2008 47th IEEE Conference on Decision and Control 2008
DOI: 10.1109/cdc.2008.4738814
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Neural network output feedback control of a quadrotor UAV

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Cited by 35 publications
(26 citation statements)
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“…is the general form of a skew symmetric matrix defined as in (Dierks & Jagannathan, 2008 , and this property is commonly referred to as the skew symmetric property (Lewis et al, 1999). The matrix…”
Section: Quadrotor Uav Dynamicsmentioning
confidence: 99%
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“…is the general form of a skew symmetric matrix defined as in (Dierks & Jagannathan, 2008 , and this property is commonly referred to as the skew symmetric property (Lewis et al, 1999). The matrix…”
Section: Quadrotor Uav Dynamicsmentioning
confidence: 99%
“…Consider a quadrotor UAV with six DOF defined in the inertial coordinate frame , E , and the dynamics of the UAV in the body fixed frame can be written as (Dierks & Jagannathan, 2008) …”
Section: Quadrotor Uav Dynamicsmentioning
confidence: 99%
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“…Meanwhile, the system behaviour can deteriorate when actuator, sensor or plant faults take place. Many control approaches have been investigated for the quad-rotor helicopter, such as backstepping control [6], sliding mode control [7], LQ control [8] and neural network control [9], to solve these problems.…”
Section: Introductionmentioning
confidence: 99%
“…Some theoretical works consider the problems of control (Dierks & Jagannathan, 2008), formation flight (Dierks & Jagannathan, 2009) and fault diagnosis (Nguyen et al, 2009;Rafaralahy et al, 2008) of the quadrotor UAV. However, few research laboratories are carrying out advanced theoretical and experimental works on the system.…”
Section: Introductionmentioning
confidence: 99%