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Modeling and Real-Time Stabilization of an Aircraft Having Eight Rotors

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Abstract

We introduce an original configuration of a multi rotor helicopter composed of eight rotors. Four rotors, also called main rotors, are used to stabilize the attitude of the helicopter, while the four extra rotors (lateral rotors) are used to perform the lateral movements of the unmanned aerial vehicle (UAV). The main characteristic of this configuration is that the attitude and translation dynamics are decoupled. The dynamic model is obtained using the well known Euler–Lagrange approach. To validate the model, we performed real-time experiments using a simple nonlinear control law using optical flow and image processing.

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References

  1. Bouguet, J.Y.: Pyramidal implementation of the Lucas Kanade feature tracker. In: Technical report Intel Corporation (1999)

  2. Lyon, D.: A military perspective on small unmanned aerial vehicles. Instrumentation and Measurement Magazine, IEEE, 7(3), 27–31 (2004)

    Article  Google Scholar 

  3. Salazar-Cruz, S., Lozano, R.: Stabilization and nonlinear control for a novel tri-rotor mini-aircraft. In: Proc. of IEEE International Conference on Robotics and Automation, pp. 2924–2929 (2005)

  4. Green, W.E., Oh, P.Y., Barrows, G.L.: Flying insect inspired vision for autonomous aerial robot maneuvers in near-earth environments. In: Proc. of IEEE International Conference on Robotics and Automation (2004)

  5. Romero, H., Benosman, R., Lozano, R.: Stabilization and location of a four rotors helicopter applying vision. In Proc. American Control Conference ACC. pp. 3931–3936 (2006)

  6. Castillo, P., Lozano, R., Dzul, A.: Stabilization of a mini rotorcraft with four rotors. Control Systems Magazine, IEEE 25, 45–55 (2005)

    Article  MathSciNet  Google Scholar 

  7. Tayebi, A., McGilvray, S.: Attitude stabilization of a four-rotor aerial robot. In: Proc. of Conference on Decision and Control, IEEE CDC., vol. 2, pp. 1216–1221 (2004)

  8. Hartley, R., Zisserman, A.: Multiple View Geometry in Computer Vision, 2nd Edn. In: Cambridge University Press, ISBN 0521540518 (2004)

  9. McCormick Jr., B.W.: Aerodynamics of V/STOL Flight. Dover Publication Inc. (1999)

  10. Beauchemin, S.S., Barron, J.L.: The computation of optical flow. In: ACM Computing Surveys, 27, 433–467 (1995)

    Article  Google Scholar 

  11. King, C.Y.: Virtual instrumentation-based system in a real-time applications of GPS/GIS. In: Proc. Conference on Recent Advances in Space Technologies, pp. 403–408 (2003)

  12. Sasiadek, J.Z., Hartana, P.: Sensor Fusion for Navigation of an Autonomous Unmanned Aerial Vehicle. In: Proc. International Conference on Robotics and Automation, vol. 4, pp. 429–434 (2004)

  13. Yoo, C.-S., Ahn, I.-K.: Low cost GPS/INS sensor fusion system for UAV navigation. In: Proc. Digital Avionics Systems Conference, vol. 2, pp. 8.A.1-1–8.A.1-9 (2003)

  14. Goldstein, H.: Classical Mechanics, 2nd Edn. Addison Wesley Series in Physics, Adison-Wesley, U.S.A. (1980)

  15. Castillo, P., Lozano, R., Dzul, A.: Modelling and Control of Mini-Flying Machines. Springer-Verlag in Advances in Industrial Control. ISBN: 1-85233-957-8 (2005) July

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Correspondence to S. Salazar.

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Partially supported by SNI-CONACyT México.

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Salazar, S., Romero, H., Lozano, R. et al. Modeling and Real-Time Stabilization of an Aircraft Having Eight Rotors. J Intell Robot Syst 54, 455–470 (2009). https://doi.org/10.1007/s10846-008-9274-x

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  • DOI: https://doi.org/10.1007/s10846-008-9274-x

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