DocumentCode
2948249
Title
Development of a pneumatically driven flight simulator Stewart platform using motion and force control
Author
Pradipta, Justin ; Klunder, Mario ; Weickgenannt, M. ; Sawodny, Oliver
Author_Institution
Inst. for Syst. Dynamics, Univ. of Stuttgart, Stuttgart, Germany
fYear
2013
fDate
9-12 July 2013
Firstpage
158
Lastpage
163
Abstract
In this paper we develop a motion platform driven by pneumatic actuators for a flight simulator. The platform itself is a Stewart platform with an extra cylinder in the middle. To control the platform two control methods are proposed, with the benefit of eliminating the kinematic constraints caused by the seven-cylinders configuration. The six outer cylinders are controlled according to motion trajectories whereas the middle cylinder acts as a pure force actuator to lift the weight of the platform. The Immersion and Invariance method with an additional friction compensator is applied for motion control. The method of exact input/output linearization is used for controlling the lift force of the middle cylinder. The measurement results show that the proposed method is effective for controlling the platform.
Keywords
aerospace simulation; force control; friction; motion control; pneumatic actuators; trajectory control; Stewart platform; force actuator; force control; friction compensator; kinematic constraints; motion control; motion trajectories; pneumatic actuators; pneumatically driven flight simulator; seven-cylinders configuration; Design automation; Gravity; Weight measurement;
fLanguage
English
Publisher
ieee
Conference_Titel
Advanced Intelligent Mechatronics (AIM), 2013 IEEE/ASME International Conference on
Conference_Location
Wollongong, NSW
ISSN
2159-6247
Print_ISBN
978-1-4673-5319-9
Type
conf
DOI
10.1109/AIM.2013.6584085
Filename
6584085
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