Non-Linear Control for Underactuated Mechanical Systems
Non-Linear Control for Underactuated Mechanical Systems
L2-Gain and Passivity Techniques in Nonlinear Control
L2-Gain and Passivity Techniques in Nonlinear Control
Nonlinear control of underactuated mechanical systems with application to robotics and aerospace vehicles
Robustness improvement of a nonlinear H∞ controller for robot manipulators via saturation functions
Journal of Robotic Systems
Exact linearization and sliding mode observer for a quadrotor unmanned aerial vehicle
International Journal of Robotics and Automation
Two inertial models of X4-flyers dynamics, motion planning and control
Integrated Computer-Aided Engineering
A predictive controller for autonomous vehicle path tracking
IEEE Transactions on Intelligent Transportation Systems
Modelling and Control of Mini-Flying Machines
Modelling and Control of Mini-Flying Machines
A Practical Visual Servo Control for an Unmanned Aerial Vehicle
IEEE Transactions on Robotics
A Diagnostic Thau Observer for a Class of Unmanned Vehicles
Journal of Intelligent and Robotic Systems
Trajectory Tracking Control for a Rotary Wing Vehicle Powered by Four Rotors
Journal of Intelligent and Robotic Systems
Modeling and Adaptive Tracking Control of a Quadrotor UAV
International Journal of Intelligent Mechatronics and Robotics
Robust H∞ attitude control of a laboratory helicopter
Robotics and Autonomous Systems
Hard Real-Time Implementation of a Nonlinear Controller for the Quadrotor Helicopter
Journal of Intelligent and Robotic Systems
Adaptive Nonlinear Stabilization Control for a Quadrotor UAV: Theory, Simulation and Experimentation
Journal of Intelligent and Robotic Systems
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This paper presents an integral predictive and nonlinear robust control strategy to solve the path following problem for a quadrotor helicopter. The dynamic motion equations are obtained by the Lagrange-Euler formalism. The proposed control structure is a hierarchical scheme consisting of a model predictive controller (mpc) to track the reference trajectory together with a nonlinear H"~ controller to stabilize the rotational movements. In both controllers the integral of the position error is considered, allowing the achievement of a null steady-state error when sustained disturbances are acting on the system. Simulation results in the presence of aerodynamic disturbances, parametric and structural uncertainties are presented to corroborate the effectiveness and the robustness of the proposed strategy.