Aircraft Engineering and Aerospace Technology: Volume 94 Issue 3

Determination of fuel consumption and pollutant emissions with the real-time engine running data of aircrafts in the taxi-out period

Mehmet Kadri Akyüz

The purpose of this paper is to calculate the fuel consumption and emissions of carbon monoxide (CO), nitrogen oxide (NO_x) and hydrocarbons (HC) in the taxi-out period of aircraft…

Evaluation of design criteria for mini unmanned aircraft systems (UAS) applications

Ramesh P.S., Muruga Lal Jeyan J.V.

This paper aims to evaluate the factors that dictate the design of a mini unmanned aircraft system (UAS).

Aerodynamic coefficients modeling using Levenberg–Marquardt algorithm and network

Zhigang Wang, Aijun Li, Lihao Wang, Xiangchen Zhou, Boning Wu

The purpose of this paper is to propose a new aerodynamic parameter estimation methodology based on neural network and output error method, while the output error method is…

Systematic fuzzy Navier–Stokes equations for aerospace vehicles

ZY Chen, Yahui Meng, Ruei-Yuan Wang, Timothy Chen

To prove the effectiveness of the proposed design method, this study aims to propose the Fisher equation and temperature cooling fins that control high-speed aerospace vehicles.

Development of an aeroelastic model based on system identification using boundary elements method

Rohollah Dehghani Firouz-Abadi, Mohammad Reza Borhan Panah

The purpose of this paper is to analyze the stability of aeroelastic systems using a novel reduced order aeroelastic model.

Determining the pointer positions of aircraft analog indicators using deep learning

Erdem Tunca, Hasan Saribas, Hasim Kafali, Sinem Kahvecioglu

The purpose of this paper is to monitor the backup indicators in case of indicator failure and to minimize the situations when the pilot may be unable to monitor the indicator…

UAV generalized longitudinal model for autopilot controller designs

Eduard Bertran, Paula Tercero, Alex Sànchez-Cerdà

This paper aims to overcome the main obstacle to compare the merits of the different control strategies for fixed-wing unmanned aerial vehicles (UAVs) to assess autopilot…

Chemical potential variation effect of new design of graphene antenna for satellite applications

Mohammed Amin Rabah, Bekhti Mohammed

The present work aims to analyze the performance of a newly designed graphene-based patch antenna by varying the chemical potential in graphene sheet, using the CST Microwave…

Target group distribution pattern analysis with bagged convolutional neural networks for UAV distribution pattern identification

Xin Xu

The purpose of this study is to address the limitations of existing target group distribution pattern analysis methods and identify subtle distribution differences within and…

Adaptive neural-based finite-time attitude synchronization and tracking control of multiple rigid bodies under actuator faults and saturation

Amin Mihankhah, Ali Doustmohammadi

The purpose of this paper, is to solve the problem of finite-time fault-tolerant attitude synchronization and tracking control of multiple rigid bodies in presence of model…

Real-time tuning of PID controller based on optimization algorithms for a quadrotor

Muharrem Selim Can, Hamdi Ercan

This study aims to develop a quadrotor with a robust control system against weight variations. A Proportional-Integral-Derivative (PID) controller based on Particle Swarm…

Knowledge creation and application of optimal tolerance distribution method for aircraft product assembly

Md Helal Miah, Jianhua Zhang, Dharmahinder Singh Chand

This paper aims to illustrate the tolerance optimization method based on the assembly accuracy constrain, precession constrain and the cost of production of the assembly product.

On the state independency and log-linearity of error propagation for discrete group affine systems with application to attitude estimation

Jiaolong Wang, Chengxi Zhang, Jin Wu

This paper aims to propose a general and rigorous study on the propagation property of invariant errors for the model conversion of state estimation problems with discrete group…

Review on critical technology development of avian radar system

Weishi Chen, Yifeng Huang, Xianfeng Lu, Jie Zhang

This paper aims to review the critical technology development of avian radar system at airports.

An efficient decision support system for selecting very light business jet using CRITIC-TOPSIS method

Aishwarya Dhara, Gurpreet Kaur, Pon Maa Kishan, Arunava Majumder, Rakesh Yadav

This paper aims to assure the selection of the most suitable very light business aircraft which is preferred by the passengers based on effectiveness and aesthetic comfort. The…

A key design parameter proposal for aerodynamically efficient subsonic blended wing body

Seyhun Durmus

Blended wing body (BWB) is a very advantageous design in terms of low fuel consumption, low emission and low noise levels. Because of these advantages, the BWB is a candidate to…