版权所有:内蒙古大学图书馆 技术提供:维普资讯• 智图
内蒙古自治区呼和浩特市赛罕区大学西街235号 邮编: 010021
出 版 物:《IFAC-PapersOnLine》
年 卷 期:2018年第51卷第22期
页 面:312-317页
核心收录:
主 题:Aircraft control Actuators Antennas Fault tolerance Unmanned aerial vehicles (UAV) Control allocation Control allocation problem Controllability studies Explicit solutions Fault tolerant control Hexarotor Parametric programming Recovery strategies
摘 要:This paper presents a fault-tolerant control approach for actuators failures in multirotor Unmanned Aerial Vehicles UAVs. The strategy is applied on an hexarotor UAV. First, the hexarotor model is derived by means of the Newton-Euler formalism. A Controllability study based on the modified Kalman Rank condition is presented in case of one or more failing motors. A control allocation based recovery strategy is applied on the hexarotor when it is controllable. The control allocation problem is stated using a parametric programming formulation and is solved for an explicit solution. Outdoor real-time experimental results demonstrate the effectiveness of the applied strategy. © 2018