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A new adaptive control scheme based on the interacting multiple model (IMM) estimation

机译:基于交互多模型(IMM)估计的新的自适应控制方案

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In this paper, an Interacting multiple model (IMM) adaptive estimation approach is incorporated to design an optimal adaptive control law for stabilizing an Unmanned vehicle. Due to variations of the forward velocity of the Unmanned vehicle, its aerodynamic derivatives are constantly changing. In order to stabilize the unmanned vehicle and achieve the control objectives for in-flight conditions, one seeks for an adaptive control strategy that can adjust itself to varying flight conditions. In this context, a bank of linear models is used to describe the vehicle dynamics in different operating modes. Each operating mode represents a particular dynamic with a different forward velocity. These models are then used within an IMM filter containing a bank of Kalman filters (KF) in a parallel operating mechanism. To regulate and stabilize the vehicle, a Linear quadratic regulator (LQR) law is designed and implemented for each mode. The IMM structure determines the particular mode based on the stored models and in-flight input-output measurements. The LQR controller also provides a set of controllers; each corresponds to a particular flight mode and minimizes the tracking error. Finally, the ultimate control law is obtained as a weighted summation of all individual controllers whereas weights are obtained using mode probabilities of each operating mode.
机译:本文采用一种交互多模型(IMM)自适应估计方法来设计用于稳定无人车辆的最优自适应控制律。由于无人飞行器前进速度的变化,其空气动力学导数不断变化。为了使无人飞行器稳定并达到飞行状态的控制目标,人们寻求一种自适应控制策略,该策略可以使其自身适应变化的飞行条件。在这种情况下,一组线性模型用于描述不同运行模式下的车辆动力学。每个运行模式代表具有不同前进速度的特定动态。这些模型然后在包含并行操作机制中的一组卡尔曼滤波器(KF)的IMM滤波器中使用。为了调节和稳定车辆,针对每种模式设计并实施了线性二次调节器(LQR)定律。 IMM结构基于存储的模型和飞行中的输入输出测量值来确定特定模式。 LQR控制器还提供了一组控制器。每个都对应于特定的飞行模式,并使跟踪误差最小。最后,最终控制律是所有单个控制器的加权总和,而权重是使用每种操作模式的模式概率获得的。

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