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Title: Concept and realization of unmanned aerial system with different modes of operation

Abstract

In this paper we describe the development process of unmanned aerial system, its mechanical components, electronics and software solutions. During the stage of design, we have formulated some necessary requirements for the multirotor vehicle and ground control station in order to build an optimal system which can be used for the reconnaissance missions. Platform is controlled by use of the ground control station (GCS) and has possibility of accomplishing video based observation tasks. In order to fulfill this requirement the on-board payload consists of mechanically stabilized camera augmented with machine vision algorithms to enable object tracking tasks. Novelty of the system are four modes of flight, which give full functionality of the developed UAV system. Designed ground control station is consisted not only of the application itself, but also a built-in dedicated components located inside the chassis, which together creates an advanced UAV system supporting the control and management of the flight. Mechanical part of quadrotor is designed to ensure its robustness while meeting objectives of minimizing weight of the platform. Finally the designed electronics allows for implementation of control and estimation algorithms without the needs for their excessive computational optimization.

Authors:
; ; ; ; ;  [1]
  1. Silesian University of Technology, Akademicka 2A, 44-100 Gliwice (Poland)
Publication Date:
OSTI Identifier:
22390785
Resource Type:
Journal Article
Resource Relation:
Journal Name: AIP Conference Proceedings; Journal Volume: 1637; Journal Issue: 1; Conference: ICNPAA 2014: 10. International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, Narvik (Norway), 15-18 Jul 2014; Other Information: (c) 2014 AIP Publishing LLC; Country of input: International Atomic Energy Agency (IAEA)
Country of Publication:
United States
Language:
English
Subject:
71 CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS; ALGORITHMS; CAMERAS; COMPUTER CODES; CONTROL; DESIGN; IMPLEMENTATION; OPERATION; OPTIMIZATION; STRATA CONTROL; VEHICLES; VISION

Citation Formats

Czyba, Roman, Szafrański, Grzegorz, Janusz, Wojciech, Niezabitowski, Michał, Czornik, Adam, and Błachuta, Marian. Concept and realization of unmanned aerial system with different modes of operation. United States: N. p., 2014. Web. doi:10.1063/1.4904587.
Czyba, Roman, Szafrański, Grzegorz, Janusz, Wojciech, Niezabitowski, Michał, Czornik, Adam, & Błachuta, Marian. Concept and realization of unmanned aerial system with different modes of operation. United States. doi:10.1063/1.4904587.
Czyba, Roman, Szafrański, Grzegorz, Janusz, Wojciech, Niezabitowski, Michał, Czornik, Adam, and Błachuta, Marian. Wed . "Concept and realization of unmanned aerial system with different modes of operation". United States. doi:10.1063/1.4904587.
@article{osti_22390785,
title = {Concept and realization of unmanned aerial system with different modes of operation},
author = {Czyba, Roman and Szafrański, Grzegorz and Janusz, Wojciech and Niezabitowski, Michał and Czornik, Adam and Błachuta, Marian},
abstractNote = {In this paper we describe the development process of unmanned aerial system, its mechanical components, electronics and software solutions. During the stage of design, we have formulated some necessary requirements for the multirotor vehicle and ground control station in order to build an optimal system which can be used for the reconnaissance missions. Platform is controlled by use of the ground control station (GCS) and has possibility of accomplishing video based observation tasks. In order to fulfill this requirement the on-board payload consists of mechanically stabilized camera augmented with machine vision algorithms to enable object tracking tasks. Novelty of the system are four modes of flight, which give full functionality of the developed UAV system. Designed ground control station is consisted not only of the application itself, but also a built-in dedicated components located inside the chassis, which together creates an advanced UAV system supporting the control and management of the flight. Mechanical part of quadrotor is designed to ensure its robustness while meeting objectives of minimizing weight of the platform. Finally the designed electronics allows for implementation of control and estimation algorithms without the needs for their excessive computational optimization.},
doi = {10.1063/1.4904587},
journal = {AIP Conference Proceedings},
number = 1,
volume = 1637,
place = {United States},
year = {Wed Dec 10 00:00:00 EST 2014},
month = {Wed Dec 10 00:00:00 EST 2014}
}
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