一种基于MRAC的航空金属切割误差补偿控制方法
本发明涉及一种基于MRAC的航空金属切割误差补偿控制方法,包括以下步骤:将棒料均分为k段,并通过激光测径仪测量每段棒料直径,根据整根棒料的体积得到棒料的密度;根据棒料的密度和需求质量,获取参考切割位置;使用梯度优化算法计算目标函数的梯度,更新自适应控制器的参数,对棒料进行切割。本发明利用梯度优化算法对控制器参数进行优化,确保系统输出能够快速、准确地跟随参考模型的输出,通过自适应律实时更新控制器参数,增强了系统的动态响应能力和抗干扰能力。
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