11   Artículos

 
en línea
Jianjian Liang, Shoukun Wang and Bo Wang    
This paper proposes the creative idea that an unmanned fixed-wing aircraft should automatically adjust its 3D landing trajectory online to land on a given touchdown point, instead of following a pre-designed fixed glide slope angle or a landing path comp... ver más
Revista: Drones    Formato: Electrónico

 
en línea
Soram Oh, Ju-Hyo Park, Hyun-Jung Kim, Hye-Jeong Kim, Eurok Shim, Jee-Yeon Woo, Hiran Perinpanayagam, Kyung-Kyu Choi and Seok Woo Chang    
This study aimed to evaluate the effects of flexural stress on the torsional fracture resistance of NiTi glide path files. PathFile #16/02, RaCe #15/04, RaCe Evo #15/04, HyFlex EDM #15/03, TruNatomy Glider #17/02, and V Taper 2H #17/04 were examined by s... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Yudong Hu, Changsheng Gao and Wuxing Jing    
Aimed at joint state and parameter estimation problems in hypersonic glide vehicle defense, a novel moving horizon estimation algorithm via Carleman linearization is developed in this paper. First, the maneuver characteristic parameters that reflect the ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shijun Zhao and Yulong Shan    
Low-level wind shear is a vital weather process affecting aircraft safety while taking off and landing and is known as the ?aircraft killer? in the aviation industry. As a result, effective monitoring and warning are required. Several ramps detection alg... ver más
Revista: Algorithms    Formato: Electrónico

 
en línea
Bartlomiej Brukarczyk, Dariusz Nowak, Piotr Kot, Tomasz Rogalski and Pawel Rzucidlo    
The paper presents automatic control of an aircraft in the longitudinal channel during automatic landing. There are two crucial components of the system presented in the paper: a vision system and an automatic landing system. The vision system processes ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Andrej Novák, Karel Havel, Michal Janovec     Pág. 117 - 126
This paper deals with the flight measuring and testing of the Instrument Landing System (ILS) by flying laboratory aircraft ? AeroLab 1 at the University of ?ilina. The paper focusses on the comparative aerial measurements of the ILS which is installed a... ver más
Revista: Transportation Research Procedia    Formato: Electrónico

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