L1_AC:这是一个使用MATLABSimulink [L1自适应控制代码]设计和测试基于L1自适应控制的自适应飞行控制的项目。-源码

上传者: 42131276 | 上传时间: 2021-05-25 21:10:19 | 文件大小: 6.02MB | 文件类型: ZIP
L1_AC 在这个项目中,使用MATLAB / Simulink I从非线性飞机模型开始设计并测试了基于L1自适应控制的自适应飞行控制。 包含的描述在simulink MATLAB / Function内部 飞机参数(NOMINAL)由INIT.m设置。在某些给定条件下,按照TAS和姿态(仅是平稳状态飞行)修剪飞机。TRIM.m脚本返回使飞机保持在一定高度所需的输入。给定的飞行条件。 L1AC以线性系统表示形式工作,因此系统在调整后的条件附近线性化。 动态和控制矩阵A和B通过“ estrai.m”提取 然后,POLE_PLACEMENT.m使用A和B矩阵计算横向和纵向动力学的反馈矩阵K 控制律参数的设计是脚本TEST_NAVION和TEST_NAVION_LAT的工作 PLOTTING.m在单个图中绘制主要状态变量PLOTTING2.m在子图中绘制主要状态变量PLOTTING3.m在子

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