Quadrotor fault tolerant incremental sliding mode control driven by sliding mode disturbance observers

X Wang, S Sun, EJ van Kampen, Q Chu - Aerospace Science and …, 2019 - Elsevier
This paper proposes an Incremental Sliding Mode Control driven by Sliding Mode
Disturbance Observers (INDI-SMC/SMDO), with application to a quadrotor fault tolerant …

Review on wind resistance for quadrotor UAVs: Modeling and controller design

J Shen, B Wang, BM Chen, R Bu, B Jin - Unmanned Systems, 2023 - World Scientific
Micro-Unmanned Air Vehicles (Micro-UAVs), especially quadrotor UAVs, have been widely
used in recent years because of their simple structure and convenient operation. However …

Robust backstepping sliding mode aircraft attitude and altitude control based on adaptive neural network using symmetric BLF

P Singh, DK Giri, AK Ghosh - Aerospace Science and Technology, 2022 - Elsevier
In this paper, asymptotic control of attitude and altitude of the aircraft is proposed by
employing robust backstepping sliding mode control (BSMC) in conjunction with adaptive …

Command-filtered incremental backstepping attitude control of spacecraft with predefined-time stability

H Zhang, H Huang, B Xiao, K Dong - Aerospace Science and Technology, 2024 - Elsevier
This paper investigates the predefined-time attitude tracking control problem within the
theoretical framework of incremental dynamic inversion. The utilization of the Taylor series …

Incremental model-based global dual heuristic programming with explicit analytical calculations applied to flight control

B Sun, EJ van Kampen - Engineering Applications of Artificial Intelligence, 2020 - Elsevier
A novel adaptive dynamic programming method, called incremental model-based global
dual heuristic programming, is proposed to generate a self-learning adaptive flight …

Nonlinear incremental control for flexible aircraft trajectory tracking and load alleviation

X Wang, T Mkhoyan, R De Breuker - Journal of Guidance, Control, and …, 2022 - arc.aiaa.org
This paper proposes a nonlinear control architecture for flexible aircraft simultaneous
trajectory tracking and load alleviation. By exploiting the control redundancy, the gust and …

Null-Space-Excitation-Based Adaptive Control for an Overactuated Hexacopter Model

H Li, S Myschik, F Holzapfel - Journal of Guidance, Control, and …, 2023 - arc.aiaa.org
This paper proposes a novel adaptive control structure featured by large closed-loop
bandwidth and satisfactory parameter estimation results. The proposed baseline control …

Unified backstepping sliding mode framework for airship control design

HS Vieira, EC de Paiva, SK Moriguchi… - … on Aerospace and …, 2020 - ieeexplore.ieee.org
This article presents a new kind of vectorial backstepping sliding mode control (BSMC) for
the positioning and trajectory tracking of an autonomous robotic airship. Also, a unified …

Observer-based incremental backstepping sliding-mode fault-tolerant control for blended-wing-body aircrafts

SQ Liu, JF Whidborne - Neurocomputing, 2021 - Elsevier
This paper presents an adaptive incremental nonlinear backstepping sliding-mode (INBSM)
controller, for fault tolerant tracking control of a blended wing body (BWB) aircraft with …

Adaptive finite-time incremental backstepping fault-tolerant control for flying-wing aircraft with state constraints

W Li, X Han, Y Zhi, B Wang, L Liu, H Fan - Aerospace Science and …, 2024 - Elsevier
This paper proposes an incremental nonlinear fault-tolerant control scheme for flying-wing
aircraft subject to state constraints under model uncertainties, external disturbances, and …