DocumentCode
3073805
Title
Fuzzy logic guidance of formation flight
Author
Kumbasar, Sarper ; Tekinalp, Ozan
Author_Institution
Dept. of Aerosp. Eng., Middle East Tech. Univ., Ankara, Turkey
fYear
2015
fDate
9-12 June 2015
Firstpage
167
Lastpage
175
Abstract
In this paper, fuzzy logic control method is used to control the formation flight of fixed wing aircraft in leader-follower form. A two loop control structure is used. In the inner loop, aircraft flight is controlled using the State Dependent Riccati Equation (SDRE) method. In the outer loop, fuzzy logic control approach is used to control the formation guidance. The success of the approach is demonstrated through simulations.
Keywords
Riccati equations; aircraft control; autonomous aerial vehicles; fuzzy control; position control; SDRE method; aircraft flight control; fixed wing aircraft; formation flight control; formation guidance; fuzzy logic control method; fuzzy logic guidance; inner loop; leader-follower form; loop control structure; outer loop; state dependent Riccati equation method; Aerospace control; Aircraft; Atmospheric modeling; Fuzzy logic; Mathematical model; Riccati equations; Simulation;
fLanguage
English
Publisher
ieee
Conference_Titel
Unmanned Aircraft Systems (ICUAS), 2015 International Conference on
Conference_Location
Denver, CO
Print_ISBN
978-1-4799-6009-5
Type
conf
DOI
10.1109/ICUAS.2015.7152288
Filename
7152288
Link To Document