Wind tunnel performance tests of the propellers with different pitch for the electric propulsion system

Z Czyż, P Karpiński, K Skiba, M Wendeker - Sensors, 2021 - mdpi.com
The geometry of a propeller is closely related to its aerodynamic performance. One of the
geometric parameters of a propeller is pitch. This parameter determines the distance by …

Design of the system for measuring uav parameters

J Novotňák, M Fiľko, P Lipovský, M Šmelko - Drones, 2022 - mdpi.com
This article deals with the design and creation of a tensometric measuring system to
measure the parameters of an unmanned aerial vehicle (UAV) of the quadcopter type. The …

Experimental measurement of a UAV propeller's thrust

M Kišev, L Vacho, L Tóth, M Olejár, M Harničárová… - Tehnički …, 2022 - hrcak.srce.hr
Sažetak At present, there are several types of propellers in the field of the use of Unmanned
Aerial Vehicles (UAVs) with unknown parameters, where it is necessary to provide …

Numerical investigation and performance comparison of UAV propeller with varying duct configuration

G Gowtham - Aircraft Engineering and Aerospace Technology, 2024 - emerald.com
Purpose The purpose of this study is to investigate the effects of propeller thrust with two
different duct configurations. Propellers in a quadcopter play an indispensable role in …

Control robusto H-infinito para la velocidad de desplazamiento de un UAV en base a estimación de flujo óptico

AS Ghersin, JI Giribet, J Luiso… - … de Automática e …, 2021 - polipapers.upv.es
Se presenta el diseño del control para la velocidad de desplazamiento de un vehículo
aéreo de seis rotores. La técnica de diseño utilizada es el control óptimo en H–infinito con el …

Analisis Gaya Dorong (Thrust) Propeller Pada Pesawat Model Remote Control (Uav)

JCR Sihaan, A Munawir, Z Husin - Jurnal Mekanova: Mekanikal …, 2022 - jurnal.utu.ac.id
Pesawat tanpa awak atau yang dikenal dengan UAV (Unmanned Aerial Vehicle)
merupakan teknologi pesawat terbang yang dikendalikan dengan jarak jauh oleh operator …

Estimasi Gaya Dorong Dari Motor Brushless Dengan Variasi Propeller Untuk Pesawat Model X-UAV Mini Talon Dengan Menggunakan Pengukur Massa

ARR Awwal, M Arifin, E Yuniarti - Jurnal Teknologi …, 2020 - jurnal.ftkunsurya.com
One that affects aircraft performance is the thrust. The thrust is determined according to the
requirements of the aircraft itself. This study uses a thrust test stand that uses a mass gauge …

Identification of electric propulsion system for unmanned aerial vehicles

M Sulewski, L Ambroziak, M Kondratiuk… - AIP Conference …, 2018 - pubs.aip.org
This paper presents the identification process of the electric propulsion system for
Unmanned Aerial Vehicles. Prepared identification test rig was described in details. It allows …

[PDF][PDF] Bukti-bukti pendukung kegiatan bidang B pada Laporan Kerja Dosen

E Yuniarti - eprints.universitassuryadarma.ac.id
Pengujian Bird Strike dilakukan menggunakan alat SHPB (Split Hopkinson Pressure Bar)
yang menembakkan sabot (wadah burung). Pada ujung alat SHPB, sabot akan dihentikan …