Dynamic surface neuro-backstepping based flight control with asymmetric output constraints

P Singh, DK Giri, AK Ghosh - IEEE Transactions on Aerospace …, 2022 - ieeexplore.ieee.org
In this article, flight path angle of the aircraft is controlled asymptotically for a class of
nonstrict feedback system by employing robust backstepping dynamic surface control. First …

Nonlinear control of aircraft flight dynamics using integrator-backstepping design method

TT Tran, VH Nguyen - Journal of Aerospace Engineering, 2022 - ascelibrary.org
This paper investigated a nonlinear control algorithm for flight dynamics of aircraft using an
integrator backstepping–based design. The paper focused on two points. Firstly, a …

Flying qualities evaluation based nonlinear flight control law design method for aircraft

L Sun, L Shi, W Tan, X Liu - Aerospace Science and Technology, 2020 - Elsevier
This paper is focused on the parameter tuning problem for the design of nonlinear flight
controllers. Taking into account the preferences and requirements of the pilot, a novel flying …

Robust sliding mode augmenting integral backstepping for lateral-directional control of a highly maneuverable aircraft

P Singh, DK Giri, AK Ghosh - Proceedings of the Institution of …, 2023 - journals.sagepub.com
In this paper, a robust hybrid backstepping and sliding mode control is designed for lateral-
directional control of a highly maneuverable aircraft. A systematic approach is implemented …

Backstepping-based control methodology for aircraft roll dynamics

TT Tran, OR Gonzalez - … Engineers, Part I: Journal of Systems …, 2020 - journals.sagepub.com
This article investigates a backstepping-based control method for aircraft roll dynamics. The
research starts with a formulation of backstepping control law for a general class of a strict …

Simulador de vuelo y comportamiento dinámico para modelos de aeronaves

SR Peñasco-Goel… - … Ciencias Básicas e …, 2023 - repository.uaeh.edu.mx
El artículo describe un proyecto enfocado a la investigación del control del movimiento de
un modelo a escala de una aeronave de ala fija en tres ejes estacionarios, así como …

A Novel Hybrid Robust Control Design Method for F‐16 Aircraft Longitudinal Dynamics

VH Nguyen, TT Tran - Mathematical Problems in Engineering, 2020 - Wiley Online Library
This paper presents a hybrid robust control design method for a third‐order lower‐triangular
model of nonlinear dynamic systems in the presence of disturbance. In this paper, a novel …

A novel intelligent control system design for aircraft flight dynamics

VH Nguyen, TT Tran - 2021 International Conference on …, 2021 - ieeexplore.ieee.org
A novel design of intelligent flight control system is proposed for nonlinear aircraft dynamic
systems, in which a proposed control system can allow aircraft to learn-to-fly (L2F) and …

[图书][B] Nonlinear flight control design using backstepping methodology

TT Tran - 2016 - search.proquest.com
The subject of nonlinear flight control design using backstepping control methodology is
investigated in the dissertation research presented here. Control design methods based on …

[PDF][PDF] A Joint Attitude Control Method for Small Unmanned Aerial Vehicles Based on Prediction Incremental Backstepping.

T Xie, J Zheng, SC Chu - J. Inf. Hiding Multim. Signal Process., 2016 - bit.nkust.edu.tw
A new second-order joint attitude control method for Small Unmanned Aerial Vehicles
(SUAVs) is presented in this paper. Based on lyapunov theory, a second-order backstepping …