[
Ahi, B. and Haeri, M. (2018). Linear active disturbance rejection control from the practical aspects, IEEE/ASME Transactions on Mechatronics 23(6): 2909–2919.]Search in Google Scholar
[
Ahmed, Q., Bhatti, A., Iqbal, S. and Kazmi, I. (2010). 2-Sliding mode based robust control for 2-DOF helicopter, 11th International Workshop on Variable Structure Systems (VSS), Mexico City, Mexico, pp. 481–486.]Search in Google Scholar
[
Bortoff, S.A. (1999). The University of Toronto RC helicopter: A test bed for nonlinear control, Proceedings of the 1999 IEEE International Conference on Control Applications, Kohala Coast, USA, Vol. 1, pp. 333–338.]Search in Google Scholar
[
Budiyono, A. and Wibowo, S. (2007). Optimal tracking controller design for a small scale helicopter, Journal of Bionic Engineering 4(4): 271–280.]Search in Google Scholar
[
Butt, S.S. and Aschemann, H. (2015). Multi-variable integral sliding mode control of a two degrees of freedom helicopter, IFAC-PapersOnLine 48(1): 802–807.]Search in Google Scholar
[
Cerezo-Pacheco, A.D., Pérez-Velasco, C.A., Lozano-Hernandez, Y., Rodriguez-Cortes, H. and Sánchez-Meza, V.G. (2021). Integration of x-plane and Matlab for modeling and simulation of a tiltrotor UAV, 2021 International Conference on Mechatronics, Electronics and Automotive Engineering (ICMEAE), Cuernavaca, Mexico, pp. 39–44.]Search in Google Scholar
[
Fareh, R., Khadraoui, S., Abdallah, M.Y., Baziyad, M. and Bettayeb, M. (2021). Active disturbance rejection control for robotic systems: A review, Mechatronics 80: 102671.]Search in Google Scholar
[
Ferdaus, M.M., Anavatti, S.G., Pratama, M. and Garratt, M.A. (2020). Towards the use of fuzzy logic systems in rotary wing unmanned aerial vehicle: A review, Artificial Intelligence Review 53(1): 257–290.]Search in Google Scholar
[
Fletcher, T.M. and Brown, R.E. (2008). Main rotor-tail rotor interaction and its implications for helicopter directional control, Journal of the American Helicopter Society 53(2): 125–138.]Search in Google Scholar
[
Fliess, M. and Join, C. (2013). Model-free control, International Journal of Control 86(12): 2228–2252.]Search in Google Scholar
[
Fliess, M., Lévine, J., Martin, P. and Rouchon, P. (1995). Flatness and defect of non-linear systems: Introductory theory and examples, International Journal of Control 61(6): 1327–1361.]Search in Google Scholar
[
Fliess, M., Marquez, R., Delaleau, E. and Sira-Ramirez, H. (2002). Correcteurs proportionnels-intégraux genéralisés, ESAIM: Control, Optimisation and Calculus of Variations 7: 23–41.]Search in Google Scholar
[
Garcia, R. and Valavanis, K.P. (2008). The implementation of an autonomous helicopter testbed, in P. Valavanis et al. (Eds), Unmanned Aircraft Systems, Springer, Dordrecht, pp. 423–454.]Search in Google Scholar
[
Han, J. (2009). From PiD to active disturbance rejection control, IEEE Transactions on Industrial Electronics 56(3): 900–906.]Search in Google Scholar
[
He, M., He, J. and Scherer, S. (2021). Model-based real-time robust controller for a small helicopter, Mechanical Systems and Signal Processing 146: 1-16, Article no. 107022.]Search in Google Scholar
[
Kantue, P. and Pedro, J.O. (2022). Integrated fault-tolerant control of a quadcopter UAV with incipient actuator faults, International Journal of Applied Mathematics and Computer Science 32(4): 601–617, DOI: 10.34768/amcs-2022-0042.]Search in Google Scholar
[
Kasac, J., Kotarski, D. and Piljek, P. (2019). Frequency-shifting-based algebraic approach to stable on-line parameter identification and state estimation of multirotor UAV, Asian Journal of Control 21(4): 1619–1629.]Search in Google Scholar
[
Kumar, E.V., Raaja, G.S. and Jerome, J. (2016). Adaptive PSO for optimal LQR tracking control of 2 DOF laboratory helicopter, Applied Soft Computing 41: 77–90.]Search in Google Scholar
[
Kutay, A.T., Calise, A.J., Idan, M. and Hovakimyan, N. (2005). Experimental results on adaptive output feedback control using a laboratory model helicopter, IEEE Transactions on Control Systems Technology 13(2): 196–202.]Search in Google Scholar
[
Leishman, J.G. (2007). The Helicopter, College Park Press, College Park, MD.]Search in Google Scholar
[
Liu, C. (2022). Stabilization control of quadrotor helicopter through matching solution by controlled Lagrangian method, Asian Journal of Control 24(4): 1885–1894.]Search in Google Scholar
[
Lozano-Hernandez, Y. and Gutierrez-Frias, O. (2016). Design and control of a four-rotary-wing aircraft, IEEE Latin America Transactions 14(11): 4433–4438.]Search in Google Scholar
[
Lynn, R.R., Robinson, F., Batra, N. and Duhon, J. (1970). Tail rotor design. Part I: Aerodynamics, Journal of the American Helicopter Society 15(4): 2–15.]Search in Google Scholar
[
Madoński, R. and Herman, P. (2015). Survey on methods of increasing the efficiency of extended state disturbance observers, ISA Transactions 56: 18-27.]Search in Google Scholar
[
Nilsen, S. (2017). Modelling and Control of Two Degrees of Freedom Helicopter Model, MS thesis, Høgskolen i Sørøst-Norge, Notodden.]Search in Google Scholar
[
Nonami, K., Kendoul, F., Suzuki, S., Wang, W. and Nakazawa, D. (2010). Autonomous Flying Robots: Unmanned Aerial Vehicles and Micro Aerial Vehicles, Springer, Tokyo.]Search in Google Scholar
[
Ordaz, P., Alazki, H., Sánchez, B. and Ordaz-Oliver, M. (2023). On the finite time stabilization via robust control for uncertain disturbed systems, International Journal of Applied Mathematics and Computer Science 33(1): 71–82, DOI: 10.34768/amcs-2023-0006.]Search in Google Scholar
[
Pereira das Neves, G. and Augusto Angélico, B. (2022). Model-free control of mechatronic systems based on algebraic estimation, Asian Journal of Control 24(4): 1575–1584.]Search in Google Scholar
[
Pizetta, I.H.B., Brandao, A.S. and Sarcinelli-Filho, M. (2016). A hardware-in-the-loop platform for rotary-wing unmanned aerial vehicles, Journal of Intelligent & Robotic Systems 84(1): 725–743.]Search in Google Scholar
[
Raffo, G.V., Ortega, M.G. and Rubio, F.R. (2015). Robust nonlinear control for path tracking of a quad-rotor helicopter, Asian Journal of Control 17(1): 142–156.]Search in Google Scholar
[
Ramírez-Neria, M., Gao, Z., Sira-Ramirez, H., Garrido-Moctezuma, R. and Luviano-Juarez, A. (2021). On the tracking of fast trajectories of a 3 DOF torsional plant: A flatness based ADRC approach, Asian Journal of Control 23(3): 1367–1379.]Search in Google Scholar
[
Ramírez-Neria, M., Sira-Ramírez, H., Garrido-Moctezuma, R. and Luviano-Juárez, A. (2014). Linear active disturbance rejection control of underactuated systems: The case of the furuta pendulum, ISA Transactions 53(4): 920–928.]Search in Google Scholar
[
Ramírez-Neria, M., Sira-Ramírez, H., Garrido-Moctezuma, R. and Luviano-Juairez, A. (2016). On the linear control of underactuated nonlinear systems via tangent flatness and active disturbance rejection control: The case of the ball and beam system, Journal of Dynamic Systems, Measurement, and Control 138(10): 104501.]Search in Google Scholar
[
Rojas-Cubides, H., Cortés-Romero, J., Coral-Enriquez, H. and Rojas-Cubides, H. (2019). Sliding mode control assisted by GPI observers for tracking tasks of a nonlinear multivariable twin-rotor aerodynamical system, Control Engineering Practice 88: 1–15.]Search in Google Scholar
[
Ross, J., Seto, M. and Johnston, C. (2022). Autonomous landing of rotary wing unmanned aerial vehicles on underway ships in a sea state, Journal of Intelligent & Robotic Systems 104(1): 1–9.]Search in Google Scholar
