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Exponential Mapping Controller Applied to Aircraft

机译:应用于飞机的指数映射控制器

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A novel modified exponential function to achieve tracking and regulatory direct and indirect model-free feedback control of a class of nonlinear dynamical systems is presented. Its simplicity was a requisite to have it run on equipment and devices with memory and processor constraints. The control algorithm needs only two parameters and can be applied to systems based on knowledge about its free response and expected disturbances. Its main advantages are relative ease of implementation and intuitive tuning. The controller is applied to the simulation of two different aircraft under stochastic winds and wind shear and its results are compared to a classical implementation. EMC presented promising results. Its intuitive form of parameterization allowed in some cases for immediate good results or at least for good initial estimatives for later tuning.
机译:提出了一种新的改进的指数功能,实现了一类非线性动力系统的实现跟踪和调节直接和间接无模型反馈控制。它的简单性是它在具有内存和处理器约束的设备和设备上运行的必要条件。控制算法仅需要两个参数,可以基于关于其自由响应和预期干扰的知识应用于系统。其主要优点是相对易于实现和直观调整。控制器应用于在随机风中的两个不同飞机的模拟,并且风剪,其结果与经典实施相比。 EMC提出了有希望的结果。在某些情况下,它允许其直观的参数化形式,以便立即进行良好的效果,或者至少适用于较晚的初始预算。

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