DocumentCode :
2473630
Title :
Modified ILMI algorithm for practical PID/PD implementation on a micro air vehicle
Author :
Satak, Neha ; Bhat, M. Seetharama
Author_Institution :
Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
fYear :
2009
fDate :
10-12 June 2009
Firstpage :
4660
Lastpage :
4665
Abstract :
This paper extends the iterative linear matrix inequality algorithm (ILMI) for systems having non-ideal PI, PD and PID implementations. The new algorithm uses the practical implementation of the feedback blocks to form the equivalent static output feedback plant. The LMI based synthesis techniques are used in the algorithm to design a multi-loop, multi-objective fixed structure control. The benefits of such a control design technique are brought out by applying it to the lateral stabilizing and tracking feedback control problem of a 30 cm wingspan micro air vehicle.
Keywords :
PD control; aircraft; control system synthesis; iterative methods; linear matrix inequalities; three-term control; LMI based synthesis techniques; PID-PD implementation; control design technique; equivalent static output feedback plant; feedback; iterative linear matrix inequality algorithm; multi-objective fixed structure control; multiloop design; wingspan micro air vehicle; Automatic control; Control design; Control system synthesis; Iterative algorithms; Linear matrix inequalities; Output feedback; Robust stability; State feedback; Three-term control; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2009. ACC '09.
Conference_Location :
St. Louis, MO
ISSN :
0743-1619
Print_ISBN :
978-1-4244-4523-3
Electronic_ISBN :
0743-1619
Type :
conf
DOI :
10.1109/ACC.2009.5160496
Filename :
5160496
Link To Document :
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