DocumentCode
2965303
Title
Auto-Tuning for High Performance Autopilot Design Using Robust Inverse Dynamics Estimation
Author
Counsell, John M. ; Zaher, Obadah S. ; Brindley, Joseph
Author_Institution
Dept. of Mech. Eng., Univ. of Strathclyde, Glasgow, UK
fYear
2010
fDate
20-25 Sept. 2010
Firstpage
10
Lastpage
17
Abstract
A novel auto-tuning method for the Robust Inverse Dynamics Estimation (RIDE) controller algorithm is presented. The RIDE controller is applied to a high performance aircraft model. The tuner utilises a constrained genetic algorithm to automate the tuning process. The stability constraints on the algorithm ensure system stability whilst allowing for the optimum controller parameters to be selected. The results of the tuner are compared with that of another tuning method which utilises unconstrained optimisation so as to highlight the efficacy of constrained optimisation for this application. It is shown from the results that the constrained genetic algorithm optimisation scheme offers a highly effective tuning solution for the RIDE control algorithm which can be used to attain safe and high performance control.
Keywords
aircraft control; estimation theory; genetic algorithms; optimal control; robust control; self-adjusting systems; RIDE controller algorithm; auto-tuning; constrained genetic algorithm; constrained optimisation; high performance aircraft model; high performance autopilot design; optimum controller parameter; robust inverse dynamics estimation; stability constraint; system stability; Aircraft; Algorithm design and analysis; Atmospheric modeling; Damping; Gallium; Optimization; Tuning; RIDE; auto-tuning; autopilot; genetic algorithm; optimisation;
fLanguage
English
Publisher
ieee
Conference_Titel
Computing in the Global Information Technology (ICCGI), 2010 Fifth International Multi-Conference on
Conference_Location
Valencia
Print_ISBN
978-1-4244-8068-5
Electronic_ISBN
978-0-7695-4181-5
Type
conf
DOI
10.1109/ICCGI.2010.38
Filename
5628946
Link To Document