The tuning of Pareto-optimal robust controllers was applied to improve the performance of a helicopter with two-degrees-of-freedom with a linear control algorithm. The tuning procedure is based on the simultaneous minimization of the integral of square sum of errors and the integral of square sum of control action. A 2D Pareto front is built with these integrals. Afterwards, a decision-making process is carried out to select the most preferable controller. Experimental results on the physical platform validate the tuning procedure as practical and reliable
[EN] This paper presents the design of a robust nonlinear controller for a scaled helicopter. This d...
This article focuses on linear matrix inequality-based controller designs that can achieve stabiliza...
This paper presents a new robust controller design approach to the yaw control of a small-scale heli...
ResumenLa sintonización de controladores Pareto-óptimo robustos ha sido empleada para mejorar el ren...
This thesis addresses some of the issues associated with linear systems subject to nonlinearities at...
This thesis describes the design and flight testing of advanced robust multivariable control laws fo...
This thesis presents one of the first applications of H∞-optimization to the design of controllers f...
Autonomous helicopter stabilization in the presence of a wind disturbance is presented. A controller...
This work proposes an improved technique for design and optimization of robust controllers norm for ...
This paper presents a robust state feedback controller tuning via constrained optimization using DE ...
This project aims at designing an on-line controller in the form of a Multi Input\ud Multi Output Se...
This thesis is concerned with controller design for helicopter systems. The emphasis will be focused...
This work comprehensively studies principal component active control systems, where plant uncertaint...
Control of autonomous helicopters in the presence of environmental and system uncertain-ties is a ch...
This paper presents an optimal state feedback controller based on Linear Quadratic Regulator (LQR) f...
[EN] This paper presents the design of a robust nonlinear controller for a scaled helicopter. This d...
This article focuses on linear matrix inequality-based controller designs that can achieve stabiliza...
This paper presents a new robust controller design approach to the yaw control of a small-scale heli...
ResumenLa sintonización de controladores Pareto-óptimo robustos ha sido empleada para mejorar el ren...
This thesis addresses some of the issues associated with linear systems subject to nonlinearities at...
This thesis describes the design and flight testing of advanced robust multivariable control laws fo...
This thesis presents one of the first applications of H∞-optimization to the design of controllers f...
Autonomous helicopter stabilization in the presence of a wind disturbance is presented. A controller...
This work proposes an improved technique for design and optimization of robust controllers norm for ...
This paper presents a robust state feedback controller tuning via constrained optimization using DE ...
This project aims at designing an on-line controller in the form of a Multi Input\ud Multi Output Se...
This thesis is concerned with controller design for helicopter systems. The emphasis will be focused...
This work comprehensively studies principal component active control systems, where plant uncertaint...
Control of autonomous helicopters in the presence of environmental and system uncertain-ties is a ch...
This paper presents an optimal state feedback controller based on Linear Quadratic Regulator (LQR) f...
[EN] This paper presents the design of a robust nonlinear controller for a scaled helicopter. This d...
This article focuses on linear matrix inequality-based controller designs that can achieve stabiliza...
This paper presents a new robust controller design approach to the yaw control of a small-scale heli...