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61 Results Found

  • Review
  • Open Access
39 Citations
23,988 Views
25 Pages

3 September 2022

Flight testing in a realistic three-dimensional virtual environment is increasingly being considered a safe and cost-effective way of evaluating aircraft models and their control systems. The paper starts by reviewing and comparing the most popular p...

  • Article
  • Open Access
12 Citations
7,126 Views
25 Pages

18 October 2022

Aircraft flight simulators have good cost efficiency, high reusability, and high flight safety. All airlines and aircraft manufacturing companies choose it as sophisticated training equipment for ground simulation, effectively reducing pilot training...

  • Article
  • Open Access
283 Views
26 Pages

7 February 2026

Terminal flight phases, particularly landing, are among the most critical, due to low altitude, low speed and the possible presence of crosswinds. Tools capable of accurately modeling and simulating these phases are essential for identifying potentia...

  • Article
  • Open Access
2 Citations
1,951 Views
17 Pages

Development of an Unmanned Glider for Temperature and Image Monitoring

  • Joel Eldo,
  • Sivasankar Sibi,
  • Zehin A. Ibrahim and
  • Efstratios L. Ntantis

7 July 2025

This paper presents the design, fabrication, simulation, and partial validation of a low-cost, fixed-wing unmanned glider equipped for temperature and image monitoring. Aerodynamic optimization was performed using XFLR5 and ANSYS Fluent 2023 R1, with...

  • Article
  • Open Access
3 Citations
4,040 Views
29 Pages

Research and Performance Optimization of Jump-Takeoff in Autogyros

  • Yukun Wang,
  • Lingxi Guo,
  • Zhiming Guo,
  • Liaoni Wu,
  • Fuqiang Bing,
  • Quanwen Hu and
  • Zonghua Sun

The main focus of this article is on the jump-takeoff method for autogyros. On the basis of a high-confidence autogyro model, we design a jump-takeoff simulation experiment to study and optimize jump-takeoff performance. Using a simplified version of...

  • Article
  • Open Access
11 Citations
5,086 Views
25 Pages

Development and Evaluation of an Enhanced Virtual Reality Flight Simulation Tool for Airships

  • Mohsen Rostami,
  • Jafer Kamoonpuri,
  • Pratik Pradhan and
  • Joon Chung

A real-time flight simulation tool is proposed using a virtual reality head-mounted display (VR-HMD) for remotely piloted airships operating in beyond-line-of-sight (BLOS) conditions. In particular, the VR-HMD was developed for stratospheric airships...

  • Review
  • Open Access
18 Citations
10,635 Views
22 Pages

10 September 2021

This paper deals with safety-critical, high-power actuation in aerospace applications. Using a system-level synthetic view, it identifies, explains and discusses the reasons why electrically supplied, or power-by-wire, solutions have not spread rapid...

  • Article
  • Open Access
13 Citations
4,612 Views
25 Pages

17 December 2020

The paper presents a methodology enabling the detection of aircraft touchdowns based on data obtained from accelerometers attached to the structural parts of the airframe in the cockpit or passenger compartment. Precise determination of the moment an...

  • Article
  • Open Access
449 Views
21 Pages

Adaptive Nonlinear Dynamic Inversion with Ground Taxiing Dynamics for Trajectory Tracking and Safe Autonomous Take-Off/Landing of Fixed-Wing UAVs

  • Yingdong Xia,
  • Mingying Huo,
  • Xiyan Zhao,
  • Lehan Wang,
  • Jianfeng Wang,
  • Yuxuan Yao,
  • Guiqi Pan,
  • Cheng Wang and
  • Ze Yu

7 January 2026

The design of control systems for aircraft autonomous takeoff and landing, as well as full-flight-envelope operations—including taxiing, takeoff, climb, cruise, descent, and landing—presents significant challenges. These challenges arise...

  • Article
  • Open Access
18 Citations
3,649 Views
20 Pages

Application of Operational Load Monitoring System for Fatigue Estimation of Main Landing Gear Attachment Frame of an Aircraft

  • Michal Dziendzikowski,
  • Artur Kurnyta,
  • Piotr Reymer,
  • Marcin Kurdelski,
  • Sylwester Klysz,
  • Andrzej Leski and
  • Krzysztof Dragan

1 November 2021

In this paper, we present an approach to fatigue estimation of a Main Landing Gear (MLG) attachment frame due to vertical landing forces based on Operational Loads Monitoring (OLM) system records. In particular, the impact of different phases of land...

