DR. ANAND SÁNCHEZ ORTA
Profesor InvestigadorPUBLICACIONES
Para ver las publicaciones de todo Robótica y Manufactura Avanzada, ver: Publicaciones RYMA
Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sanchez-Orta, Anand Fractional integral sliding modes for robust tracking of nonlinear systems Artículo de revista En: Nonlinear Dynamics, vol. 87, no 2, pp. 895–901, 2017. Muñoz-Vazquez, Aldo Jonathan; Ramirez-Rodriguez, Heriberto; Parra-Vega, Vicente; Sanchez-Orta, Anand Fractional sliding mode control of underwater ROVs subject to non-differentiable disturbances Artículo de revista En: International Journal of Control, Automation and Systems, pp. 1–8, 2017. Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sanchez-Orta, Anand Continuous Fractional-Order Sliding PI Control for Nonlinear Systems Subject to Non-Differentiable Disturbances Artículo de revista En: Asian Journal of Control, vol. 19, no 1, pp. 279–288, 2017, ISSN: 1934-6093, (asjc.1370). Oliva-Palomo, F.; Sanchez-Orta, Anand; Alazki, Hussain Position Estimation Improvement Using and Observer Based on Attractive Ellipsoid Method for a Quadrotor Artículo de revista En: 2016. Izaguirre-Espinosa, Carlos; Muñoz-Vazquez, Aldo Jonathan; Sanchez-Orta, Anand; Parra-Vega, Vicente; Castillo, Pedro Attitude control of quadrotors based on fractional sliding modes: theory and experiments Artículo de revista En: IET Control Theory & Applications, vol. 10, no 7, pp. 825–832, 2016. Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sanchez-Orta, Anand Uniformly continuous differintegral sliding mode control of nonlinear systems subject to Hölder disturbances Artículo de revista En: Automatica, vol. 66, pp. 179–184, 2016. Izaguirre-Espinosa, Carlos; Muñoz-Vazquez, Aldo Jonathan; Sanchez-Orta, Anand; Parra-Vega, Vicente; Sanahuja, G Fractional attitude-reactive control for robust quadrotor position stabilization without resolving underactuation Artículo de revista En: Control Engineering Practice, vol. 53, pp. 47 - 56, 2016, ISSN: 0967-0661. Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sanchez-Orta, Anand Control of Constrained Robot Manipulators based on Fractional Order Error Manifolds Artículo de revista En: IFAC-PapersOnLine, vol. 48, no 19, pp. 118 - 123, 2015, ISSN: 2405-8963, (11th IFAC Symposium on Robot Control SYROCO 2015). Sanchez-Fraire, U.; Parra-Vega, Vicente; Martinez-Peon, D.; Sepulveda-Cervantes, G.; Sanchez-Orta, Anand; Muñoz-Vazquez, Aldo Jonathan On the Brain Computer Robot Interface (BCRI) to Control Robots Artículo de revista En: IFAC-PapersOnLine, vol. 48, no 19, pp. 154 - 159, 2015, ISSN: 2405-8963, (11th IFAC Symposium on Robot Control SYROCO 2015). Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sánchez-Orta, Anand Continuous fractional sliding mode-like control for exact rejection of non-differentiable Hölder disturbances Artículo de revista En: IMA Journal of Mathematic al Control and Information, vol. 34, 2015, ISSN: 0265-0754. Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sanchez-Orta, Anand; Castillo, Pedro; Lozano, R. Generalized order integral sliding mode control for non-differentiable disturbance rejection: A comparative study Proceedings Article En: 2015 54th IEEE Conference on Decision and Control (CDC), pp. 4092-4097, 2015. Martinez, V.; Garcia, Octavio; Sanchez-Orta, Anand; Parra-Vega, Vicente; Escobar, A. Adaptive backstepping control for a convertible UAV Proceedings Article En: 2015 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS), pp. 298-307, 2015. Guerrero, F.; Martinez, V.; Garcia, Octavio; Sanchez-Orta, Anand; Espinoza, E. S. Aerodynamic analysis and performance of a mini airplane UAV Proceedings Article En: 2015 International Conference on Unmanned Aircraft Systems (ICUAS), pp. 1112-1117, 2015. Martinez-Peon, D.; Parra-Vega, Vicente; Sanchez-Orta, Anand EEG-motor sequencing signals for online command of dynamic robots Proceedings Article En: The 3rd International Winter Conference on Brain-Computer Interface, pp. 1-4, 2015. Sanchez-Orta, Anand; Parra-Vega, Vicente; Izaguirre-Espinosa, Carlos; Garcia, Octavio Position–Yaw Tracking of Quadrotors Artículo de revista En: Journal of Dynamic Systems, Measurement, vol. 137, 2014, ISSN: 002-0434. Ramirez-Rodriguez, Heriberto; Parra-Vega, Vicente; Sanchez-Orta, Anand; Garcia-Salazar, Octavio Robust Backstepping Control Based on Integral Sliding Modes for Tracking of Quadrotors Artículo de revista En: Journal of Intelligent & Robotic Systems, vol. 73, no 1, pp. 51–66, 2014, ISSN: 1573-0409. Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sanchez-Orta, Anand A Passive Velocity Field Control for Navigation of Quadrotors with Model-free Integral Sliding Modes Artículo de revista En: Journal of Intelligent & Robotic Systems, vol. 73, no 1, pp. 373–385, 2014, ISSN: 1573-0409. Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sanchez-Orta, Anand Attitude tracking control of a quadrotor based on absolutely continuous fractional integral sliding modes Conferencia Attitude tracking control of a quadrotor based on absolutely continuous fractional integral sliding modes, iee multi-conference on system and control 2014, ISSN: 1085-1992. Muñoz-Vazquez, Aldo Jonathan; Parra-Vega, Vicente; Sanchez-Orta, Anand free-model fractional-order absolutely continuous sliding mode, control for euler-lagrange systems Conferencia free-model fractional-order absolutely continuous sliding mode, control for euler-lagrange systems, ieee conference on decision and control 2014, ISSN: 0191-2216. Martinez-Alvarado, Ricardo; Ruiz-Sanchez, Francisco J.; Sanchez-Orta, Anand; Garcia-Salazar, Octavio Dynamic Response of BLDC-Thruster for Small Scale Quadrotors under Aerodynamic Load Torque Proceedings Article En: Dynamic Response of BLDC-Thruster for Small Scale Quadrotors under Aerodynamic Load Torque, pp. 1-6, iee international autumn meeting on power, electronics and computing 2014, ISBN: 978-1-4799-5683-8. Martínez-Alvarado, Ricardo; Sánchez-Orta, Anand; Granda-Gutiérrez, E.; Ruiz-Sanchez, Francisco J. performance evaluation of propeller-engine systems for unmanned aerial vehicles in hovering Proceedings Article En: performance evaluation of propeller-engine systems for unmanned aerial vehicles in hovering, pp. 131-136, congreso internacional en ingenieria electronica electro 2014, 2014, ISSN: 1405-2172.2017
Artículos de revista
@article{munoz2017fractional,
title = {Fractional integral sliding modes for robust tracking of nonlinear systems},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and Sanchez-Orta, Anand},
year = {2017},
date = {2017-01-01},
journal = {Nonlinear Dynamics},
volume = {87},
number = {2},
pages = {895--901},
publisher = {Springer},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{munoz2017fractionalb,
title = {Fractional sliding mode control of underwater ROVs subject to non-differentiable disturbances},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Ramirez-Rodriguez, Heriberto and Parra-Vega, Vicente and Sanchez-Orta, Anand},
year = {2017},
date = {2017-01-01},
journal = {International Journal of Control, Automation and Systems},
pages = {1--8},
publisher = {Springer},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{ASJC:ASJC1370,
title = {Continuous Fractional-Order Sliding PI Control for Nonlinear Systems Subject to Non-Differentiable Disturbances},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and Sanchez-Orta, Anand},
url = {http://dx.doi.org/10.1002/asjc.1370},
doi = {10.1002/asjc.1370},
issn = {1934-6093},
year = {2017},
date = {2017-01-01},
journal = {Asian Journal of Control},
volume = {19},
number = {1},
pages = {279--288},
note = {asjc.1370},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
2016
Artículos de revista
@article{Oliva-Palomo2016,
title = {Position Estimation Improvement Using and Observer Based on Attractive Ellipsoid Method for a Quadrotor},
author = {Oliva-Palomo, F. and Sanchez-Orta, Anand and Alazki, Hussain},
year = {2016},
date = {2016-07-15},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{Izaguirre-Espinosa2016,
title = {Attitude control of quadrotors based on fractional sliding modes: theory and experiments},
author = {Izaguirre-Espinosa, Carlos and Mu\~{n}oz-Vazquez, Aldo Jonathan and Sanchez-Orta, Anand and Parra-Vega, Vicente and Castillo, Pedro},
year = {2016},
date = {2016-01-01},
journal = {IET Control Theory \& Applications},
volume = {10},
number = {7},
pages = {825--832},
publisher = {IET},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{Aldo-Jonathan2016,
title = {Uniformly continuous differintegral sliding mode control of nonlinear systems subject to H\"{o}lder disturbances},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and Sanchez-Orta, Anand},
year = {2016},
date = {2016-01-01},
journal = {Automatica},
volume = {66},
pages = {179--184},
publisher = {Elsevier},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{Izaguirre-Espinosa2016,
title = {Fractional attitude-reactive control for robust quadrotor position stabilization without resolving underactuation},
author = {Izaguirre-Espinosa, Carlos and Mu\~{n}oz-Vazquez, Aldo Jonathan and Sanchez-Orta, Anand and Parra-Vega, Vicente and G Sanahuja },
