控制理论(社会学)
控制器(灌溉)
运动模拟器
运动学
模拟
斯图尔特站台
仿真
计算机科学
加速度
控制工程
过程(计算)
李雅普诺夫函数
反馈线性化
线性化
补偿(心理学)
工程类
控制(管理)
人工智能
运动(物理)
非线性系统
生物
操作系统
经典力学
物理
量子力学
经济增长
经济
心理学
精神分析
农学
作者
Mojtaba Eftekhari,Hossein Karimpour
出处
期刊:Robotica
[Cambridge University Press]
日期:2018-01-22
卷期号:36 (4): 588-606
被引量:6
标识
DOI:10.1017/s0263574717000662
摘要
SUMMARY This paper presents a model-based controller consisting of a feedback linearization scheme and a state-dependent proportional derivative (PD) controller adapted to a parallel flight simulator Stewart mechanism. This parallel robot is considered to emulate motions of highly maneuverable aircrafts, which require well-trained pilots. The simulations are based upon a reduced-model prototype built in order to verify kinematic design aspects and control laws. Indeterminacies in the mass distribution of the system will generally affect model-based controllers, necessitating compensation or the employment of robust control methods. Through introducing the pilot's sensorial feedback of acceleration, the pilot's behavior in giving commands is emulated via an optimization process, which tunes the controller coefficients accordingly. Stability of the designed control system is guaranteed via the Lyapunov approach. To further explore the system through perilous flight scenarios, three pre-designed maneuvers are selected as test cases. It is expected that closed-loop control tasks in which a pilot tracks a target, while at the same time the controller rejects disturbances and adapts itself to the pilot's progressive skills, are ameliorated through this arrangement. Numerical results show that the proposed method is found robust in the training process in conditions of parameters indeterminacy.
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