[
Rysdyk, R.T. and Calise, A.J. (1999). Adaptive model inversion flight control for tilt-rotor aircraft, Journal of Guidance, Control, and Dynamics 22(3): 402–407.]Search in Google Scholar
[
Sánchez-Meza, V. G., Lozano-Hernández, Y. and Gutiérrez-Frías, O.O. (2020). Modeling and control of a two DOF helicopter with tail rotor disturbances, International Conference on Mechatronics, Electronics and Automotive Engineering (ICMEAE), pp. 79–84.]Search in Google Scholar
[
Schäferlein, U., Keßller, M. and Krämer, E. (2018). Aeroelastic simulation of the tail shake phenomenon, Journal of the American Helicopter Society 63(3): 1–17.]Search in Google Scholar
[
Siciliano, B., Sciavicco, L., Villani, L. and Oriolo, G. (2010). Robotics: Modelling, Planning and Control, London.]Search in Google Scholar
[
Sira-Ramírez, H. (2018). From flatness, GPI observers, GPI control and flat filters to observer-based ADRC, Control Theory and Technology 16(4): 249–260.]Search in Google Scholar
[
Sira-Ramírez, H., Luviano-Juárez, A., Ramírez-Neria, M. and Zurita-Bustamante, E.W. (2017). Active Disturbance Rejection Control of Dynamic Systems: A Flatness Based Approach, Butterworth-Heinemann, Kidlington.]Search in Google Scholar
[
Sira-Ramírez, H., Zurita-Bustamante, E.W. and Huang, C. (2019). Equivalence among flat filters, dirty derivative-based PID controllers, ADRC, and integral reconstructor-based sliding mode control, IEEE Transactions on Control Systems Technology 28(5): 1696–1710.]Search in Google Scholar
[
Spong, M., Hutchinson, S. and Vidyasagar, M. (2006). Robot Modeling and Control, Wiley, Hoboken.]Search in Google Scholar
[
Ta, D.A., Fantoni, I. and Lozano, R. (2012). Modeling and control of a tilt tri-rotor airplane, 2012 American Control Conference (ACC), Montreal, Canada, pp. 131–136.]Search in Google Scholar
[
Tang, P., Wang, F. and Dai, Y. (2019). Controller design for different electric tail rotor operating modes in helicopters, International Journal of Pattern Recognition and Artificial Intelligence 33(08): 1959022.]Search in Google Scholar
[
Tanner, O. and Geering, H.P. (2003). Two-degree-of-freedom robust controller for an autonomous helicopter, Proceedings of the American Control Conference, Denver, USA, Vol. 2, pp. 993–998.]Search in Google Scholar
[
Tavoosi, J. (2021). Hybrid intelligent adaptive controller for tiltrotor UAV, International Journal of Intelligent Unmanned Systems 9(4): 256–273.]Search in Google Scholar
[
Velagic, J. and Osmic, N. (2010). Design and implementation of fuzzy logic controllers for helicopter elevation and azimuth controls, Conference on Control and Fault-Tolerant Systems (SysTol), Nice, France, pp. 311–316.]Search in Google Scholar
[
Vitzilaios, N.I. and Tsourveloudis, N.C. (2009). An experimental test bed for small unmanned helicopters, Journal of Intelligent and Robotic Systems 54(5): 769–794.]Search in Google Scholar
[
Wang, B., Shen, Y. and Zhang, Y. (2020). Active fault-tolerant control for a quadrotor helicopter against actuator faults and model uncertainties, Aerospace Science and Technology 99: 105745.]Search in Google Scholar
[
Zeng, Y., Xu, J. and Zhang, R. (2019). Energy minimization for wireless communication with rotary-wing UAV, IEEE Transactions on Wireless Communications 18(4): 2329–2345.]Search in Google Scholar
[
Zhan, C. and Huang, R. (2020). Energy efficient adaptive video streaming with rotary-wing UAV, IEEE Transactions on Vehicular Technology 69(7): 8040–8044.]Search in Google Scholar
[
Zhu, B. and Huo, W. (2013). Robust nonlinear control for a model-scaled helicopter with parameter uncertainties, Nonlinear Dynamics 73(1): 1139–1154.]Search in Google Scholar
