DocumentCode :
3057825
Title :
Accurate mathematical model for describing electrohydraulic loading system of helicopter pitch adjusting hydromechanical servos
Author :
Liu, Guojian ; Li, Yunhua ; Yang, Liman
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear :
2010
fDate :
28-30 June 2010
Firstpage :
309
Lastpage :
314
Abstract :
This paper deals with the establishment of the exact mathematical model for describing the electro-hydraulic load system which is applied to the earth-experiment of the hydromechanical servomechanism (hydraulic assistor) for the helicopter pitch adjusting. Based on the working principle analysis of the electro-hydraulic load system, the accurate mathematical model of electric-hydraulic loading system is established and the influence of the model on the system characteristics is deeply analyzed. It is proved that surplus force is concerned with not only the velocity but also the acceleration of rudderpost. Moreover, the traditional structure invariance principle is improved. Experiments in the paper validate the correctness of complex mathematical model, of which the guiding effect in eliminating the extraneous force is revealed also.
Keywords :
electrohydraulic control equipment; helicopters; loading equipment; mathematical analysis; servomechanisms; accurate mathematical model; earth experiment; electro hydraulic loading system; helicopter pitch adjusting hydromechanical servos; hydraulic assistor; rudderpost acceleration; Acceleration; Control systems; Electrohydraulics; Force control; Force sensors; Gears; Helicopters; Mathematical model; Servomechanisms; Torque; electro-hydraulic load system; force control; hydraulic assistor; mathematical model; surplus force;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Robotics Automation and Mechatronics (RAM), 2010 IEEE Conference on
Conference_Location :
Singapore
Print_ISBN :
978-1-4244-6503-3
Type :
conf
DOI :
10.1109/RAMECH.2010.5513173
Filename :
5513173
Link To Document :
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