UAV autonomous formation flight experiment with Virtual Leader control structure
Z Gosiewski, L Ambroziak - Solid State Phenomena, 2013 - Trans Tech Publ
The problem of autonomous formation flight control of UAVs (Unmanned Aerial Vehicles) is
presented in the paper. A decentralized control method of the autonomous formation flight …
presented in the paper. A decentralized control method of the autonomous formation flight …
Preliminary uav autopilot integration and in-flight testing
L Ambroziak, Z Gosiewski - Solid State Phenomena, 2013 - Trans Tech Publ
The paper presents integration process of commercial autopilot. The autopilot was
integrated with a fixed wing airframe. The main aim of this work was an experimental study …
integrated with a fixed wing airframe. The main aim of this work was an experimental study …
[PDF][PDF] Efficient Positioning of Two Long-Range Passenger Aircraft in Formation Flight
A Antczak, M Lasek, K Sibilski - Transactions on Aerospace Research, 2022 - sciendo.com
In today's world, each airline is forced to look for new savings opportunities. One of the
methods may be the use of formation flights in daily flight operations, which may allow a …
methods may be the use of formation flights in daily flight operations, which may allow a …
Quad-Tiltrotor–modelling and control
M Ciopcia, C Szczepański - Journal of Marine Engineering & …, 2017 - Taylor & Francis
Aircrafts with VTOL capabilities announced a new era in marine aviation. Their aerodrome
requirements, which are as low as for helicopters, make them excellent candidates for many …
requirements, which are as low as for helicopters, make them excellent candidates for many …
Optimization of wing parameters to achieve minimum weight at defined aerodynamic loads
S Kachel - Journal of theoretical and applied mechanics, 2013 - ptmts.org.pl
The paper presents the method suitable for optimization of parameters and applied to
design aircraft subassemblies on the example of a swept wing. It outlines the assumptions …
design aircraft subassemblies on the example of a swept wing. It outlines the assumptions …
Model samolotu MP-02 dla sterowania w locie autonomicznym
P Cieciński, J Pieniążek - Zeszyty Naukowe/Wyższa Szkoła …, 2015 - yadda.icm.edu.pl
W prezentowanym artykule opisano model ruchu samolotu ultralekkiego typu MP-02A
„Czajka”, będący częścią prac realizowanych w projekcie Latającego Obserwatora Terenu …
„Czajka”, będący częścią prac realizowanych w projekcie Latającego Obserwatora Terenu …
3d attitude estimation in indoor environments with a complementary filter for the special orthogonal group so (3)
M Kmiecik, K Sibilski - Solid State Phenomena, 2013 - Trans Tech Publ
This paper presents a practical implementation of a complementary filter for 3D attitude
estimation in an indoor setting. The structure of the filter is chosen basing on design …
estimation in an indoor setting. The structure of the filter is chosen basing on design …
Identyfikacja charakterystyk aerodynamicznych mikrosamolotu
L Ambroziak, Z Gosiewski… - Prace Instytutu Lotnictwa, 2011 - yadda.icm.edu.pl
W artykule zaprezentowano proces obliczeniowy charakterystyk aerodynamicznych
bezzałogowego aparatu latającego. Jako obiekt badań wybrany został mikro-samolot typu …
bezzałogowego aparatu latającego. Jako obiekt badań wybrany został mikro-samolot typu …
[PDF][PDF] Effect of the Man-Weapon System on the Trajectory of a Projectile Fired from a Machine Pistol
Z Dziopa, K Zdeb - Problemy Mechatroniki: uzbrojenie, lotnictwo …, 2017 - bibliotekanauki.pl
The process of burst-firing two projectiles from a Skorpion vz. 61 7.65 mm calibre machine
pistol was recorded during a test at a firing range operated by the Polish Police. This …
pistol was recorded during a test at a firing range operated by the Polish Police. This …
[PDF][PDF] Analiza trwałości zmęczeniowej połączenia skrzydło-centropłat samolotu myśliwskiego
S Kachel, A Kozakiewicz, T Łącki - Biuletyn Wojskowej Akademii …, 2011 - bibliotekanauki.pl
Praca przedstawia wyniki analiz numerycznych modelu węzła siłowego układu skrzydło-
centropłat samolotu MiG-29. Do celów obliczeń zbudowano model numeryczny wybranych …
centropłat samolotu MiG-29. Do celów obliczeń zbudowano model numeryczny wybranych …