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Constraint Enforcement Methods for Command Governor based Adaptive Control of Uncertain Dynamical Systems

机译:基于命令调控器的不确定动力系统自适应控制约束实施方法

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Recently, research has been conducted in order to improve the transient behavior of adaptively-controlled uncertain nonlinear dynamical systems. In this paper, an adaptive control architecture is extended in order to achieve predictable transient performance in the presence of state constraints. The methodology at hand is based on a robust command governor framework, which is a dynamical system adjusting the trajectory of a given command in order to track a certain desired closed-loop reference model both in transient time and steady-state. Specifically, the command, which is applied on the reference model and the actual system, is changed by the command governor framework for improved transient performance with respect to classical adaptive control schemes and by a constraint enforcement command in order to keep the states within pre-defined bounds. The constraint enforcement method here is able to handle state constraints in the range space of the control input matrix. The application of command governor and constraint enforcement on nonlinear dynamic inversion controllers is discussed and an example is implemented using a helicopter model for illustration purposes. An example using the wing rock dynamics shows the performance and additional methods for enforcing state constraints outside of the range space of the input matrix are also introduced.
机译:最近,已经进行了研究以改善自适应控制的不确定非线性动力学系统的瞬态行为。在本文中,对自适应控制体系结构进行了扩展,以便在存在状态约束的情况下实现可预测的瞬态性能。当前的方法基于健壮的命令调节器框架,该框架是一个动态系统,可调整给定命令的轨迹,以便在瞬态时间和稳态下跟踪某个所需的闭环参考模型。具体来说,适用于参考模型和实际系统的命令将通过命令调节器框架进行更改,以相对于传统的自适应控制方案改善瞬态性能,并通过约束执行命令进行更改,以将状态保持在预先设定的范围内。定义的界限。这里的约束实施方法能够处理控制输入矩阵的范围空间中的状态约束。讨论了指挥调节器和约束执行在非线性动态反演控制器上的应用,并以直升机模型为例进行了示例说明。使用机翼岩石动力学的示例显示了性能,并介绍了用于在输入矩阵的范围空间之外强制执行状态约束的其他方法。

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