Metaheuristic-assisted complex H-infinity flight control tuning for the Hawkeye unmanned aerial vehicle: A comparative study

Y Kanokmedhakul, S Bureerat, N Panagant… - Expert Systems with …, 2024 - Elsevier
Selecting weighting factors for H-infinity controller requires tones of knowledge and
experience without guaranteeing obtaining the best results. This paper proposes novel idea …

Modified monarch butterfly optimization with distribution functions and its application for 3 DOF Hover flight system

A Ates, M Akpamukcu - Neural Computing and Applications, 2022 - Springer
Abstract In this study, Modified Monarch Butterfly Optimization Algorithm (M 2 BO) is
proposed by modeling stochastic processes in Monarch Butterfly Optimization (MBO) …

Aerodynamic characterisation of delta wing unmanned aerial vehicle using non-gradient-based estimator

N Kumar, S Saderla, Y Kim - The Aeronautical Journal, 2023 - cambridge.org
Aerodynamic characterisation from flight testing is an integral subroutine for evaluating a
new flight vehicle's aerodynamic performance, stability and controllability. The estimation of …

Model-free control approach for fixed-wing UAVs with uncertain parameters analysis

JMO Barth, JP Condomines… - … on Methods & …, 2018 - ieeexplore.ieee.org
This paper presents first results of an innovative Model-Free Control (MFC) architecture
applied to fixed-wing UAVs. MFC is an algorithm dedicated to systems with poor modeling …

System identification of cropped delta UAVs from flight test methods using particle Swarm-Optimisation-based estimation

N Kumar, S Saderla, Y Kim - The Aeronautical Journal, 2023 - cambridge.org
In the era of Unmanned Aerial Systems (UAS), an onboard autopilot occupies a prominent
place and is inevitable for many of their modern applications. The efficacy of autopilot …

Model-Free Control of the PVTOL

ET García, AC Luna, DL Alabazares… - 2024 International …, 2024 - ieeexplore.ieee.org
This paper present the implementation of the Model Free Control (MFC) to stabilize
interconnected multi-SISO subsystems, such a the case of the Planar Vertical Take Off and …

[PDF][PDF] Heuristic procedure for optimal structural design of a subsonic aircraft wingbox

N Kanchev - Aeronautical, 2022 - journal_aeronautical.af-acad.bg
The wingbox optimal design is characterized by the intrinsic non-linearity and large scale of
the optimization procedures, as well as the inevitable presence of multiple imposed …

Investigation of Linear Quadratic Control and Guidance System Design for a small UAV

TD Chollom - 2019 - figshare.le.ac.uk
Autonomous air vehicles that are effcient and robust require reliable control systems that
enable them fly a mission. Modern ight controllers such as the linear quadratic regulators …

[PDF][PDF] Fault-tolerant Control of an Unmanned Aerial Vehicle Using Optimised Neural Network

TB Tshabalala - 2018 - wiredspace.wits.ac.za
Abstract An intelligent Fault-Tolerant Control (FTC) system for an Unmanned Aerial Vehicle
(UAV) was developed to be capable of tolerating a number of different control actuator faults …