Aircraft Engineering and Aerospace Technology: Volume 90 Issue 5
Strapline:
An International JournalTable of contents
Properties of direct-quenched aircraft forged component made of ultrahigh-strength steel 300M
Piotr Skubisz, Jan SinczakThis paper aims to investigate the possibilities and determination of hot and warm forging of ultrahigh-strength steel 300M and subsequent quenching with accelerated air. Analysis…
Fatigue life prediction of ceramic-matrix composites
Longbiao LiThis paper aims to predict fatigue life and fatigue limit of fiber-reinforced ceramic-matrix composites (CMCs) with different fiber preforms, i.e. unidirectional, cross-ply, 2D-…
Trajectory optimization of a multi-tethered space robot on large spinning net structures
Phongsatorn Saisutjarit, Takaya InamoriThe purpose of this paper is to investigate the time optimal trajectory of the multi-tethered robot (MTR) on a large spinning net structures in microgravity environment.
Spacecraft localization by indirect linear measurements from a single antenna
Chingiz Hajiyev, Ahmet SofyaliThe purpose of this paper is to present a two-stage approach for estimation of spacecraft’s position and velocity by indirect linear measurements from a single antenna.
Optimal wingtip device design for transport airplane
Bento Silva de Mattos, Paulo Jiniche Komatsu, Jesuíno Takachi TomitaThe present work aims to analyze the feasibility of wingtip device incorporation into transport airplane configurations considering many aspects such as performance, cost and…
Aircraft neural modeling and parameter estimation using neural partial differentiation
Majeed Mohamed, Vikalp DongareThe purpose of this paper is to build a neural model of an aircraft from flight data and online estimation of the aerodynamic derivatives from established neural model.
Performance monitoring and analysis of various parameters for a small UAV turbojet engine
Emre Kiyak, Gulay Unal, Nilgun Fazilet OzerThis paper aims to discuss engine health monitoring for unmanned aerial vehicles. It is intended to make consistent predictions about the future status of the engine performance…
Design of the composite casing of microstrip antenna for the aerospace satellite
Artur Lach, Andrzej Katunin, Adam GnatowskiThe paper aims to present a design and numerical verification procedure of a composite casing of a microstrip antenna for an aerospace satellite.
Trajectory planning for mini unmanned helicopter in obstacle and windy environments
Jinwu Xiang, Tong Shen, Daochun LiObstacle and wind field are common environmental factors for mini unmanned helicopter (MUH) flight. This paper aims to develop a trajectory planning approach guiding MUH to avoid…
Modelling and hovering control for a coaxial unmanned helicopter using sliding mode
Zhi Chen, Daobo Wang, Ziyang ZhenTo facilitate the nonlinear controller design, dynamic model of a novel coaxial unmanned helicopter (UH) is established and its coupling analysis is presented.
A method to analyze and optimize hybrid electric architectures applied to unmanned aerial vehicles
Teresa Donateo, Antonio Ficarella, Luigi SpedicatoThis paper addressed some critical issues in the development of hybrid electric powertrains for aircraft and propose a design methodology based on multi-objective optimization…
Vision-based relative navigation using cubature Huber-based filtering
Cheng Chen, Xiaogang Wang, Wutao Qin, Naigang CuiA novel vision-based relative navigation system (VBRNS) plays an important role in aeronautics and astronautics fields, and the filter is the core of VBRNS. However, most of the…
Digitalization of aircraft performance nomograms
Petar D. Mirosavljević, Đorđe I. Pantović, Radomir M. MijailovićThe purpose of this paper is to develop a new tool for aircraft performance analysis and optimization.
Autopilot design for an aircraft by using Luenberger observer design
Muhammad Taimoor, Li Aijun, Rooh ul Amin, Hongshi LuThe purpose of this paper is to design linear quadratic regulator (LQR) based Luenberger observer for the estimation of unknown states of aircraft.
Simulation of dynamic stall using direct-forcing immersed boundary method at low Reynolds number
Nima Vaziri, Ming-Jyh Chern, Tzyy-Leng HorngThe purpose of this study is simulation of dynamic stall behavior around the Eppler 387 airfoil in the low Reynolds number flow with a direct-forcing immersed boundary (DFIB…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb