M Labbadi, M Cherkaoui - IEEE Transactions on Aerospace …, 2021 - ieeexplore.ieee.org
Random external disturbances/parametric uncertainties and other factors deteriorate the tracking control performances of the quadrotor unmanned aerial vehicle (QUAV). To achieve …
With the increasing use of quadrotors, the design of flight control systems has become particularly important. In this paper, a new robust flight control system consisted of an …
B Brogliato - Annual Reviews in Control, 2023 - Elsevier
So-called robot–object Lagrangian systems consist of a class of nonsmooth underactuated complementarity Lagrangian systems, with a specific structure: an “object” and a “robot” …
S Roy, S Baldi, P Li… - … /ASME Transactions on …, 2021 - ieeexplore.ieee.org
Artificial-delay control is a method in which state and input measurements collected at an immediate past time instant (ie, artificially delayed) are used to compensate the uncertain …
L Kong, J Reis, W He, C Silvestre - IEEE Transactions on …, 2023 - ieeexplore.ieee.org
In this article, we develop a methodology for trajectory tracking control of a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) in the presence of unknown mass and …
W Liu, M Chen, P Shi - … Transactions on Circuits and Systems I …, 2022 - ieeexplore.ieee.org
By considering the under-actuated characteristics of the quadcopter suspension transportation system and the external disturbance, the effective tracking control of the …
B Xian, S Yang - IEEE/ASME Transactions on Mechatronics, 2020 - ieeexplore.ieee.org
In this article, the control problem for the underactuated dynamic system, which consists of a quadrotor unmanned aerial vehicle and a suspended payload is investigated under the …
Two novel nonlinear control schemes for Unmanned Aerial Vehicles (UAV) carrying a load and their comparative results are presented in this paper. The goal is to carry the load to a …
J Wang, B Zhu, Z Zheng - IEEE Transactions on Aerospace and …, 2023 - ieeexplore.ieee.org
In controller design for quadrotors, the drag coefficients, thrust coefficients, and aerodynamic damping coefficients are usually unmeasurable, and they have to be regarded as uncertain …