url = {http://www.sciencedirect.com/science/article/pii/S0967066116300867},
doi = {http://dx.doi.org/10.1016/j.conengprac.2016.04.016},
issn = {0967-0661},
year = {2016},
date = {2016-01-01},
journal = {Control Engineering Practice},
volume = {53},
pages = {47 - 56},
abstract = {Quadrotors are Unmanned Aerial Systems (UAS), whose nonlinearities, uncertainties, and unavoidable aerodynamic disturbances stand for a difficult control problem. Additionally, the highly nonlinear coupling between the position and the orientation dynamics exacerbates the underactuation problem when the objective is the position tracking. In this paper, aiming at designing a robust position controller without resolving underactuation, a novel “reactive orientation control” is proposed. The orientation controller is model-free and it is build upon differintegral fractional operators to react to a continuous and bounded additive term that stands for an affine exogenous position controller. Such term indeed becomes an attitude disturbance that is purposely injected to displace the quadrotor towards the desired position of the underactuated coordinates. The closed-loop analysis shows that the norm of the transfer function between the disturbance and the position tracking error is minimized for a stable and robust position regime. Simulations and experimental results are given to discuss the feasibility of the proposed scheme.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
2015
Artículos de revista
@article{MUNOZVAZQUEZ2015118,
title = {Control of Constrained Robot Manipulators based on Fractional Order Error Manifolds},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and Sanchez-Orta, Anand},
url = {http://www.sciencedirect.com/science/article/pii/S2405896315026440},
doi = {http://dx.doi.org/10.1016/j.ifacol.2015.12.020},
issn = {2405-8963},
year = {2015},
date = {2015-01-01},
journal = {IFAC-PapersOnLine},
volume = {48},
number = {19},
pages = {118 - 123},
note = {11th IFAC Symposium on Robot Control SYROCO 2015},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{SANCHEZFRAIRE2015154b,
title = {On the Brain Computer Robot Interface (BCRI) to Control Robots},
author = {Sanchez-Fraire, U. and Parra-Vega, Vicente and Martinez-Peon, D. and Sepulveda-Cervantes, G. and Sanchez-Orta, Anand and Mu\~{n}oz-Vazquez, Aldo Jonathan},
url = {http://www.sciencedirect.com/science/article/pii/S2405896315026506},
doi = {http://dx.doi.org/10.1016/j.ifacol.2015.12.026},
issn = {2405-8963},
year = {2015},
date = {2015-01-01},
journal = {IFAC-PapersOnLine},
volume = {48},
number = {19},
pages = {154 - 159},
note = {11th IFAC Symposium on Robot Control SYROCO 2015},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{Mu\~{n}oz-V\'{a}zquez2015,
title = {Continuous fractional sliding mode-like control for exact rejection of non-differentiable H\"{o}lder disturbances},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and S\'{a}nchez-Orta, Anand},
url = {https://academic.oup.com/imamci/article/34/2/597/2885232/Continuous-fractional-sliding-mode-like-control},
doi = {https://doi.org/10.1093/imamci/dnv064},
issn = {0265-0754},
year = {2015},
date = {2015-00-00},
journal = {IMA Journal of Mathematic al Control and Information},
volume = {34},
abstract = {Exploiting algebraic and topological properties of differintegral operators as well as a proposed principle of dynamic memory resetting, a uniform continuous sliding mode controller for a general class of integer order affine non-linear systems is proposed. The controller rejects a wide class of disturbances, enforcing in finite-time a sliding regime without chattering. Such disturbance is of H\"{o}lder type that is not necessarily differentiable in the usual (integer order) sense. The control signal is uniformly continuous in contrast to the classical (integer order) discontinuous scheme that has been proposed for both fractional and integer order systems. The proposed principle of dynamic memory resetting allows demonstrating robustness as well as: (i) finite-time convergence of the sliding manifold, (ii) asymptotic convergence of tracking errors, and (iii) exact disturbance observation. The validity of the proposed scheme is discussed in a representative numerical study.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
Proceedings Articles
@inproceedings{7402856,
title = {Generalized order integral sliding mode control for non-differentiable disturbance rejection: A comparative study},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and Sanchez-Orta, Anand and Castillo, Pedro and Lozano, R.},
