基于状态相关riccati方程的三自由度直升机次优控制

Ahmet Cagri Arican, Sinan Ozcan, Bedrettin Mahmut Kocagil, U. M. Guzey, M. U. Salamci
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引用次数: 5

摘要

本文介绍了基于状态相关Riccati方程(SDRE)的非线性系统最优控制器设计的应用。在局部意义上设计最优控制器以最小化给定的二次性能指标,从而导致众所周知的线性二次调节器(LQR)问题,并且在每个采样时间更新最优控制器以应对非线性动力学。由于基于SDRE的最优控制器是通过将非线性系统冻结在某些采样周期来设计的,因此研究了采样周期对性能指标的影响。针对一架三自由度直升机的实验装置,设计了基于SDRE的最优控制器,并在不同工作频率的实验装置上实现。然后计算不同工作频率的性能指数和成本函数的值。实验研究表明,随着采样周期的增加,成本函数的值会减小。
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Suboptimal control of a 3 dof helicopter with state dependent riccati equations
The paper presents the application of State Dependent Riccati Equation (SDRE) based optimal controller design for nonlinear systems. Optimal controller is designed in local sense to minimize a given quadratic performance index, leading to well-known Linear Quadratic Regulator (LQR) problem and the optimal controller is updated at each sampling time to cope with the nonlinear dynamics. Since the SDRE based optimal controller is designed by freezing the nonlinear system at some sampling periods, the effect of sampling period on the performance index is studied. The SDRE based optimal controller is designed for an experimental setup of a 3 DOF Helicopter and implemented on the setup for different working frequencies. The performance index and therefore the values of the cost function is then computed for different working frequencies. Experimental studies reveals that an increased sampling period results in decreased value of the cost function.
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