Advantages of fuzzy control while dealing with complex/unknown model dynamics: A quadcopter example

L Ibarra, C Webb - New Appl. Artif. Intell, 2016 - books.google.com
Commonly, complex and uncertain plants cannot be faced through well-known linear
approaches. Most of the time, complex controllers are needed to attain expected stability …

Adaptive neural network based sliding mode altitude control for a quadrotor UAV

H Razmi - Journal of Central South University, 2018 - Springer
Reasons and realities such as being non-linear of dynamical equations, being lightweight
and unstable nature of quadrotor, along with internal and external disturbances and …

Design of an Intelligent Controller of a Self-Tuned Quadcopter for IoT-Based Application on COVID Infected Area Sanitization

MD Mohanty, PK Mallick… - IEEE Internet of Things …, 2021 - ieeexplore.ieee.org
The COVID-19 outbreak has created a major global health crisis that has had an impact on
the actions we perform. The only solution to the problem is getting sanitized and maintaining …

Robust flight control of a small unmanned helicopter

M He, J He, X Zhou - arXiv preprint arXiv:2101.09937, 2021 - arxiv.org
This paper addresses the design and application controller for a small-size unmanned aerial
vehicle (UAV). In this work, the main objective is to study the modeling and attitude controller …

Optimal direct adaptive fuzzy controller based on bat algorithm for UAV quadrotor

HE Glida, L Abdou, A Chelihi… - 2019 8th International …, 2019 - ieeexplore.ieee.org
An optimal direct robust adaptive fuzzy controller (ODAFC) for a quadrotor system using bat
algorithm (BA) is presented in this paper. The concept of this approach is to decouple the …

Different control scheme for the quadcopter: a Brief tour

S Kumar, L Dewan - 2020 First IEEE International Conference …, 2020 - ieeexplore.ieee.org
This paper given brief tour on the different control techniques for the quadcopter that can
improve the flight control stability and trajectory tracking of a quadcopter. Four main control …

[PDF][PDF] 小型无人直升机鲁棒飞行控制

何淼磊, 贺继林, 周烜亦 - 机器人, 2016 - academia.edu
针对小型无人直升机的全自主飞行控制问题, 提出一种基于直升机悬停模型的快速优化H∞
鲁棒控制器的设计方法, 设计了基于降阶观测器的双闭环的飞行控制器. 内环控制器采用H∞ …

Research on Nonlinear Guidance Law Design for UAV-to-Ground Attack Under Field-of-View Constraint

C Haiyue, L Yue, Y Jun - 2023 42nd Chinese Control …, 2023 - ieeexplore.ieee.org
This paper addresses the guidance law design problem for unmanned aerial vehicles
(UAVs) to attack ground targets by presenting the three-dimensional relative motion …

Modelling, Controller Design and Simulation of Quadrotor Aircraft Based on Cascade PID

Q Zhong, C Wang, Q Guo, J Yang - 2023 5th International …, 2023 - ieeexplore.ieee.org
The quadrotor vehicle control system possesses characteristics such as nonlinearity and
strong coupling. This paper presents a design for a quadcopter unmanned aerial vehicle …

Optimal Trajectory Generation of UAV Considering Attitude Constraints

C Liu, H Zhou, X Dong, D Wang - … ICGNC 2020, Tianjin, China, October 23 …, 2022 - Springer
The six degrees of freedom (6-DOF) trajectory planning of quadrotors with attitude
constraints is studied. Based on active disturbance rejection control (ADRC) technology, a …