Model and Simulation of Six-DOF Parallel Platform Based on Direct Drive Volume Control

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Abstract:

The fuel system experimental platform based on Stewart manipulator is used to test the performance and reliability of airplane’s fuel system. Synthesizing efficiency and safety, direct drive method is used as actuator of the experimental platform. Kinematic and dynamic model of the parallel manipulator platform is established. Servo motor and hydraulic cylinder of pump control are modeled for deducing the mathematical model of the experimental platform. Simulation results of the experimental platform show the platform of direct drive method can satisfy the requirements of operation. In addition, data from the simulation can be used as the basis for the design and optimization of the experimental platform for fuel system.

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381-385

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April 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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