  • Article
  • Open Access
3 Citations
2,043 Views
12 Pages

The angular motion of aircraft landing gear retraction and extension must be accurate to ensure flight safety. Therefore, this study experimentally evaluated the motion accuracy of the landing gear retraction and extension processes associated with a...

  • Article
  • Open Access
5 Citations
2,512 Views
24 Pages

A Self-Attention Integrated Learning Model for Landing Gear Performance Prediction

  • Lin Lin,
  • Changsheng Tong,
  • Feng Guo,
  • Song Fu,
  • Yancheng Lv and
  • Wenhui He

7 July 2023

The landing gear structure suffers from large loads during aircraft takeoff and landing, and an accurate prediction of landing gear performance is beneficial to ensure flight safety. Nevertheless, the landing gear performance prediction method based...

  • Article
  • Open Access
2 Citations
1,718 Views
16 Pages

Fiber Bragg Grating Bonding Characterization under Long-Period Cyclic Loading

  • Angela Brindisi,
  • Cristian Vendittozzi,
  • Costanzo Bellini,
  • Vittorio Di Cocco,
  • Lidia Travascio,
  • Luigi Di Palma,
  • Marika Belardo and
  • Antonio Concilio

The Smart Landing Gear system to be developed in the framework of the ANGELA project provides the strain measurements on landing gear structure at landings, and this system should be maintained efficiently under operational conditions. It is intended...

  • Article
  • Open Access
6 Citations
3,352 Views
12 Pages

Optimization of Ski Attitude for the In-Flight Aerodynamic Performance of Ski Jumping

  • Lianzhong Cao,
  • Youcai Guo,
  • Xiong Li,
  • Long Chen,
  • Xin Wang and
  • Tianyu Zhao

17 September 2022

The control and adjustment of in-flight attitudes are critical to enlarging the flight distance of ski jumping. As one of the most important gears, the skis provide sufficient lift and drag forces for the athletes, and thus their in-flight attitudes...

  • Article
  • Open Access
32 Citations
15,174 Views
16 Pages

Predicting the Remaining Useful Life of Landing Gear with Prognostics and Health Management (PHM)

  • Tzu-Hsuan Hsu,
  • Yuan-Jen Chang,
  • He-Kai Hsu,
  • Tsung-Ti Chen and
  • Po-Wen Hwang

20 August 2022

Landing gear is an essential part of an aircraft. However, the components of landing gear are susceptible to degradation over the life of their operation, which can result in the shimmy effect occurring during take-off and landing. In order to reduce...

  • Article
  • Open Access
1 Citations
1,032 Views
24 Pages

15 October 2025

Predicting the Remaining Useful Life (RUL) of light aircraft landing gear is complicated by flight-to-flight variability in operational loads, particularly in sensor-free fleets that rely only on mass-and-balance records. This study develops a hybrid...

  • Article
  • Open Access
23 Citations
5,512 Views
21 Pages

7 August 2020

Vertical take-off and landing unmanned aerial vehicles (VTOL UAV) are widely used in various fields because of their stable flight, easy operation, and low requirements for take-off and landing environments. To further expand the UAV’s take-off...

  • Article
  • Open Access
120 Views
29 Pages

The safety-critical nature of aircraft landing gear has led to interest in Structural Health Monitoring (SHM) and Remaining Useful Life (RUL) methodologies for the fatigue substantiation of landing gear assemblies. Due to the engineering effort that...

  • Article
  • Open Access
4 Citations
9,554 Views
19 Pages

Selection Methodology of an Electric Actuator for Nose Landing Gear of a Light Weight Aircraft

  • Taimur Ali Shams,
  • Syed Irtiza Ali Shah,
  • Muhammad Ayaz Ahmad,
  • Kashif Mehmood,
  • Waseem Ahmad and
  • Syed Tauqeer ul Islam Rizvi

6 December 2020

Landing gear system of an aircraft enables it to take off and land with safety and comfort. Because of the horizontal and vertical velocity of aircraft, upon landing, the complete aircraft undergoes different forcing functions in the form of the impa...

  • Article
  • Open Access
2 Citations
1,817 Views
20 Pages

22 January 2025

In this paper, a method for planning the perching trajectory of a fixed-wing unmanned aerial vehicle (UAV) based on the estimation of the region of attraction (ROA) is proposed, to expand the feasible domain of a UAV in the presence of aerodynamic pe...

