Abstract—This paper considers the problem of constrained nonlinear trajectory tracking control for unmanned air vehicles (UAVs). We assume that the UAV is equipped with longitudinal and lateral autopilots which reduces the 12-state model to a six-state model with altitude, heading, and velocity command inputs. One of the novel features of our approach is that we explicitly account for heading rate and velocity input constraints. For a UAV, the velocity is constrained to lie between two positive constants, and therefore presents particular challenges for the control design. We propose a control Lyapunov function (CLF) approach. We first introduce a CLF for the input constrained case, and then construct the set of all constrained inputs that ...
Methods from linear control theory have a considerable share in the state-of-the-art toolbox for con...
We study tracking controller design problems for key models of planar vertical takeoff and landing (...
In this work, a sliding-mode-based attitude controller constrained with the angular rate for unmanne...
We study an important class of tracking problems for unmanned air vehicles (UAVs) with input constra...
In this paper, we study the problem of controlling an unmanned aerial vehicle (UAV) to provide a tar...
This paper provides a solution to the problem of ground target tracking using an unmanned aerial veh...
With growing worldwide interests in commercial, scientific, and military issues, there has been a co...
International audienceWe study an important class of tracking problems for unmanned air vehicles (UA...
International audiencePath following is a basic autonomous navigation capability for UAV’s and in th...
This work proposes an adaptive dynamic controller to guide an unmanned aerial vehicle (UAV) when acc...
Abstract — This paper presents experimental results of nonlinear trajectory tracking controllers for...
This paper deals with the problem of adversarial ground target tracking using Unmanned Aerial Vehicl...
The last decade has seen significant advances in the development of Vertical takeoff and landing (VT...
International audienceThis paper addresses a predictive control strategy for Unmanned Air Vehicles i...
The flight trajectory of unmanned aerial vehicles (UAVs) can be significantly affected by external d...
Methods from linear control theory have a considerable share in the state-of-the-art toolbox for con...
We study tracking controller design problems for key models of planar vertical takeoff and landing (...
In this work, a sliding-mode-based attitude controller constrained with the angular rate for unmanne...
We study an important class of tracking problems for unmanned air vehicles (UAVs) with input constra...
In this paper, we study the problem of controlling an unmanned aerial vehicle (UAV) to provide a tar...
This paper provides a solution to the problem of ground target tracking using an unmanned aerial veh...
With growing worldwide interests in commercial, scientific, and military issues, there has been a co...
International audienceWe study an important class of tracking problems for unmanned air vehicles (UA...
International audiencePath following is a basic autonomous navigation capability for UAV’s and in th...
This work proposes an adaptive dynamic controller to guide an unmanned aerial vehicle (UAV) when acc...
Abstract — This paper presents experimental results of nonlinear trajectory tracking controllers for...
This paper deals with the problem of adversarial ground target tracking using Unmanned Aerial Vehicl...
The last decade has seen significant advances in the development of Vertical takeoff and landing (VT...
International audienceThis paper addresses a predictive control strategy for Unmanned Air Vehicles i...
The flight trajectory of unmanned aerial vehicles (UAVs) can be significantly affected by external d...
Methods from linear control theory have a considerable share in the state-of-the-art toolbox for con...
We study tracking controller design problems for key models of planar vertical takeoff and landing (...
In this work, a sliding-mode-based attitude controller constrained with the angular rate for unmanne...