Performance evaluation of RW-Quadrotor and Bi-Quadrotor for payload delivery
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61989100%3A27240%2F23%3A10253114" target="_blank" >RIV/61989100:27240/23:10253114 - isvavai.cz</a>
Výsledek na webu
<a href="https://ietresearch.onlinelibrary.wiley.com/doi/10.1049/itr2.12403" target="_blank" >https://ietresearch.onlinelibrary.wiley.com/doi/10.1049/itr2.12403</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1049/itr2.12403" target="_blank" >10.1049/itr2.12403</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Performance evaluation of RW-Quadrotor and Bi-Quadrotor for payload delivery
Popis výsledku v původním jazyce
Payload delivery is one of the many Unmanned Aerial Vehicle (UAV) applications that save time, energy, and human resources. The present simulation study compares rotary-wing quadrotors (RW-Quadrotors) and tail-sitter biplane quadrotors (Bi-Quadrotors) under payload delivery conditions that help to choose the best UAV for the particular mission. A comparative study is performed based on (i) time taken to accomplish the given mission, (ii) trajectory tracking performance, (iii) motor speed throughout the entire flight envelope, and (iv) remains SoC (State of Charge) after the mission. Furthermore, a Backstepping Controller (BSC) and an Adaptive Backstepping Controller (ABSC) are developed for both UAVs to handle mass changes during flight while Genetic Algorithm (GA) is used for the gain optimization. MATLAB Simulink-based numerical simulation reveals that the Bi-Quadrotor has a lower average rotor speed than the RW-Quadrotor. However, the Bi-Quadrotor's SoC after the mission is higher than the RW-Quadrotor, and it took less time to accomplish the mission. The ABSC designed for RW-Quadrotor and Bi-Quadrotor effectively handles mass change during the mission. However, the BSC controller increases energy consumption for the Bi-Quadrotor in the presence of wind gusts.
Název v anglickém jazyce
Performance evaluation of RW-Quadrotor and Bi-Quadrotor for payload delivery
Popis výsledku anglicky
Payload delivery is one of the many Unmanned Aerial Vehicle (UAV) applications that save time, energy, and human resources. The present simulation study compares rotary-wing quadrotors (RW-Quadrotors) and tail-sitter biplane quadrotors (Bi-Quadrotors) under payload delivery conditions that help to choose the best UAV for the particular mission. A comparative study is performed based on (i) time taken to accomplish the given mission, (ii) trajectory tracking performance, (iii) motor speed throughout the entire flight envelope, and (iv) remains SoC (State of Charge) after the mission. Furthermore, a Backstepping Controller (BSC) and an Adaptive Backstepping Controller (ABSC) are developed for both UAVs to handle mass changes during flight while Genetic Algorithm (GA) is used for the gain optimization. MATLAB Simulink-based numerical simulation reveals that the Bi-Quadrotor has a lower average rotor speed than the RW-Quadrotor. However, the Bi-Quadrotor's SoC after the mission is higher than the RW-Quadrotor, and it took less time to accomplish the mission. The ABSC designed for RW-Quadrotor and Bi-Quadrotor effectively handles mass change during the mission. However, the BSC controller increases energy consumption for the Bi-Quadrotor in the presence of wind gusts.
Klasifikace
Druh
J<sub>imp</sub> - Článek v periodiku v databázi Web of Science
CEP obor
—
OECD FORD obor
20204 - Robotics and automatic control
Návaznosti výsledku
Projekt
—
Návaznosti
S - Specificky vyzkum na vysokych skolach
Ostatní
Rok uplatnění
2023
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název periodika
IET Intelligent Transport Systems
ISSN
1751-956X
e-ISSN
1751-9578
Svazek periodika
Neuveden
Číslo periodika v rámci svazku
08
Stát vydavatele periodika
US - Spojené státy americké
Počet stran výsledku
16
Strana od-do
1-16
Kód UT WoS článku
001043119100001
EID výsledku v databázi Scopus
2-s2.0-85166967761