ServoFlight: pneumatically actuated full flight simulator

Authors

  • Justin Pradipta Institute for System Dynamics, University of Stuttgart, Stuttgart, Germany http://orcid.org/0000-0001-6419-3823
  • Oliver Sawodny Institute for System Dynamics, University of Stuttgart, Stuttgart, Germany

DOI:

https://doi.org/10.1080/14399776.2015.1127724

Keywords:

Pneumatic cylinder, parallel robot, motion platform, full flight simulator

Abstract

This contribution covers a new way to provide motion feedback in a full flight simulator. Seven pneumatic cylinders are utilized to actuate our 6 degrees-of-freedom motion platform. The motion platform being investigated is a parallel manipulator configured similarly to a Stewart platform with additional one redundant cylinder in the middle. The models of the pneumatic cylinder and the parallel manipulator are used to derive a dual control method. The dual control follows two different trajectories which are generated by a modified motion cueing algorithm and a force trajectory generator. The measurements are conducted on a full size build. The experiment results show that the platform performs well with a low total transport delay, therefore the platform is suitable to be used in a full flight simulator.

Downloads

Download data is not yet available.

Author Biographies

Justin Pradipta, Institute for System Dynamics, University of Stuttgart, Stuttgart, Germany

Justin Pradipta received the bachelor and master degrees in engineering physics from the Bandung Institute of Technology, Indonesia, in 2007 and 2010 respectively. He joined the Institute for System Dynamics at the University of Stuttgart in 2011 with a DAAD scholarship and is working toward his Ph.D. His research interests include control engineering, mechatronic systems, and trajectory generation.

Oliver Sawodny, Institute for System Dynamics, University of Stuttgart, Stuttgart, Germany

Oliver Sawodny received the diploma degree in electrical engineering from the University of Karlsruhe, Germany, in 1991, and the Ph.D. degree from the University of Ulm, Germany, in 1996. In 2002, he became a full professor at the Technical University of Ilmenau, and in 2005, he became the Director of the Institute for System Dynamics at the University of Stuttgart. His current research interests include methods of differential geometry, trajectory generation, methods and application to mechatronic systems.

References

Airbus, 2015. FLIGHT TRAINING WITH A350 XWB

[online]. Available from: http://www.airbus.com/support/

training/flight/flight-training-with-a350-xwb/ [Accessed

November 2015].

Allerton, D., 2009. Principles of flight simulation. Chichester:

John Wiley & Sons.

Andrievsky, B., Kazunin, D., Kostygova, D., and Kuznetsov,

N., 2014. Control of pneumatically actuated 6-DOF

Stewart. In: 19th International conference on methods and

models in automation and robotics (MMAR), Miedzyzdroje,

–668.

Astolfi, A. and Karagiannis, D., 2008. Nonlinear and adaptive

control with applications. London: Springer Verlag.

Bigras, P., Khayati, K., and Wong, T., 2002. Modified

feedback linearization controller for pneumatic system

with non negligible connection port restriction. In: IEEE

International conference on systems, man and cybernetics,

Yasmine Hammamet, Tunisia, 227–231.

Bone, G. and Ning, S., 2007. Experimental comparison

of position tracking control algorithms for pneumatic

cylinder actuators. IEEE/ASME transaction on

mechatronics, 12, 557–561.

Brun, X., et al., 1999. Control of an electropneumatic

actuator, comparison between some linear and nonlinear

control laws. Journal of systems and control engineering,

, 387–403.

CAE, 2015. CAE 7000XR SERIES LEVEL D FULL-FLIGHT

SIMULATOR [online]. Available from: http://www.cae.

com/civil-aviation/simulation-products/cae-7000XRseries-

full-flight-simulator/ [Accessed 1 November

.

Carniero, J.F. and de Almeida, F.G., 2011. A high-accuracy

trajectory following controller for pneumatic devices.

International Journal of Advance Manufacturing

Technology, 253–267.

Chakarov, D., 2004. Study of the antagonistic stiffness

of parallel manipulators with actuation redundancy.

Mechanism and machine theory, 39, 589–601.

Chen, H.-M., Chen, Z.-Y., & Chung, M.-C., 2009.

Implementation of an integral sliding mode controller for

a pneumatic cylinder position servo control system. In:

Fourth international conference on innovative computing,

information and control, Kaohsiung, 552–555.

Diamond Simulation, 2015. D-SIM-42 [online]. Available

from: http://www.diamond-simulation.de/d-sim-42.

html?&L=3 [Accessed 15 May 2015].

FAA, 2008. 14 CFR part 60, NSP consolidated version [online].

Available from: www.faa.gov/about/initiatives/nsp/media/

consolidated_version.pdf [Accessed 12 May 2015].

FESTO, 2015. Standard cylinders DNCI, with measuring

transducer DADE, Standard cylinder DNC 15552 [online].

Available from: www.festo.com/catalog [Accessed 1 July

.

Fischer, M., 2009. Motion-Cueing-Algortihmen für eine

realitätsnahe Bewegungssimulation [Motion Cueing

Algorithms for a near reality motion simulation]. s.l.:

Deutsches Zentrum für Luft- und Raumfahrt.

Gattringer, H., Naderer, R., and Bremer, H., 2009. Modeling

and control of a pneumatically driven stewart platform.

In: H. Ulbrich and L. Ginzinger, eds. Motion and vibration

control. s.l. Springer, 93–102.

Downloads

Published

2016-03-01

How to Cite

Pradipta, J., & Sawodny, O. (2016). ServoFlight: pneumatically actuated full flight simulator. International Journal of Fluid Power, 17(1), 49–64. https://doi.org/10.1080/14399776.2015.1127724

Issue

Section

Original Article

Most read articles by the same author(s)