Hardware in the Loop of Two Rotors Platform
DOI:
https://doi.org/10.11113/jt.v71.3711Keywords:
Two rotors, rotor, platform, open loop, closed loopAbstract
This study is aimed to control unstable platform by introducing control system design through low-cost test rig for two rotor system with a feedback control. The rig is used to control the bank angle by adjusting the thrust from each rotor and useful as a teaching aid in control system design. In this paper, the transfer functions of the dynamic system for the two rotor platform was derived and introduce into the controller system. Inertia Measurement Unit (IMU) was installed to provide feedback to the control system. MATLAB Simulink is used to simulate the response of the system before going to the real application while LabVIEW is used to interface the hardware interface and programmed the control system.
References
G. Gremillion. and J. S. Humbert. 2010. System identification of a quadrotor micro air vehicle. AIAA Flight Mechanics Conferences. AIAA 7644:1–7.
G. M. Hoffman, H. Haomiao, W. e L and T. Claire J. 2007. Quadrotor helicopter flight dynamic and control : Theory and experiment. AIAA Guidance, Navigation and Control Conferences and Exhibit. AIAA 6461:1–20.
H. Jamaluddin, M. S. Yaacob, R. Ahmad. 2011. Introduction to control engineering. Penerbit UTM. Johor Bahru.
M. Karpenko, P. Sekhavat, J. Park, I. M. Ross. 2010. Closed-loop optimal guidance and control of quadrotor unmanned aerial vehicle. AIAA Guidance, Navigation and Control Conference. AIAA. 8051 : 1–11.
S. Hanford, L. Long, J. Horn. 2005. A small semi-autonomous rotary-wing unmanned air vehicle (UAV). Infotech@Aerospace. 7077:1–10.
S. Bouabdallah, R. Siegwart. 2004. Design and control of an indoor micro quadrotor. IEEE: International Conferences on Robotics and Automation. 5:4393–4398.
H. C. Yang, R. Addousleiman, B. Sababha, E. Gjoni, D. Korff, O. Rawashdeh. 2009. Implementation of an autonomous surveillance quadrotor system. AIAA Infotech@Aerospace Conference. AIAA 2047:1–7.
R. Colgren, R. Loschke. 1997. To tail or two tails? The effective design and modeling of yaw control devices. AIAA Modelling and Simulation Technologies Conference and Exhibit. AIAA 4609: 1–13.
R. C. Nelson. 1998. Flight Stability and Automatic Control. Second Edi. University of Notre Dame: McGraw-Hill International Editions.
G. F. Cook. 1999. “PWM motor speed controller/DC light dimmer,†Home Power Magazine.
Cytron Technologies. 2012. “IMU 5 degree of freedom,â€. [Online]. Available: http://www.cytron.com.my/.
H. C. Yang, B. Sababha, C. Acar, O. Rawashded. 2010. Rapid prototyping of quadrotor controllers using Matlab RTW and dsPICS. AIAA Infotech@Aerospace.AIAA 3407:1–6
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