DocumentCode
181487
Title
Influence of number of measured states on accuracy and robustness of flight control system
Author
Klipa, A.M. ; Sydorenko, A.D.
Author_Institution
Aircraft Control Syst. Dept., Nat. Aviation Univ., Kiev, Ukraine
fYear
2014
fDate
14-17 Oct. 2014
Firstpage
125
Lastpage
128
Abstract
Recently in many countries the efforts of researchers are directed to the design of low cost, accurate and robust controllers for small Unmanned Aerial Vehicle (UAV) using the minimum number of on-board sensors. The basic problem of such kind of design is to restore the unknown (unmeasured) states. The approach proposed in the paper consists of two procedures: state restoration by the reduced-order observer (Luenberger filter) and optimal deterministic controller design. This technique was applied to the “benchmark” model of UAV longitudinal motion (there were considered two cases: with three and two on-board sensors only) and results of its application are presented.
Keywords
aircraft control; autonomous aerial vehicles; control system synthesis; observers; optimal control; Luenberger filter; UAV longitudinal motion; flight control system; measured states; on-board sensors; optimal deterministic controller design; reduced-order observer; state restoration; unmanned aerial vehicle; Aerospace control; Aircraft; Mathematical model; Observers; Robustness; Sensors; Vectors; aircraft and actuator dynamics; incomplete measurements; longitudinal motion; optimal deterministic controller; small UAV; state restoration;
fLanguage
English
Publisher
ieee
Conference_Titel
Methods and Systems of Navigation and Motion Control (MSNMC), 2014 IEEE 3rd International Conference on
Conference_Location
Kiev
Print_ISBN
978-1-4799-6578-6
Type
conf
DOI
10.1109/MSNMC.2014.6979749
Filename
6979749
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