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Quaternion-Based Attitude Estimation of an Aircraft Model Using Computer Vision

Sensors (Basel, Switzerland), 2024-06, Vol.24 (12), p.3795

2024

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Wind Preview-Based Model Predictive Control of Multi-Rotor UAVs Using LiDAR

Sensors (Basel, Switzerland), 2023-04, Vol.23 (7), p.3711

2023

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Multirotor Sizing Methodology with Flight Time Estimation

Journal of advanced transportation, 2020, Vol.2020 (2020), p.1-14

2020

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High-Input-Voltage High-Frequency Class E Rectifiers for Resonant Inductive Links

IEEE transactions on power electronics, 2015-03, Vol.30 (3), p.1328-1335

2015

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Road vehicle state estimation using low-cost GPS/INS

Mechanical systems and signal processing, 2011-08, Vol.25 (6), p.1988-2004

2011

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Application of an Efficient Gradient-Based Optimization Strategy for Aircraft Wing Structures

Aerospace, 2018-03, Vol.5 (1), p.3

2018

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An Advanced Unmanned Aerial Vehicle (UAV) Approach via Learning-Based Control for Overhead Power Line Monitoring: A Comprehensive Review

IEEE access, 2021, Vol.9, p.130410-130433

2021

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Development of Aerodynamic and Propulsion Models Using the Iterative Equation Error Method

Aerospace, 2024-01, Vol.11 (1), p.8

2024

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Mixed Uncertainty Analysis of Pole Placement and H∞ Controllers for Directional Drilling Attitude Tracking

Journal of dynamic systems, measurement, and control, 2015-12, Vol.137 (12)

2015

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Effect of Rotor Tilt on the Gust Rejection Properties of Multirotor Aircraft

Drones (Basel), 2022-10, Vol.6 (10), p.305

2022

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Gain-Scheduled H∞ Control for Tensor Product Type Polytopic Plants

Asian journal of control, 2015-03, Vol.17 (2), p.417-431

2015

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Ground Vibration Testing of a Flexible Wing: A Benchmark and Case Study

Aerospace, 2022-08, Vol.9 (8), p.438

2022

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The Accuracy and Computational Efficiency of the Loewner Framework for the System Identification of Mechanical Systems

Aerospace, 2023-06, Vol.10 (6), p.571

2023

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Disturbance Observer Enhanced Neural Network LPV Control for a Blended-Wing-Body Large Aircraft

IEEE transactions on aerospace and electronic systems, 2021-10, Vol.57 (5), p.2689-2703

2021

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Adaptive Backstepping Nonsingular Terminal Sliding-Mode Attitude Control of Flexible Airships with Actuator Faults

Aerospace, 2022-04, Vol.9 (4), p.209

2022

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Electronic Tuning of Misaligned Coils in Wireless Power Transfer Systems

IEEE transactions on power electronics, 2014-11, Vol.29 (11), p.5975-5982

2014

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Modelling and control of the roll-stabilised control unit of a rotary steerable system directional drilling tool

Journal of engineering (Stevenage, England), 2019-06, Vol.2019 (17), p.4555-4559

2019

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Tuning Class E Inverters Applied in Inductive Links Using Saturable Reactors

IEEE transactions on power electronics, 2014-06, Vol.29 (6), p.2969-2978

2014

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Direct Method Based Control System for an Autonomous Quadrotor

Journal of intelligent & robotic systems, 2010-11, Vol.60 (2), p.285-316

2010

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Wireless Power Transfer Using Class E Inverter With Saturable DC-Feed Inductor

IEEE transactions on industry applications, 2014-07, Vol.50 (4), p.2710-2718

2014

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Development of Gas-Liquid Flow Regimes Identification Using a Noninvasive Ultrasonic Sensor, Belt-Shape Features, and Convolutional Neural Network in an S-Shaped Riser

IEEE transactions on cybernetics, 2023-01, Vol.53 (1), p.3-17

2023

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Neural network adaptive backstepping fault tolerant control for unmanned airships with multi-vectored thrusters

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2021-09, Vol.235 (11), p.1507-1520

2021

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Design and Implementation of an L1 Adaptive Proportional Output Feedback Controller

Actuators, 2024-05, Vol.13 (5), p.172

2024

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Adopting exergy analysis for use in aerospace

Progress in aerospace sciences, 2017-08, Vol.93, p.73-94

2017

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Active Stall Flutter Suppression for a Revised Leishman–Beddoes Model

Journal of aerospace engineering, 2024-01, Vol.37 (1)

2024

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Quaternion-Based Attitude Estimation of an Aircraft Model Using Computer Vision

Wind Preview-Based Model Predictive Control of Multi-Rotor UAVs Using LiDAR

Multirotor Sizing Methodology with Flight Time Estimation

High-Input-Voltage High-Frequency Class E Rectifiers for Resonant Inductive Links

Road vehicle state estimation using low-cost GPS/INS

Application of an Efficient Gradient-Based Optimization Strategy for Aircraft Wing Structures

An Advanced Unmanned Aerial Vehicle (UAV) Approach via Learning-Based Control for Overhead Power Line Monitoring: A Comprehensive Review

Development of Aerodynamic and Propulsion Models Using the Iterative Equation Error Method

Mixed Uncertainty Analysis of Pole Placement and H∞ Controllers for Directional Drilling Attitude Tracking

Effect of Rotor Tilt on the Gust Rejection Properties of Multirotor Aircraft

Gain-Scheduled H∞ Control for Tensor Product Type Polytopic Plants

Ground Vibration Testing of a Flexible Wing: A Benchmark and Case Study

The Accuracy and Computational Efficiency of the Loewner Framework for the System Identification of Mechanical Systems

Disturbance Observer Enhanced Neural Network LPV Control for a Blended-Wing-Body Large Aircraft

Adaptive Backstepping Nonsingular Terminal Sliding-Mode Attitude Control of Flexible Airships with Actuator Faults

Electronic Tuning of Misaligned Coils in Wireless Power Transfer Systems

Modelling and control of the roll-stabilised control unit of a rotary steerable system directional drilling tool

Tuning Class E Inverters Applied in Inductive Links Using Saturable Reactors

Direct Method Based Control System for an Autonomous Quadrotor

Wireless Power Transfer Using Class E Inverter With Saturable DC-Feed Inductor

Development of Gas-Liquid Flow Regimes Identification Using a Noninvasive Ultrasonic Sensor, Belt-Shape Features, and Convolutional Neural Network in an S-Shaped Riser

Neural network adaptive backstepping fault tolerant control for unmanned airships with multi-vectored thrusters

Design and Implementation of an L1 Adaptive Proportional Output Feedback Controller

Adopting exergy analysis for use in aerospace

Active Stall Flutter Suppression for a Revised Leishman–Beddoes Model

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