Publications

@conference{Walid2014343b,

title = {Modeling and control of a quadrotor UAV},

author = {Mizouri Walid and Najar Slaheddine and Aoun Mohamed and Bouabdallah Lamjed},

url = {https://www.scopus.com/inward/record.uri?eid=2-s2.0-84949924882\&doi=10.1109%2fSTA.2014.7086762\&partnerID=40\&md5=db71272eff7a282d2cd18cd653d2cd93},

doi = {10.1109/STA.2014.7086762},

year  = {2014},

date = {2014-01-01},

journal = {STA 2014 - 15th International Conference on Sciences and Techniques of Automatic Control and Computer Engineering},

pages = {343 \textendash 348},

abstract = {In the recent years, the control of Unmanned Aerial Vehicles (UAV) has become one of the most interesting field of research, especially for Vertical Take-Off and Landing vehicles (VTOL), due to the needs to such system, the simplicity of their construction and due to the important technological advances in control boards, sensors, communication tools, energy storage. In this paper, a mathematical model has been developed with Lagrange formalism and a control approach based on Proportional Derivative PD controller has been built and provided with numerical simulation in MATLAB/Simulink. © 2014 IEEE.},

note = {Cited by: 20},

keywords = {Automation, Communication tools, Lagrange formalism, MATLAB, Modeling and control, Models, PD control, Proportional derivatives, Quad rotors, Technological advances, Trajectories, Unmanned aerial vehicles (UAV), Vehicle to vehicle communications, Vehicles, Vertical take-off and landings},

pubstate = {published},

tppubtype = {conference}

}

@conference{Walid2014343,

title = {Modeling and control of a quadrotor UAV},

author = {Mizouri Walid and Najar Slaheddine and Aoun Mohamed and Bouabdallah Lamjed},

url = {https://www.scopus.com/inward/record.uri?eid=2-s2.0-84949924882\&doi=10.1109%2fSTA.2014.7086762\&partnerID=40\&md5=db71272eff7a282d2cd18cd653d2cd93},

doi = {10.1109/STA.2014.7086762},

year  = {2014},

date = {2014-01-01},

journal = {STA 2014 - 15th International Conference on Sciences and Techniques of Automatic Control and Computer Engineering},

pages = {343 \textendash 348},

abstract = {In the recent years, the control of Unmanned Aerial Vehicles (UAV) has become one of the most interesting field of research, especially for Vertical Take-Off and Landing vehicles (VTOL), due to the needs to such system, the simplicity of their construction and due to the important technological advances in control boards, sensors, communication tools, energy storage. In this paper, a mathematical model has been developed with Lagrange formalism and a control approach based on Proportional Derivative PD controller has been built and provided with numerical simulation in MATLAB/Simulink. © 2014 IEEE.},

note = {Cited by: 20},

keywords = {Automation, Communication tools, Lagrange formalism, MATLAB, Modeling and control, Models, PD control, Proportional derivatives, Quad rotors, Technological advances, Trajectories, Unmanned aerial vehicles (UAV), Vehicle to vehicle communications, Vehicles, Vertical take-off and landings},

pubstate = {published},

tppubtype = {conference}

}