航空学报 > 1994, Vol. 15 Issue (6): 647-651

数字式颤振主动抑制系统的研究

邹丛青, 陈桂彬   

  1. 北京航空航天大学五系,北京,100083
  • 收稿日期:1992-11-04 修回日期:1993-07-08 出版日期:1994-06-25 发布日期:1994-06-25

RESEARCH ON DIGITAL ACTIVE FLUTTER SUPPRESSION

Zou Congqing, Chen Guibin   

  1. 5th Department,Beijing University of Aeronautics and Astronautics,Beijing,100083
  • Received:1992-11-04 Revised:1993-07-08 Online:1994-06-25 Published:1994-06-25

摘要: 介绍了数字式颤振主动抑制系统的控制律综合、风洞实验及其工程特性。控制律的设计采用连续域离散化的方法。对4种不同控制律进行了风洞实验,验证了理论计算与实验设计的正确性。实验中控制律用微机和工业控制机联合实现;还根据工程应用的观点提出了颤振主动抑制系统应该具有的特性。对一个与实际飞机动力相似的机翼/外挂系统的研究表明,颤振速度提高了20%左右,并且系统的工程特性也是基本可行的。

关键词: 颤振-阻滞, 控制理论, 风洞试验

Abstract: his paper presents the control law design, experience and its relative properties in digital active flutter suppression system. A method of discretization of continuous domain is adopted in this control law design,and we have obtained their digital control law with this method to four sorts of control law. The wind tunnel test affirms the correctness of the theoreti-cal calculation and the test design. The control law is implemented by use of microcomputer and industrial controller in this test.The properties of the active flutter suppression system are raised according to engineering application. The research to a dynamically scaled Wing/Store configura-tion shows that the flutter speed has increased by 20% or so and the performance of this system is basically satisfactory.

Key words: flutter-retarding, control theory, wind tunnel tests

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