  • Feature Paper
  • Article
  • Open Access
3 Citations
1,145 Views
16 Pages

Transmitting Double-D Coil to Wirelessly Recharge the Battery of a Drone with a Receiving Coil Integrated in the Landing Gear

  • Wassim Boumerdassi,
  • Tommaso Campi,
  • Silvano Cruciani,
  • Francesca Maradei and
  • Mauro Feliziani

16 May 2025

The aim of this work is the design of a 200 W transmitting coil for a high-power wireless power transfer (WPT) system based on magnetic resonant coupling (MRC) to charge the battery of a drone in 1 h equipped with a WPT receiving coil integrated into...

  • Technical Note
  • Open Access
16 Citations
5,904 Views
15 Pages

A Note on the Electromechanical Design of a Robotic Hummingbird

  • André Preumont,
  • Han Wang,
  • Shengzheng Kang,
  • Kainan Wang and
  • Ali Roshanbin

7 March 2021

This paper analyzes the lift-production system in hovering of the flapping wing robot COLIBRI of the size of a hummingbird. The paper first examines the flapping wing mechanism for which a new gear transmission is proposed to reduce the friction and...

  • Article
  • Open Access
4 Citations
3,177 Views
20 Pages

The Optimization of a Model for Predicting the Remaining Useful Life and Fault Diagnosis of Landing Gear

  • Yuan-Jen Chang,
  • He-Kai Hsu,
  • Tzu-Hsuan Hsu,
  • Tsung-Ti Chen and
  • Po-Wen Hwang

15 November 2023

With the development of next-generation airplanes, the complexity of equipment has increased rapidly, and traditional maintenance solutions have become cost-intensive and time-consuming. Therefore, the main objective of this study is to adopt predict...

  • Article
  • Open Access
9 Citations
6,151 Views
13 Pages

Preliminary Assessment of an FBG-Based Landing Gear Weight on Wheel System

  • Angela Brindisi,
  • Cristian Vendittozzi,
  • Lidia Travascio,
  • Luigi Di Palma,
  • Marika Belardo,
  • Michele Ignarra,
  • Vincenzo Fiorillo and
  • Antonio Concilio

14 July 2022

Weight-on-Wheels (WoW) systems are aimed at indicating if the aircraft weight is loading onto the landing gear and its wheels, even partially. These systems are an integral part of the actuation system for safety-critical applications and shall provi...

  • Article
  • Open Access
7 Citations
2,409 Views
19 Pages

8 June 2023

Frequent aviation safety accidents of civil aircraft misses and crashes lead to an urgent need for flight safety assurance. Due to long-time flights over different backgrounds, accompanied by the changes in flight altitude and speed, it is difficult...

  • Article
  • Open Access
5 Citations
6,288 Views
10 Pages

Thermal Performance Evaluation in Gas Turbine Aero Engines Accessory Gearbox

  • Soheil Jafari,
  • Ahmed Bouchareb and
  • Theoklis Nikolaidis

This paper presents a methodological approach for mathematical modelling and physics-based analysis of accessory gearbox (AGB) thermal behavior in gas turbine aero engines. The AGB structure, as one of the main sources of heat in gas turbine aero eng...

  • Article
  • Open Access
6 Citations
10,448 Views
22 Pages

Development of a Morphing Landing Gear Composite Door for High Speed Compound Rotorcraft

  • Antonio Chiariello,
  • Salvatore Orlando,
  • Pasquale Vitale,
  • Mauro Linari,
  • Raffaele Longobardi and
  • Luigi Di Palma

In the framework of fast rotorcraft, smoothness and flushness of external aerodynamic surfaces present challenges for high-speed conditions, where aerodynamics is the driver of helicopter performance. For AIRBUS-RACER helicopter the main landing gear...

  • Article
  • Open Access
4 Citations
4,956 Views
18 Pages

29 November 2023

Catapult-assisted takeoff is the initiation of flight missions for carrier-based aircrafts. Ensuring the safety of aircrafts during catapult-assisted takeoff requires a thorough analysis of their motion characteristics. In this paper, a rigid–f...

  • Article
  • Open Access
5 Citations
2,902 Views
26 Pages

10 April 2023

TC18 titanium alloy is an essential material for aircraft landing gear. To reveal the wear and corrosion mechanisms of landing gear in service, a WC-12Co coating on a TC18 substrate was prepared by High-Velocity Air-Fuel (HVAF) spraying based on opti...

  • Article
  • Open Access
2 Citations
3,807 Views
26 Pages

Optimization of Airplane Landing in Crosswind Conditions for Minimum Tire Wear

  • Stefano Cacciola,
  • Carlo E. D. Riboldi and
  • Edoardo Generali

Being one of the most critical phases of a flight, landing deserves specific attention, especially when the aircraft is subject to external disturbances such as wind. A notable concern associated with touchdown events, especially when crosswind is pr...

