Variable phase control of wing rock

Zeng Lian Liu; Chun-Yi Su; Jaroslav Svoboda

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Variable phase control of wing rock

机译：机翼岩石的变相控制

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This paper addresses a variable phase control issue for suppressing wing rock with hysteresis. In free-to-roll tests, as the angle of attack (AOA) is increased, the roll angle versus the rolling moment indicates hysteresis and provides clues about where wing rock motion is being driven and where the motion is being damped. We present the analysis method of wing rock energy to explain the mechanism of wing rock and the formation of hysteresis, and then develop a variable phase control (VPC) scheme to compensate the phase and magnitude distortions. The effectiveness and robustness of the proposed scheme are demonstrated by suppressing wing rock phenomenon at various AOA and any initial conditions.

机译：本文讨论了用于抑制具有滞后作用的机翼岩石的可变相位控制问题。在自由滑测试中，随着迎角（AOA）的增加，侧倾角与侧倾力矩之间会显示出滞后现象，并提供有关机翼岩石运动被驱动和阻尼运动的线索。我们提出了一种机翼岩石能量分析方法，以解释机翼岩石的机理和滞后现象的形成，然后提出一种可变相位控制（VPC）方案来补偿相位和幅度失真。通过抑制各种AOA和任何初始条件下的机翼岩石现象，证明了该方案的有效性和鲁棒性。

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来源
《Aerospace science and technology》 |2006年第1期|p.27-35|共9页
作者
Zeng Lian Liu; Chun-Yi Su; Jaroslav Svoboda;
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作者单位

Department of Mechanical Engineering, Concordia University, 1455, de Maisonneuve Blvd. W., Montreal, Quebec, Canada, H3G IMS;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空、航天;
关键词
hysteresis; nonlinear system; variable phase control; wing rock;

机译：迟滞;非线性系统;可变相位控制;机翼;

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1. A Variable Control Structure Controller for the Wing Rock Phenomenon [J] . Abdullatif Alshati, Mohammed Alkandari International Journal of Engineering Research and Applications . 2016,第8期

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2. Composite adaptive posicast controller for the wing rock phenomenon in a delta-wing aircraft [J] . Yousefimanesh Amir, Khosravi Alireza, Sarhadi Pouria Proceedings of the Institution of Mechanical Engineers . 2019,第15期

机译：三角翼飞机机翼岩石现象的复合自适应Poscast控制器
3. Design of a Sliding Mode Control for Wing Rock Suppression in Highly-Swept Wing Aircraft [J] . Giorgio Guglieri, Daniele Sartori International Journal of Aerospace Sciences . 2013,第1期

机译：大扫掠机翼飞机压制机翼的滑模控制设计
4. Variable structure adaptive control of wing-rock motion of slender delta wings [C] . de Araujo, Aldayr D. In: AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, Aug. 11-13, 1997, Collection of Technical Papers (A97-37244 10-08), Reston, VA, American Institute of Aeronautics and Astronautics, 1997 . 1997

机译：细长三角翼机翼-岩石运动的变结构自适应控制
5. A microwave phased array with variable and controllable magnitudes and phases. [D] . Aiken, Paul R. 2004

机译：具有可变和可控制的幅度和相位的微波相控阵。
6. ROCK-ALS: Protocol for a Randomized Placebo-Controlled Double-Blind Phase IIa Trial of Safety Tolerability and Efficacy of the Rho Kinase (ROCK) Inhibitor Fasudil in Amyotrophic Lateral Sclerosis [O] . Paul Lingor, Markus Weber, William Camu, 2019

机译：ROCK-ALS：Rho激酶（ROCK）抑制剂Fasudil在肌萎缩性侧索硬化症中的安全性耐受性和有效性的随机安慰剂对照双盲IIa期试验协议
7. A Generalization for Model Reference Adaptive Control and Robust Model Reference Adaptive Control Adaptive Laws for a Class of Nonlinear Uncertain Systems with Application to Control of Wing Rock Phenomenon [O] . 2020

机译：一类非线性不确定系统的模型参考自适应控制和鲁棒模型参考自适应控制自适应控制自适应控制自适应规律，其应用于控制翼岩现象
8. Effect of skewed wing-tip controls on a variable-sweep wing-fuselage configuration [R] . Grow, J. W., Landrum, E. J. 1967

机译：歪斜翼尖控制对可变扫掠机翼 - 机身配置的影响

Variable phase control of wing rock

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