Designing Back-stepping Sliding Mode Controller for a Class of 4Y Octorotor

This paper presents a combination of both robust
nonlinear controller and nonlinear controller for a class of nonlinear
4Y Octorotor UAV using Back-stepping and sliding mode controller.
The robustness against internal and external disturbance and
decoupling control are the merits of the proposed paper. The
proposed controller decouples the Octorotor dynamical system. The
controller is then applied to a 4Y Octortor UAV and its feature will
be shown.





References:
[1] S. Bouabdallah, “Design and Control of Quadrotors with Applications to
Autonomous Flying”, PhD Thesis, Ecole Polytechnique Federale de
Lausanne, 2007.
[2] Patrick Adigbil, “Nonlinear Attitude and Position Control of a Micro
Quadrotor using Sliding Mode and Backstepping Techniques”, rd USEuropean
Competition and Workshop on Micro Air Vehicle Systems
(MAV07) & European Micro Air Vehicle Conference and Flight
Competition (EMAV2007), September 2007, pp.17-21.
[3] Fernando, H.C.T.E., De Silva, A.T.A, “Modelling, imulation and
implementation of a quadrotor UAV”, ISBN 978-1-4799-0908-7, 2013.
[4] Kis, L., Regula, G., ‘Design and hardware-in-the-loop test of the
embedded control system of an indoor quadrotor helicopter’, ISBN 978-
3-00-024989-1, 2008
[5] Madani, T., Benallegue, A., ‘Backstepping Control for a Quadrotor
Helicopter’, in Intelligence Robots and system Conference, 2006.
[6] A. Freddi, A. Lanzon and S. Longhi, “A Feedback Linearization
Approach to Fault Tolerance in Quadrotor Vehicles”, in Preprints of the
18th IFAC World Congress, Milano (Italy), 2011, pp. 5413-5418.
[7] V. G. Adîr, A. M. Stoica, A. Marks and J. F. Whidborne, “Modelling,
stabilization and single motor failure recovery of a 4Y octorotor”, in
Proceedings of the IASTED International Conference of Intelligent
Systems and Control (ISC 2011), Cambridge, United Kingdom, July
2011, pp. 82 – 87.
[8] Mehmet Onder Efe, ‘Robust Low Altitude Behavior Control of a
Quadrotor Rotorcraft Through Sliding Modes’, in Proceedings of the
15th Mediteranean Conference on Control & Automation, 2007.
[9] H. Khebbache, M. Tadjine, “Robust Fuzzy Backstepping Sliding Mode
Controller For a Quadrotor Unmanned Aerial Vehicle” CEAI, Vol.15,
No.2 pp. 3-11, 2013
[10] S. Bouabdallah, P. Murrieri and R. Siegwart, “Design and control of an
indoor micro quadrotor”, in Proceedings of the 2004 IEEE International
Conference on Robotics and Automation (ICRA ’04), vol. 5, New
Orleans, LA, April 2004, pp. 4393 – 4398.
[11] S. Bouabdallah, A. Noth and R. Siegwart, “PID vs LQ control
techniques applied to an indoor micro quadrotor”, in Proceedings of
2004 IEEE/RSJ International Conference on Intelligent Robots and
Systems (IROS 2004), vol. 3, Sendai, Japan, October 2004, pp. 2451 –
2456 .
[12] S. Bouabdallah and R. Siegwart, “Backstepping and sliding-mode
techniques applied to an indoor micro quadrotor”, in Proceedings of the
2005 IEEE International Conference on Robotics and Automation
(ICRA ’05), Barcelona, Spain, April 2005, pp. 2247 – 2252
[13] T. Bresciani,”Modeling, Identification and Control of a Quadrotor
Helicopter”, MSc Thesis, Lund University, 2008.
[14] Y. Zhang and A. Chamseddine, “Fault Tolerant Flight Control
Techniques with Application to a Quadrotor UAV Testbed”, Automatic
Flight Control Systems – Latest Developments, InTech, January 2012.
[15] Chelaru T.V., Dinamica Zborului – Note de curs (Flight Dynamics –
Lecture Notes), Editura POLITEHNICA PRESS, Bucuresti, 2009 (in
Romanian)
[16] Guilherme V. Raffo, Manuel G. Ortega and Francisco R. Rubio,
“Backstepping/Nonlinear H∞ Control for Path Tracking of a QuadRotor Unmanned Aerial Vehicle”, American Control Conference, Westin
Seattle Hotel, USA, June 2008
[17] Slotine, J. J. E., and Li, W., Applied Nonlinear Control, Prentice-Hall,
Upper Saddle River, NJ, 1991, pp. 276-309.