  • Article
  • Open Access
591 Views
18 Pages

24 September 2025

The JAYA algorithm has been widely applied due to its simplicity and efficiency but is prone to entrapment in sub-optimal solutions. This study introduces the Lévy flight mechanism and proposes the CLJAYA-LF algorithm, which integrates large-s...

  • Article
  • Open Access
14 Citations
5,317 Views
23 Pages

Smooth 3D Path Planning by Means of Multiobjective Optimization for Fixed-Wing UAVs

  • Franklin Samaniego,
  • Javier Sanchis,
  • Sergio Garcia-Nieto and
  • Raul Simarro

Demand for 3D planning and guidance algorithms is increasing due, in part, to the increase in unmanned vehicle-based applications. Traditionally, two-dimensional (2D) trajectory planning algorithms address the problem by using the approach of maintai...

  • Article
  • Open Access
1 Citations
2,944 Views
10 Pages

10 November 2023

Causes and contributing factors of amphibious airplane accidents are examined by comparing the proportion of fatal accidents for different causes of accidents, with a focus on landings on water and low-level flying maneuvers. A set of 183 accidents i...

  • Article
  • Open Access
180 Views
23 Pages

High-performance geared turbofan engines generate significant heat within the planetary power gearbox. This study presents the thermal design of an integrated fan guide vane heat exchanger aimed at recovering gearbox heat losses with minimal pressure...

  • Article
  • Open Access
9 Citations
3,579 Views
25 Pages

Research on the Effect Characteristics of Free-Tail Layout Parameters on Tail-Sitter VTOL UAVs

  • Hao Qi,
  • Shi-Jie Cao,
  • Jia-Yue Wu,
  • Yi-Ming Peng,
  • Hong Nie and
  • Xiao-Hui Wei

The tail-sitter VTOL UAV boasts not only high-speed cruising and air hovering capabilities, but also its unique tail-sitting vertical takeoff and landing and hovering attitude enable aerial operations with an exceptionally small cross-sectional area....

  • Article
  • Open Access
1 Citations
1,514 Views
20 Pages

Multi-Agent Reinforcement Symbolic Regression for the Fatigue Life Prediction of Aircraft Landing Gear

  • Yi-Pin Sun,
  • Haozhe Feng,
  • Baiyang Zheng,
  • Jiong-Ran Wen,
  • Ai-Fang Chao and
  • Cheng-Wei Fei

12 August 2025

Accurate fatigue life prediction of aircraft landing gear is crucial for ensuring flight safety and preventing catastrophic structural failures. However, traditional empirical methods face significant limitations in capturing complex multiaxial loadi...

  • Article
  • Open Access
10 Citations
5,971 Views
16 Pages

1 September 2019

The emergence extension system (a mechanical system) of nose landing gear (NLG) seriously influences the reliability, safety and airworthiness of civil aircrafts. To efficiently realize the NLG emergence extension, a promising driving plan of emergen...

  • Article
  • Open Access
1,444 Views
30 Pages

14 August 2025

This paper deals with the design and the robustness analysis of a model predictive control (MPC) for the position tracking of primary flight movables driven by electro-mechanical actuators. This study is, in particular, focused on a rotary electro-me...

  • Article
  • Open Access
452 Views
23 Pages

Automatic Grasping System and Hybrid Controller Towards Multi-Drone Parcel Delivery

  • Bruno J. Guerreiro,
  • Francisco Azevedo,
  • Paulo Oliveira and
  • Rita Cunha

18 January 2026

This paper presents the development of an autonomous grasping mechanism for drone-based parcel delivery systems towards developing capabilities for in-flight package transfer. The approach integrates a mechanical gripper fitted with sensors and a pos...

  • Article
  • Open Access
2 Citations
3,280 Views
17 Pages

Growing concerns over the CO2 footprint due the exponential demand of the aviation industry, along with the requirements for high aerodynamic performance, cost saving, and manoeuvrability during different phases of a flight, pave the path towards ada...

  • Article
  • Open Access
8 Citations
4,229 Views
20 Pages

Design and Aerodynamic Analysis of a Flapping Mechanism for Foldable Biomimetic Aircraft

  • Shuai Yan,
  • Yongjun Zhou,
  • Shuxia Jiang,
  • Hao Xue and
  • Pengcheng Guo

This study investigates the unsteady aerodynamic mechanisms underlying the efficient flight of birds and proposes a biomimetic flapping-wing aircraft design utilizing a double-crank double-rocker mechanism. Building upon a detailed analysis of avian...

