Title :
Design of fuzzy inference system for estimating the flight control dynamics
Author :
Deepika, K.M. ; Roopashree, S. ; Bhat, Shubha
Author_Institution :
Dept. of Comput. Sci. & Eng., Dayananda Sagar Coll. of Eng., Bangalore, India
Abstract :
This paper describes the design of Fuzzy Inference System to control the flight dynamic parameters of Unmanned Aerial Vehicle such as attitude [latitude, longitude and altitude], angles of rotation known as pitch and roll. A Soft Computing technique called Fuzzy Logic is used to design the Fuzzy Inference System. Visual simulation tool and Aerosim (Aeronautical Simulation Set) Flight gear interface are used for Simulation purpose.
Keywords :
aerospace simulation; aircraft; attitude control; control engineering computing; fuzzy control; fuzzy reasoning; mobile robots; remotely operated vehicles; aeronautical simulation set; aerosim flight gear interface; attitude control; flight control dynamics; fuzzy inference system; fuzzy logic; soft computing technique; unmanned aerial vehicle; visual simulation tool; Aerodynamics; Aircraft; Aircraft navigation; Atmospheric modeling; Fuzzy logic; Mathematical model; Unmanned aerial vehicles; Fuzzy Inference System (FIS); Fuzzy Logic (FL); Soft Computing Techniques; Unmanned Aerial Vehicle (UAV);
Conference_Titel :
Intelligent Agent and Multi-Agent Systems (IAMA), 2011 2nd International Conference on
Conference_Location :
Chennai
Print_ISBN :
978-1-4577-0876-3
DOI :
10.1109/IAMA.2011.6048995