url = {http://ieeexplore.ieee.org/document/7402856/},
doi = {10.1109/CDC.2015.7402856},
year = {2015},
date = {2015-12-01},
booktitle = {2015 54th IEEE Conference on Decision and Control (CDC)},
pages = {4092-4097},
keywords = {},
pubstate = {published},
tppubtype = {inproceedings}
}
@inproceedings{7441020,
title = {Adaptive backstepping control for a convertible UAV},
author = {Martinez, V. and Garcia, Octavio and Sanchez-Orta, Anand and Parra-Vega, Vicente and Escobar, A.},
url = {http://ieeexplore.ieee.org/document/7441020/},
doi = {10.1109/RED-UAS.2015.7441020},
year = {2015},
date = {2015-11-01},
booktitle = {2015 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)},
pages = {298-307},
keywords = {},
pubstate = {published},
tppubtype = {inproceedings}
}
@inproceedings{7152403,
title = {Aerodynamic analysis and performance of a mini airplane UAV},
author = {Guerrero, F. and Martinez, V. and Garcia, Octavio and Sanchez-Orta, Anand and Espinoza, E. S.},
url = {http://ieeexplore.ieee.org/document/7152403/},
doi = {10.1109/ICUAS.2015.7152403},
year = {2015},
date = {2015-06-01},
booktitle = {2015 International Conference on Unmanned Aircraft Systems (ICUAS)},
pages = {1112-1117},
keywords = {},
pubstate = {published},
tppubtype = {inproceedings}
}
@inproceedings{7073043,
title = {EEG-motor sequencing signals for online command of dynamic robots},
author = {Martinez-Peon, D. and Parra-Vega, Vicente and Sanchez-Orta, Anand},
url = {http://ieeexplore.ieee.org/document/7073043/},
doi = {10.1109/IWW-BCI.2015.7073043},
year = {2015},
date = {2015-01-01},
booktitle = {The 3rd International Winter Conference on Brain-Computer Interface},
pages = {1-4},
keywords = {},
pubstate = {published},
tppubtype = {inproceedings}
}
2014
Artículos de revista
@article{Sanchez-Orta2014,
title = {Position\textendashYaw Tracking of Quadrotors},
author = {Sanchez-Orta, Anand and Parra-Vega, Vicente and Izaguirre-Espinosa, Carlos and Garcia, Octavio},
url = {http://dynamicsystems.asmedigitalcollection.asme.org/article.aspx?articleid=2088643#Abstract},
doi = {10.1115/1.4029464},
issn = {002-0434},
year = {2014},
date = {2014-12-19},
issuetitle = {Position-Yaw Tracking of Quadrotors},
journal = {Journal of Dynamic Systems, Measurement},
volume = {137},
abstract = {A yaw angle, different from zero, introduces highly nonlinear couplings in the rotational and translational quadrotor dynamics, implying undesirable motions. This argument has motivated that the position control problem of quadrotors is studied generally regulating yaw at zero. However, zeroing yaw limits the maneuverability of underactuated quadrotors because yaw is one of the four actuated motions. In this paper, the simultaneous tracking of position and time-varying heading is proposed, based on an integral sliding mode control with a quaternion-based sliding surface. An exponential tracking with chattering-free is obtained without requiring any knowledge of the dynamic model or its parameters for implementation. Since a linear invariant orientation error manifold is enforced for all time, a time-varying gain is introduced for a well-posed finite time convergence, which is useful not only to realize the virtual position control scheme, due to underactuation, but also to guarantee a desired contact in a given point at a given desired contact time for the yaw motion. Illustrative applications are explored in a simulation study which shows the viability and versatility of position\textendashyaw tracking in the surveillance of a field-of-view (FoV) target, aerial screw driver, and aerial grasping.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{Ramirez-Rodriguez2014,
title = {Robust Backstepping Control Based on Integral Sliding Modes for Tracking of Quadrotors},
author = {Ramirez-Rodriguez, Heriberto and Parra-Vega, Vicente and Sanchez-Orta, Anand and Garcia-Salazar, Octavio },
url = {http://dx.doi.org/10.1007/s10846-013-9909-4},
doi = {10.1007/s10846-013-9909-4},
issn = {1573-0409},
year = {2014},
date = {2014-01-01},
journal = {Journal of Intelligent \& Robotic Systems},
volume = {73},
number = {1},
pages = {51--66},
