<?xml version="1.0" encoding="UTF-8"?><xml><records><record><source-app name="Biblio" version="7.x">Drupal-Biblio</source-app><ref-type>10</ref-type><contributors><authors><author><style face="normal" font="default" size="100%">Yacine Aoun</style></author><author><style face="normal" font="default" size="100%">Medjghou, Ali</style></author><author><style face="normal" font="default" size="100%">Slimane, Noureddine</style></author><author><style face="normal" font="default" size="100%">Bedreddine Maaoui</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">Improved Sliding Mode Controller Using Backstepping and Fuzzy Logic for a Quadrotor Aircraft</style></title><secondary-title><style face="normal" font="default" size="100%">International Symposium on Mechatronics and Renewable Energies  10- 11 December </style></secondary-title></titles><dates><year><style  face="normal" font="default" size="100%">2018</style></year><pub-dates><date><style  face="normal" font="default" size="100%">2018</style></date></pub-dates></dates><urls><web-urls><url><style face="normal" font="default" size="100%">http://dspace.univ-eloued.dz/bitstream/123456789/1383/1/Improved%20Sliding%20Mode%20Controller%20Using.pdf</style></url></web-urls></urls><pub-location><style face="normal" font="default" size="100%">El-oued, Algérie</style></pub-location><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">&lt;p style=&quot;text-align: justify;&quot;&gt;
	In this work, a new robust nonlinear controller is presented in presence of large external disturbances for a quadrotor aircraft. The controller is based on an improved sliding mode control. The improvement is done by adding two other terms, one is a backstepping synthesis and the other one is a fuzzy logic term in order to reduce the chattering phenomenon and achieve more acceptable performance. The dynamical motion equations are obtained by Euler-Newton formalism. Lyapunov theorem is used to prove the stability of control system. A simulation is carried out to illustrate the effectiveness of the proposed control.
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