Input saturated visual servoing for unmanned aerial vehicles

H Xie, AF Lynch - IEEE/ASME Transactions on Mechatronics, 2016 - ieeexplore.ieee.org
This paper presents an input saturated visual servoing controller for a quadrotor unmanned
aerial vehicle (UAV). The controller regulates relative pose between the vehicle and a …

Keeping a ground point in the camera field of view of a landing UAV

L Burlion, H De Plinval - 2013 IEEE International Conference …, 2013 - ieeexplore.ieee.org
This paper proposes a key feature for vision based automatic landing of a UAV: the addition
to a given control law of the constraint that a given ground point be maintained in the camera …

Dynamic visual servoing of rotary wing unmanned aerial vehicles

H Xie - 2016 - era.library.ualberta.ca
Dynamic Visual Servoing of Rotary Wing Unmanned Aerial Vehicles Hui Xie Doctor of
Philosophy Control Systems Page 1 Dynamic Visual Servoing of Rotary Wing Unmanned Aerial …

Adaptive dynamic positioning control for accommodation vessels with multiple constraints

F Tu, S Sam Ge, YS Choo… - IET Control Theory & …, 2017 - Wiley Online Library
In this study, adaptive constrained control with non‐linear adaptive filter is proposed for the
dynamic positioning of an accommodation vessel (AV) in deep water area. To reduce wear …

Longitudinal manoeuvre load control of a flexible large-scale aircraft

L Burlion, C Poussot-Vassal, P Vuillemin… - IFAC Proceedings …, 2014 - Elsevier
This paper discusses the design and validation of an integrated long range flexible aircraft
load controller, at a single flight/mass configuration. The contributions of the paper are in …

Time-response shaping using output to input saturation transformation

E Chambon, L Burlion, P Apkarian - International Journal of Control, 2018 - Taylor & Francis
For linear systems, the control law design is often performed so that the resulting closed loop
meets specific frequency-domain requirements. However, in many cases, it may be …

Toward vision based landing of a fixed-wing UAV on an unknown runway under some fov constraints

L Burlion, H De Plinval - 2017 International Conference on …, 2017 - ieeexplore.ieee.org
In this article, a vision based landing framework is proposed for fixed-wing UAVs. Being able
to automatically land a UAV without on-ground instrumentation or in the case of eg GPS …

Attitude tracking control of a flexible spacecraft under angular velocity constraints

L Burlion, JM Biannic, T Ahmed-Ali - International journal of control, 2019 - Taylor & Francis
In this paper, a new technique is proposed for trajectory tracking of a flexible spacecraft
subject to angular velocity constraints. The problem is addressed using an output to input …

UAV obstacle avoidance scheme using an output to input saturation transformation technique

C Chauffaut, F Defaÿ, L Burlion… - … on Unmanned Aircraft …, 2016 - ieeexplore.ieee.org
This paper presents a novel obstacle avoidance scheme for UAVs. This scheme is based on
the use of a technique recently developed by one of the authors, which is based on a …

Robust output interval constraint using O/I saturation transformation with application to uncertain linear launch vehicle

E Chambon, L Burlion… - 2015 European Control …, 2015 - ieeexplore.ieee.org
In this article, the case is considered where a regulated output of an uncertain system with
unknown disturbance input is constrained to lie between two specified time-varying bounds …