abstract = {Modern non-inertial robots are usually underactuated, such as fix or rotary wing Unmanned Aerial Vehicles (UAVs), underwater or nautical robots, to name a few. Those systems are subject to complex aerodynamic or hydrodynamic forces which make the dynamic model more difficult, and typically are subject to bounded smooth time-varying disturbances. In these systems, it is preferred a formal control approach whose closed-loop system can predict an acceptable performance since deviations may produce instability and may lead to catastrophic results. Backstepping provides an intuitive solution since it solves underactuation iteratively through slaving the actuated subsystem so as to provide a virtual controller in order to stabilize the underactuated subsystem. However it requires a full knowledge of the plant and derivatives of the state, which it is prone to instability for any uncertainty; and although robust sliding mode has been proposed, discontinuities may be harmful for air- or water-borne nonlinear plants. In this paper, a novel robust backstepping-based controller that induces integral sliding modes is proposed for the Newton--Euler underactuated dynamic model of a quadrotor subject to smooth bounded disturbances, including wind gust and sideslip aerodynamics, as well as dissipative drag in position and orientation dynamics. The chattering-free sliding mode compensates for persistent or intermittent, and possible unmatched state dependant disturbances with reduced information of the dynamic model. Representative simulations are presented and discussed.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
@article{Munoz-Vazquez2014,
title = {A Passive Velocity Field Control for Navigation of Quadrotors with Model-free Integral Sliding Modes},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and Sanchez-Orta, Anand},
url = {http://dx.doi.org/10.1007/s10846-013-9892-9},
doi = {10.1007/s10846-013-9892-9},
issn = {1573-0409},
year = {2014},
date = {2014-01-01},
journal = {Journal of Intelligent \& Robotic Systems},
volume = {73},
number = {1},
pages = {373--385},
abstract = {Velocity field (VF) control has proved effective for kinematic robots, aiming essentially at providing desired velocities for navigation along the field, and for obstacle avoidance in cluttered environments. When robot dynamics are involved, it is usually considered either that dynamics are known and that robot is fully actuated, thus it is not clear how to deal with VF control (VFC) for unknown underactuated dynamics, such as for a quadrotor. Moreover, passive VF (PVF) stands for an attractive methodology for quadrotors because of it yields time-invariant nominal spatial field for smooth approaching and easy manoeuvring. In this paper, we propose a constructive method to design a PVF-based controller with a chattering-free integral sliding modes for local exponential position tracking. The salient feature of our proposal is the passive nature of the field as well as the controller is model-free for the complete standard quasi-Lagrangian dynamic model of the quadrotor. The controller does not require the derivative nor any assumption on boundedness on the integral of the VF, yet the closed-loop withstands robustness against parametric and model uncertainties. Simulations are discussed, and remarks address the viability of the proposed approach.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
Conferencias
@conference{Mu\~{n}oz-V\'{a}zquez2014b,
title = {Attitude tracking control of a quadrotor based on absolutely continuous fractional integral sliding modes},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and Sanchez-Orta, Anand},
doi = {10.1109/CCA.2014.6981425},
issn = {1085-1992},
year = {2014},
date = {2014-00-00},
booktitle = {Attitude tracking control of a quadrotor based on absolutely continuous fractional integral sliding modes},
pages = {717-722},
organization = {iee multi-conference on system and control},
abstract = {Abstract:
The model-free sliding mode control based on fractional order sliding surface is built upon: i) An absolutely continuous control structure that does not require the exact dynamic model to induce a fractional sliding motion in finite time, and ii) A methodology to design fractional references with a clear counterpart in the frequency domain is proposed. This in order to improve the system response, in particular the transient period, and to generate a high-performance during the sliding motion. Numerical simulations support the proposal and illustrates the closed-loop system, which provides a better insight of the proposed scheme.},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
The model-free sliding mode control based on fractional order sliding surface is built upon: i) An absolutely continuous control structure that does not require the exact dynamic model to induce a fractional sliding motion in finite time, and ii) A methodology to design fractional references with a clear counterpart in the frequency domain is proposed. This in order to improve the system response, in particular the transient period, and to generate a high-performance during the sliding motion. Numerical simulations support the proposal and illustrates the closed-loop system, which provides a better insight of the proposed scheme.@conference{Munoz-Vazquez2014b,
