Development of Motion Manipulator System for a Generic Aircraft Flight Dynamic Simulator

  • Authors

    • Yusuf Kurniawan Asalani
    • Rianto Adhy Sasongko
    • Ony Arifianto
    2018-11-30
    https://doi.org/10.14419/ijet.v7i4.25.22246
  • Acceleration Cue, Aircraft Simulator, Inverse Dynamic, Hexapod Manipulator, Newton-Euler Approach, SimScape Feature.

  • Abstract

    The purpose of this development program is to apply some prior studies about hexapod manipulator for designing aircraft simulator motion platform in terms of acceleration cue. Acceleration would represent human perception to describe a motion. By giving acceleration cues in a simulator, the operator would obtain similar sensation corresponding to real phenomenon/condition. Iteration process is used to collect relations between hexapod manipulator parameters, platform size and actuator position, and manipulator performances describing as manipulator displacement and acceleration range. Its kinematics and dynamics are modelled by using Newton-Euler approach and validated by using SimScape feature provided in MATLAB/Simulink. Hereafter, actuation control scheme would be implemented in order to convey manipulator from a conceptual world into real world based on its dynamics. As part of this development, constructing hexapod manipulator numerical model becomes the main objective of this current research.

     

     

  • References

    1. [1] David Allerton, Principles of Flight Simulation, Wiley, (2009), pp: 1-24.

      [2] Zafer Bingul and Oguzhan Karahan, Dynamic Modelling and Simulation of Stewart Platform, Serial and Parallel Robot Manipulators – Kinematics, Dynamics, Control and Optimization, Intech, (2012), pp: 19-42.

      [3] Bhaskar Dasgupta and T. S. Mruthyunjaya, “A Newton-Euler Formulation for the Inverse Dynamics of the Stewart Platform Manipulatorâ€, Mech. Mach. Theory, Vol.33, No.8, (1998), pp.1135-1152, available online, https://doi.org/10.1016/S0094-114X(97)00118-3, last visit: 18.02.2018.

      [4] Mauricio Becerra-Vargas and Eduardo Morgado Belo, “Application of H Theory to A 6 DOF Flight Simulator Motion Baseâ€, J. Braz. Soc. Mech. Sci. & Eng., Vol.34, No.2, (2012), pp.193-204, available online, http://dx.doi.org/10.1590/S1678-58782012000200011, last visit: 10.03.2018.

      [5] Fumio Hamamo, “Derivative of Rotation Matrix – Direct Matrix Derivation of Well-Known Formulaâ€, Proceedings of Green Energy and Systems Conference, (2013).

      [6] MATLAB User Manual, Mathworks Inc.

      [7] Simulink User Manual, Mathworks Inc.

      [8] Arduino User Guide, Arduino.

      [9] Python User Manual, Python.

      [10] The Mathematics of the Stewart Platform. http://www.instructables.com/id/Stewart-Platform/

      [11] Actuonix L16 Micro Linear Actuator Specification. https://www.actuonix.com/L16-R-Miniature-Linear-Servo-For-RC-p/l16-r.htm?1=1&CartID=0.

      [12] PI Motion | Positioning Corporation. http://www.pi-usa.us.

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  • How to Cite

    Kurniawan Asalani, Y., Adhy Sasongko, R., & Arifianto, O. (2018). Development of Motion Manipulator System for a Generic Aircraft Flight Dynamic Simulator. International Journal of Engineering & Technology, 7(4.25), 43-52. https://doi.org/10.14419/ijet.v7i4.25.22246