DEVELOPMENT OF A HYBRID FIXED-WING VTOL UNMANNED AERIAL VEHICLE
Апстракт
As the use of unmanned aerial vehicles (UAV) in the world has expanded, the market needs for the development of multi-role unmanned systems are increasing. These unmanned systems tend to largely find their constant and irreplaceable role in many industries. The development of such systems is a complex process, which, among other things, must include detailed structural, static and dynamic calculations and testing. The UAV presented in this paper is a hybrid powered aircraft with vertical take-off and landing (VTOL) with a composite structure and an innovative hybrid propulsion with a starter-generator system. VTOL gives an advantage in the exploitation of the aircraft itself, because it does not require special ground conditions or space for take-off and landing. The starter and generator system enables a smaller amount of fixed mass, such as batteries, while the structure made of composite materials enables a smaller mass and the desired characteristics of strength, resistance to corr...osion and fatigue. This paper present development review process of the latest technology in terms of the concept of system and subsystem operation, as well as financially favorable and high-quality construction.
Кључне речи:
Composite materials / Hybrid propulsion / VTOL UAV / developmentИзвор:
9th International Congress of Serbian Society of Mechanics, Vrnjačka Banja 5–7.07.2023, 2023Издавач:
- Serbian Society of Mechanics
Финансирање / пројекти:
- Динамика хибридних система сложених структура. Механика материјала (RS-MESTD-Basic Research (BR or ON)-174001)
Колекције
Институција/група
Mašinski fakultetTY - CONF AU - Radulović, Radoslav AU - Milić, Milica PY - 2023 UR - https://machinery.mas.bg.ac.rs/handle/123456789/7727 AB - As the use of unmanned aerial vehicles (UAV) in the world has expanded, the market needs for the development of multi-role unmanned systems are increasing. These unmanned systems tend to largely find their constant and irreplaceable role in many industries. The development of such systems is a complex process, which, among other things, must include detailed structural, static and dynamic calculations and testing. The UAV presented in this paper is a hybrid powered aircraft with vertical take-off and landing (VTOL) with a composite structure and an innovative hybrid propulsion with a starter-generator system. VTOL gives an advantage in the exploitation of the aircraft itself, because it does not require special ground conditions or space for take-off and landing. The starter and generator system enables a smaller amount of fixed mass, such as batteries, while the structure made of composite materials enables a smaller mass and the desired characteristics of strength, resistance to corrosion and fatigue. This paper present development review process of the latest technology in terms of the concept of system and subsystem operation, as well as financially favorable and high-quality construction. PB - Serbian Society of Mechanics C3 - 9th International Congress of Serbian Society of Mechanics, Vrnjačka Banja 5–7.07.2023 T1 - DEVELOPMENT OF A HYBRID FIXED-WING VTOL UNMANNED AERIAL VEHICLE UR - https://hdl.handle.net/21.15107/rcub_machinery_7727 ER -
@conference{ author = "Radulović, Radoslav and Milić, Milica", year = "2023", abstract = "As the use of unmanned aerial vehicles (UAV) in the world has expanded, the market needs for the development of multi-role unmanned systems are increasing. These unmanned systems tend to largely find their constant and irreplaceable role in many industries. The development of such systems is a complex process, which, among other things, must include detailed structural, static and dynamic calculations and testing. The UAV presented in this paper is a hybrid powered aircraft with vertical take-off and landing (VTOL) with a composite structure and an innovative hybrid propulsion with a starter-generator system. VTOL gives an advantage in the exploitation of the aircraft itself, because it does not require special ground conditions or space for take-off and landing. The starter and generator system enables a smaller amount of fixed mass, such as batteries, while the structure made of composite materials enables a smaller mass and the desired characteristics of strength, resistance to corrosion and fatigue. This paper present development review process of the latest technology in terms of the concept of system and subsystem operation, as well as financially favorable and high-quality construction.", publisher = "Serbian Society of Mechanics", journal = "9th International Congress of Serbian Society of Mechanics, Vrnjačka Banja 5–7.07.2023", title = "DEVELOPMENT OF A HYBRID FIXED-WING VTOL UNMANNED AERIAL VEHICLE", url = "https://hdl.handle.net/21.15107/rcub_machinery_7727" }
Radulović, R.,& Milić, M.. (2023). DEVELOPMENT OF A HYBRID FIXED-WING VTOL UNMANNED AERIAL VEHICLE. in 9th International Congress of Serbian Society of Mechanics, Vrnjačka Banja 5–7.07.2023 Serbian Society of Mechanics.. https://hdl.handle.net/21.15107/rcub_machinery_7727
Radulović R, Milić M. DEVELOPMENT OF A HYBRID FIXED-WING VTOL UNMANNED AERIAL VEHICLE. in 9th International Congress of Serbian Society of Mechanics, Vrnjačka Banja 5–7.07.2023. 2023;. https://hdl.handle.net/21.15107/rcub_machinery_7727 .
Radulović, Radoslav, Milić, Milica, "DEVELOPMENT OF A HYBRID FIXED-WING VTOL UNMANNED AERIAL VEHICLE" in 9th International Congress of Serbian Society of Mechanics, Vrnjačka Banja 5–7.07.2023 (2023), https://hdl.handle.net/21.15107/rcub_machinery_7727 .