title = {free-model fractional-order absolutely continuous sliding mode, control for euler-lagrange systems},
author = {Mu\~{n}oz-Vazquez, Aldo Jonathan and Parra-Vega, Vicente and Sanchez-Orta, Anand},
url = {http://ieeexplore.ieee.org/document/7040478/},
doi = {DOI: 10.1109/CDC.2014.7040478},
issn = {0191-2216},
year = {2014},
date = {2014-00-00},
booktitle = {free-model fractional-order absolutely continuous sliding mode, control for euler-lagrange systems},
pages = {6933-6938},
organization = {ieee conference on decision and control},
abstract = {Abstract:
Euler-Lagrange systems, such as robots, exhibit benign structural properties, including passivity, which allow us to design robust and efficient energy-shaping controllers. A great variety of passivity-based control schemes are available and recently model-based fractional order discontinuous sliding mode control has been proposed. In this paper, a fractional order absolutely continuous control scheme for Euler-Lagrange systems is proposed, without depending on the dynamic model, which enforces in finite-time a commensurable rational fractional order regime. Additionally, a frequency domain analysis is addressed, which is very useful for some applications. A numerical simulation assessment is presented, including the frequency domain response based on Bode plots. Final concluding remarks are discussed in view of the state of the art in fractional order controllers.},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
Euler-Lagrange systems, such as robots, exhibit benign structural properties, including passivity, which allow us to design robust and efficient energy-shaping controllers. A great variety of passivity-based control schemes are available and recently model-based fractional order discontinuous sliding mode control has been proposed. In this paper, a fractional order absolutely continuous control scheme for Euler-Lagrange systems is proposed, without depending on the dynamic model, which enforces in finite-time a commensurable rational fractional order regime. Additionally, a frequency domain analysis is addressed, which is very useful for some applications. A numerical simulation assessment is presented, including the frequency domain response based on Bode plots. Final concluding remarks are discussed in view of the state of the art in fractional order controllers.Proceedings Articles
@inproceedings{Martinez-Alvarado2014b,
title = {Dynamic Response of BLDC-Thruster for Small Scale Quadrotors under Aerodynamic Load Torque},
author = {Martinez-Alvarado, Ricardo and Ruiz-Sanchez, Francisco J. and Sanchez-Orta, Anand and Garcia-Salazar, Octavio},
url = {https://www.researchgate.net/publication/276958535_Dynamic_Response_of_BLDC-Thruster_for_Small_Scale_Quadrotors_under_Aerodynamic_Load_Torque},
doi = {10.1109/ROPEC.2014.7036341},
isbn = {978-1-4799-5683-8},
year = {2014},
date = {2014-01-01},
booktitle = {Dynamic Response of BLDC-Thruster for Small Scale Quadrotors under Aerodynamic Load Torque},
pages = {1-6},
organization = {iee international autumn meeting on power, electronics and computing},
abstract = {In multi-rotor UAVs, a controlled Thrust is a main factor to achieve a safe and stable flight. Thrust is the result of a coordinated action of a set of symmetrically distributed thrusters whose single contribution is usually described as a square function of its rotor speed; however, aerodynamic forces induce a load torque on the rotor that disturb its expected speed response, thus its effective Thrust, affecting the whole performance of the aircraft. In this paper, we analyse and quantify the effects of the aerodynamic load torque induced on the spinning propeller of a BLDC thruster used in small scale Quadrotors and present some experimental validation. We describe the model of a 3-phase thruster with a two blade propeller of fixed pitch angle, we analyse its numerical simulation to determine the effects of the induced load torque on the dynamic response of the rotor, and we experimentally verify the results assuming ideal conditions of hover flight. Finally we illustrate the convenience of using feedback control to reduce the sensibility of thrusters face to non modelled dynamics applying a PD controller and we discuss about the importance of an accurate dynamic model of the thruster for control purposes.
