A Modular and Scalable System Architecture for Heterogeneous
In this paper a modular and scalable architecture for heterogeneous swarm-based Counter Unmanned Aerial Systems (C-UASs) built on PX4-Autopilot and Robot Operating System 2
In this paper a modular and scalable architecture for heterogeneous swarm-based Counter Unmanned Aerial Systems (C-UASs) built on PX4-Autopilot and Robot Operating System 2
This powerful computing platform can quickly process flight status, navigation data, and unmanned aerial vehicle sensor information, such as camera images, radar data, and
A helicopter unmanned aerial vehicle for stabilizing a range of objects in landed and hovering conditions is introduced and demonstrated [6]. This paper discusses the challenges in
TECHNOLOGY AREA (S): Sensors, Electronics, Battlespace OBJECTIVE: Develop a scalable, directional C-Band active array antenna system suitable for Group-IV Unmanned Aerial
The UAV can serve as a scalable testbed for power systems without the prohibitive costs or safety concerns of experimenting with large commercial aircraft. As the power rating of UAVs is
To enhance their efficiency and duration, UAVs typically employ a hybrid power system. This system integrates diverse energy sources, such as fuel cells, batteries, solar
This paper presents the topology selection, optimization, and design of a 48 V drive inverter for drone applications. With predefined efficiency targets at rate.
Last decade witnessed a significant growth for unmanned aerial vehicle (UAV) development, marked by advancements in innovation, production, and diverse applications across various
Recently, Unmanned Aerial Vehicles (UAVs) have attracted significant attentions attributed to their high mobility, low cost, and flexible deployment. Thus, UAVs may potentially
This paper presents the topology selection, optimization, and design of a 48 V drive inverter for drone applications. With predefined efficiency targets at rate.
This research investigated the reliability evaluation of conventional models of multi-level inverters for use in hybrid unmanned aerial vehicles with electric propulsion.
Through these, it is possible to provide flexible and stable network services. Unmanned aerial vehicles perform a wide range of tasks using Internet-of-Things technology,
Atrenne''s engineered solutions are designed to maximize flexibility, scalability, and performance, ensuring that unmanned system manufacturers can integrate cutting-edge modular electronics
To increase endurance and achieve good performance, UAVs generally use a hybrid power supply system architecture. A hybrid power architecture may combine several
Multi-agent unmanned aerial vehicle (UAV) systems have emerged as a promising solution for complex applications such as industrial automation, surveillance, and disaster response.
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Comprehensive state of the art review on electric unmanned aerial vehicles. UAVs critical evaluation of power supply structures and energy management systems. UAVs development gaps, useful guiding recommendations, and prospects. The interest in electric unmanned aerial vehicles (UAVs) is rapidly growing in recent years.
UAV POWER SYSTEM OVERVIEW A generic UAV power system architecture consists of the following elements: power sources, DC-DC converters, a DC bus (DC link), DC-AC inverters, and propulsion motors.
It is worth noting that most available electrical UAVs are using a fuel cell as the main power source. A supercapacitor can also contribute to the power supplying process since it has very high power density and quick response to peak power needed in UAV takeoff and sudden maneuvers.
An example UAV platform is designed to demonstrate applications of the model. Power system architectures are compared based on power losses, craft mass and flight-time. A realistic mission profile is used to examine power system losses and required input energy over various flight stages. Simulation shows