[HTML][HTML] Nonlinear robust adaptive NN control for variable-sweep aircraft

Z Ma, J Feng, J Hu, A Liu - Journal of Vibroengineering, 2018 - extrica.com
In this paper, we address the problem of altitude and velocity controllers design for variable-
sweep aircraft with model uncertainties. The object is to maintain altitude and velocity during …

Robust adaptive neural control of morphing aircraft with prescribed performance

Z Wu, J Lu, J Shi, Y Liu, Q Zhou - Mathematical Problems in …, 2017 - Wiley Online Library
This study proposes a low‐computational composite adaptive neural control scheme for the
longitudinal dynamics of a swept‐back wing aircraft subject to parameter uncertainties. To …

Adaptive neural control based on high order integral chained differentiator for morphing aircraft

Z Wu, J Lu, J Rajput, J Shi, W Ma - Mathematical Problems in …, 2015 - Wiley Online Library
This paper presents an adaptive neural control for the longitudinal dynamics of a morphing
aircraft. Based on the functional decomposition, it is reasonable to decompose the …

Adaptive NN control for multisteering plane aircraft with dead zone or backlash input nonlinearity

X Meng, Y Wang, M Lv - Mathematical Problems in …, 2017 - Wiley Online Library
Considering that many factors such as actuator input dead zone, backlash, and external
disturbance could affect the exactness of trajectory tracking, therewith a robust adaptive …

Research on Flight Control of High-Aspect-Ratio Unmanned Aerial Vehicles Based on L1 Adaptive Control

S Hao, X Duan, B Xiao, T Li… - 2023 6th International …, 2023 - ieeexplore.ieee.org
The geometry nonlinear aeroelastic problems of the high-aspect-ratio unmanned aerial
vehicles (UAV) are prominent, which will bring many adverse factors to flight control. A high …

Modified adaptive neural dynamic surface control for morphing aircraft with input and output constraints

Z Wu, J Lu, Q Zhou, J Shi - Nonlinear Dynamics, 2017 - Springer
In this paper, a barrier Lyapunov function-based adaptive neural dynamic surface control
approach is proposed for morphing aircraft subject to unknown parameters and input–output …

Attitude tracking control of aircraft subjected to unsteady aerodynamic disturbance

D Wu, H Gong, M Chen - 2016 International Conference on …, 2016 - ieeexplore.ieee.org
In this paper, a robust adaptive tracking control scheme is proposed for the lateral attitude
dynamic of an aircraft in the presence of unmeasured unsteady aerodynamic disturbance …

[PDF][PDF] Near Space Hypersonic Unmanned Aerial Vehicle Dynamic Surface Backstepping Control Design

J Yu, J Chen, C Wang, S Li - Sensors & Transducers, 2014 - sensorsportal.com
Compared with traditional aircraft, the near space hypersonic unmanned aerial vehicle
control system design must deal with the extra prominent dynamics characters, which are …

Adaptive neural dynamic surface control of morphing aircraft with input constraints

Z Wu, J Lu, J Shi - 2017 29th Chinese Control And Decision …, 2017 - ieeexplore.ieee.org
A robust adaptive neural dynamic surface control (DSC) approach is presented for the
longitudinal dynamics of a morphing aircraft in the presence of unknown dynamics and input …

Adaptive flight control law based on neural networks and dynamic inversion for unmanned aerial vehicle

Y Ning, W Liao-ni, L Qi - 2012 - IET
For the small-sized UAV, the paper puts forward a nonlinear control method based on
dynamic inversion. In order to compensate the dynamic inversion error, the paper designs …