Dynamic Response of BLDC-Thruster for Small Scale Quadrotors under Aerodynamic Load Torque (PDF Download Available). Available from: https://www.researchgate.net/publication/276958535_Dynamic_Response_of_BLDC-Thruster_for_Small_Scale_Quadrotors_under_Aerodynamic_Load_Torque [accessed Jun 16, 2017].},
keywords = {},
pubstate = {published},
tppubtype = {inproceedings}
}
Dynamic Response of BLDC-Thruster for Small Scale Quadrotors under Aerodynamic Load Torque (PDF Download Available). Available from: https://www.researchgate.net/publication/276958535_Dynamic_Response_of_BLDC-Thruster_for_Small_Scale_Quadrotors_under_Aerodynamic_Load_Torque [accessed Jun 16, 2017].@inproceedings{Mart\'{i}nez-Alvarado2014,
title = {performance evaluation of propeller-engine systems for unmanned aerial vehicles in hovering},
author = {Mart\'{i}nez-Alvarado, Ricardo and S\'{a}nchez-Orta, Anand and Granda-Guti\'{e}rrez, E. and Ruiz-Sanchez, Francisco J.},
url = {https://www.researchgate.net/publication/267094930_PERFORMANCE_EVALUATION_OF_PROPELLER-ENGINE_SYSTEMS_FOR_UNMANNED_AERIAL_VEHICLES_IN_HOVERING_MODE},
issn = {1405-2172},
year = {2014},
date = {2014-00-00},
booktitle = {performance evaluation of propeller-engine systems for unmanned aerial vehicles in hovering},
volume = {36},
pages = {131-136},
publisher = {congreso internacional en ingenieria electronica electro 2014},
abstract = {A flexible tool to dimensioning and optimizing the performance of a propeller-engine system for multi-rotor Unmanned Aerial Vehicles (UAVs) is proposed. The study is centered on an experimental platform designed to identify the dynamic behavior of the thruster which operates as main actuator in multi-rotor UAVs. The aim is to optimize the performance of the propulsion system with basis on its dynamic behavior. The dynamic of an UAV changes notably according to the performance of the thruster, which is composed by a propeller coupled to a Brushless Direct Current (BLDC) Motor. The dynamic response of the propulsion system is acquired from the experimental data, including the electric, mechanical and aerodynamic effects of the wing when the propeller is the load of the rotor. The experimental platform allows evaluating the performance of the system and determining the payload for a UAV, but also validates control laws to regulate the thruster action.
PERFORMANCE EVALUATION OF PROPELLER-ENGINE SYSTEMS FOR UNMANNED AERIAL VEHICLES IN HOVERING MODE (PDF Download Available). Available from: https://www.researchgate.net/publication/267094930_PERFORMANCE_EVALUATION_OF_PROPELLER-ENGINE_SYSTEMS_FOR_UNMANNED_AERIAL_VEHICLES_IN_HOVERING_MODE [accessed Jun 16, 2017].},
keywords = {},
pubstate = {published},
tppubtype = {inproceedings}
}
PERFORMANCE EVALUATION OF PROPELLER-ENGINE SYSTEMS FOR UNMANNED AERIAL VEHICLES IN HOVERING MODE (PDF Download Available). Available from: https://www.researchgate.net/publication/267094930_PERFORMANCE_EVALUATION_OF_PROPELLER-ENGINE_SYSTEMS_FOR_UNMANNED_AERIAL_VEHICLES_IN_HOVERING_MODE [accessed Jun 16, 2017].
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