 s, overshoot of less than 10% of maximum flow (or minimum flow), and average absolute steady-state error of less than 2%. After several trials, the resulting control system achieved these objectives for full steps from maximum andminimum flow rates (and vice versa) at carrier pressures from 140 to 410 kPa. Ramp response analyses revealed the maximum flow rate change (mL s-2) of the nozzle control system. Operation was considered successful if the average absolute error was less than 5% and the average absolute error +2σ did not exceed 10% of the desired flow, thereby ensuring that the nozzle operated within specifications 95% of the time. An additional goal was to maintain nozzle response lag times of less than 1.0 s based on input rate changes in the form of ramp signal input frequencies. Lag times were found to be less than 0.5 s (±0.05 s) over the carrier pressure range at input frequencies of up to 0.2 Hz. Further, these results indicated that for each carrier pressure, a maximum rate change frequency of 0.07 Hz ensured that system errors were within the design requirements. Lag times at this frequency were less than 0.38 s for all carrier pressures tested. The range of rate change achieved by the nozzle control system ranged from 2.97 to 6.39 mL s-2 for carrier pressures of 140 to 414 kPa, respectively. Thus, as operating pressure increased, the nozzle was capable of compensating for greater changes in the desired flow rate. While the turndown ratios (~2.4:1) over the range of carrier pressures were essentially stable, flow rates increased with carrier pressure.
机译:该研究项目的目的是通过创建一个电子控制系统,然后根据阶跃和斜坡输入对该系统进行评估,从而进一步开发机电控制的可变节流喷嘴。该控制系统是在编程环境中开发的,该环境将电子数据采集系统和执行器与压力和流量传感器结合在一起。开发了比例可变增益(基于系统压力)控制系统,以调节喷嘴流量以满足目标应用率。限制条件是要实现小于1.0 s的建立时间,小于最大流量(或最小流量)的10%的过冲以及小于2%的平均绝对稳态误差。经过几次试验,最终的控制系统在载气压力为140至410 kPa时,从最大和最小流速(反之亦然)实现了完整的目标。斜坡响应分析显示喷嘴控制系统的最大流量变化(mL s-2)。如果平均绝对误差小于5%,并且平均绝对误差+2σ不超过所需流量的10%,则认为操作成功,从而确保喷嘴在规定时间内95%的时间内运行。另一个目标是基于斜坡信号输入频率形式的输入速率变化,使喷嘴响应滞后时间保持小于1.0 s。发现在高达0.2 Hz的输入频率下,在载架压力范围内的滞后时间小于0.5 s(±0.05 s)。此外,这些结果表明,对于每个载气压力,最大速率变化频率为0.07 Hz,可确保系统误差在设计要求之内。对于所有测试的载气压力,该频率下的滞后时间均小于0.38 s。对于140至414 kPa的载气压力,喷嘴控制系统实现的速率变化范围分别为2.97至6.39 mL s-2。因此,随着工作压力的增加,喷嘴能够补偿所需流量的更大变化。尽管载气压力范围内的调节比(〜2.4:1)基本稳定,但流速随载气压力的增加而增加。

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