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Title: Synthesis of the unmanned aerial vehicle remote control augmentation system

Abstract

Medium size Unmanned Aerial Vehicle (UAV) usually flies as an autonomous aircraft including automatic take-off and landing phases. However in the case of the on-board control system failure, the remote steering is using as an emergency procedure. In this reason, remote manual control of unmanned aerial vehicle is used more often during take-of and landing phases. Depends on UAV take-off mass and speed (total energy) the potential crash can be very danger for airplane and environment. So, handling qualities of UAV is important from pilot-operator point of view. In many cases the dynamic properties of remote controlling UAV are not suitable for obtaining the desired properties of the handling qualities. In this case the control augmentation system (CAS) should be applied. Because the potential failure of the on-board control system, the better solution is that the CAS algorithms are placed on the ground station computers. The method of UAV handling qualities shaping in the case of basic control system failure is presented in this paper. The main idea of this method is that UAV reaction on the operator steering signals should be similar - almost the same - as reaction of the 'ideal' remote control aircraft. The model following methodmore » was used for controller parameters calculations. The numerical example concerns the medium size MP-02A UAV applied as an aerial observer system.« less

Authors:
 [1]
  1. Department of Avionics and Control Systems, Faculty of Mechanical Engineering and Aeronautics, Rzeszów University of Technology, Al. Powstañców Warszawy 12, 35-959 Rzeszów (Poland)
Publication Date:
OSTI Identifier:
22390767
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; AIRCRAFT; ALGORITHMS; CONTROL SYSTEMS; FAILURES; MASS; MATHEMATICAL SOLUTIONS; POTENTIALS; REMOTE CONTROL; SIGNALS; SYNTHESIS; VELOCITY

Citation Formats

Tomczyk, Andrzej, E-mail: A.Tomczyk@prz.edu.pl. Synthesis of the unmanned aerial vehicle remote control augmentation system. United States: N. p., 2014. Web. doi:10.1063/1.4904684.
Tomczyk, Andrzej, E-mail: A.Tomczyk@prz.edu.pl. Synthesis of the unmanned aerial vehicle remote control augmentation system. United States. doi:10.1063/1.4904684.
Tomczyk, Andrzej, E-mail: A.Tomczyk@prz.edu.pl. 2014. "Synthesis of the unmanned aerial vehicle remote control augmentation system". United States. doi:10.1063/1.4904684.
@article{osti_22390767,
title = {Synthesis of the unmanned aerial vehicle remote control augmentation system},
author = {Tomczyk, Andrzej, E-mail: A.Tomczyk@prz.edu.pl},
abstractNote = {Medium size Unmanned Aerial Vehicle (UAV) usually flies as an autonomous aircraft including automatic take-off and landing phases. However in the case of the on-board control system failure, the remote steering is using as an emergency procedure. In this reason, remote manual control of unmanned aerial vehicle is used more often during take-of and landing phases. Depends on UAV take-off mass and speed (total energy) the potential crash can be very danger for airplane and environment. So, handling qualities of UAV is important from pilot-operator point of view. In many cases the dynamic properties of remote controlling UAV are not suitable for obtaining the desired properties of the handling qualities. In this case the control augmentation system (CAS) should be applied. Because the potential failure of the on-board control system, the better solution is that the CAS algorithms are placed on the ground station computers. The method of UAV handling qualities shaping in the case of basic control system failure is presented in this paper. The main idea of this method is that UAV reaction on the operator steering signals should be similar - almost the same - as reaction of the 'ideal' remote control aircraft. The model following method was used for controller parameters calculations. The numerical example concerns the medium size MP-02A UAV applied as an aerial observer system.},
doi = {10.1063/1.4904684},
journal = {AIP Conference Proceedings},
number = 1,
volume = 1637,
place = {United States},
year = 2014,
month =
}
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