  • Review
  • Open Access
1 Citations
307 Views
41 Pages

31 January 2026

An accurate prediction of aircraft wheel and brake (W&B) temperatures is increasingly important for ensuring landing gear safety, supporting turnaround decision-making, and allowing for more effective condition monitoring. Although the thermal be...

  • Article
  • Open Access
6 Citations
8,220 Views
17 Pages

Launch Bar Dynamics Character Analysis of Carrier-Based Aircraft Catapult Launch

  • Qidan Zhu,
  • Peng Lu,
  • Zhibo Yang,
  • Xun Ji,
  • Yu Han and
  • Lipeng Wang

30 July 2019

The launch bar is a unique device of carrier-based aircraft, which is connected to the nose gear and shuttle. In order to avoid the launch bar striking the flight deck after the launch bar pops out of the shuttle, it is very important to research the...

  • Article
  • Open Access
7 Citations
2,901 Views
22 Pages

Optimal Processing Parameters of Transmission Parts of a Flapping-Wing Micro-Aerial Vehicle Using Precision Injection Molding

  • Huei-Yu Huang,
  • Fang-Yu Fan,
  • Wei-Chun Lin,
  • Chiung-Fang Huang,
  • Yung-Kang Shen,
  • Yi Lin and
  • Muhammad Ruslin

4 April 2022

In this study, we designed and fabricated transmission parts for a flapping-wing micro-aerial vehicle (FW-MAV), which was fabricated by precision injection molding, and analyzed its warpage phenomena. First, a numerical simulation (Moldflow) was used...

  • Article
  • Open Access
9 Citations
4,903 Views
15 Pages

Helicopter Inside Cabin Acoustic Evaluation: A Case Study—IAR PUMA 330

  • Marius Deaconu,
  • Grigore Cican,
  • Adina-Cristina Toma and
  • Luminița Ioana Drăgășanu

This paper presents an inside-cabin acoustic evaluation of the IAR PUMA 330 helicopter, manufactured by IAR S.A. Brasov. In this study, based on the acoustic assessment inside the helicopter, areas with high noise levels are identified. In this regar...

  • Article
  • Open Access
3 Citations
4,674 Views
42 Pages

Design and Validation of a New Tilting Rotor VTOL Drone: Structural Optimization, Flight Dynamics, and PID Control

  • Haixia Gong,
  • Wei He,
  • Shuping Hou,
  • Ming Chen,
  • Ziang Yang,
  • Qin Si and
  • Deming Zhao

4 June 2025

This study addresses the gap in the experimental validation of the tilt-rotor vertical take-off and landing (VTOL) UAVs by developing a novel prototype that integrates fixed-wing and multi-rotor advantages. A dynamic model based on the “X&rdquo...

  • Article
  • Open Access
33 Citations
39,887 Views
44 Pages

13 May 2015

In this paper, an ornithopter prototype that mimics the flapping motion of bird flight is developed, and the lift and thrust generation characteristics of different wing designs are evaluated. This project focused on the spar arrangement and material...

  • Article
  • Open Access
15 Citations
7,462 Views
19 Pages

Vibration Response Aspects of a Main Landing Gear Composite Door Designed for High-Speed Rotorcraft

  • Maurizio Arena,
  • Antonio Chiariello,
  • Martina Castaldo and
  • Luigi Di Palma

19 February 2021

One of the crucial issues affecting the structural safety of propeller vehicles is the propeller tonal excitation and related vibrations. Propeller rotation during flight generates vibrating sources depending upon its rotational angular velocity, num...

  • Article
  • Open Access
8 Citations
3,640 Views
20 Pages

Multi-UAV Data Collection and Path Planning Method for Large-Scale Terminal Access

  • Linfeng Zhang,
  • Chuhong He,
  • Yifeng Peng,
  • Zhan Liu and
  • Xiaorong Zhu

20 October 2023

In the context of the relentless evolution of network and communication technologies, the need for enhanced communication content and quality continues to escalate. Addressing the demands of data collection from the abundance of terminals within Inte...

  • Review
  • Open Access
27 Citations
8,493 Views
26 Pages

This paper reviews applications of gas chromatography-mass spectrometry techniques for the characterization of photooxidation and autoxidation products of lipids of senescent phototrophic organisms. Particular attention is given to: (i) the selection...

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