飞机数字式电子防滑系统采用新控制律的仿真研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1995, Vol. 16 ›› Issue (1): 124-128.

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THE SIMULATION RESEARCH OF AIRCRAFT DIGITAL-ELECTRO ANTISKID SYSTEM EMPLOYING NEW CONTROL LAW

Zhang Yu¹, Wang Jisen¹, Shi Dianyun²

1. Faculty 908, Northwestern Polytechnical University, Xi'an, 710072; 2. Box 48-46 of Shaanxi Xingping, Xingping, 713106

Received:1993-08-14 Revised:1994-06-15 Online:1995-02-25 Published:1995-02-25

Abstract

Abstract: The methods are discussed for improving the performance of the system from developing the antiskid control law. Based on developing a model of reference velocity generator being adapted to the random disturbance of antiskid system and enhancing releasing voltage function, a fuzzy compound controller is designed. It regulates the antiskid cycle frequency and earns big benefit from reducing wheel's deep skid and raising the braking efficiency.

Key words: antiskid devices, digital simulation, numerical control, fuzzy systems

CLC Number:

Zhang Yu;Wang Jisen;Shi Dianyun. THE SIMULATION RESEARCH OF AIRCRAFT DIGITAL-ELECTRO ANTISKID SYSTEM EMPLOYING NEW CONTROL LAW[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(1): 124-128.

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THE SIMULATION RESEARCH OF AIRCRAFT DIGITAL-ELECTRO ANTISKID SYSTEM EMPLOYING NEW CONTROL LAW

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