Design of a flexible high performance quadcopter platform breaking the MAV endurance record with laser power beaming
Разработка гибкой высокопроизводительной платформы квадрокоптера, установившей рекорд продолжительности полёта БПЛА сверхмалого класса с использованием лазерной передачи энергии
2011-09-01
SCID: 54.1/47y5z75v
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MAV enduranceflight control systemlaser power beamingposition control systemquadcopter platform
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Abstract (AI)
In this paper we present the design of a highly flexible quadcopter platform and the software tools used in an example experiment to show unlimited flight time of an MAV with laser power beaming.We describe the mechanical design as well as the flight control system architecture which are focused on easy adaption to a wide variety of experiments. The paper also includes size, payload and flight time considerations and explains the tools to adapt the vehicle to the specific application. The design of a position control system implemented on the microprocessor hardware using a specially developed framework for MATLAB/Simulink is described as well. The robustness of the overall system and the presented position control structure is proven by the result of the 12:27 h continuous flight with a 1 kg MAV.
Key Findings
1
A highly flexible quadcopter platform was designed to support easy adaptation across a wide variety of experiments.
2
System robustness was demonstrated through a 12:27-hour continuous flight of a 1 kg MAV, breaking the MAV endurance record.
3
The paper presents a flight-control architecture and MATLAB/Simulink-based development framework enabling adaptable position-control implementation.
4
The platform integrates laser power beaming to demonstrate effectively unlimited flight time for a micro aerial vehicle.
Research Object
a flexible 1 kg quadcopter micro aerial vehicle (MAV) powered by laser power beaming
Research Subject
the vehicle’s adaptable mechanical and flight-control design, position-control performance, and endurance enabling a 12:27 h continuous flight
Publication Details
Publication Date
2011-09-01
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