DocumentCode
2317281
Title
Robust Fixed Order Lateral H2 Controller for Micro Air Vehicle
Author
Meenakshi, M. ; Bhat, M. Seetharama
Author_Institution
Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore
fYear
2006
fDate
5-8 Dec. 2006
Firstpage
1
Lastpage
6
Abstract
This paper presents a robust fixed order H2controller design using strengthened discrete optimal projection equations, which approximate the first order necessary optimality condition. The novelty of this work is the application of the robust H2controller to a micro aerial vehicle named Sarika2 developed in house. The controller is designed in discrete domain for the lateral dynamics of Sarika2 in the presence of low frequency atmospheric turbulence (gust) and high frequency sensor noise. The design specification includes simultaneous stabilization, disturbance rejection and noise attenuation over the entire flight envelope of the vehicle. The resulting controller performance is comprehensively analyzed by means of simulation
Keywords
aerospace control; aerospace simulation; control system synthesis; optimal control; robust control; vehicle dynamics; Sarika2; atmospheric turbulence; controller design; discrete optimal projection equations; disturbance rejection; flight envelope; lateral dynamics; micro air vehicle; noise attenuation; robust control; robust fixed order lateral H2 controller; sensor noise; simultaneous stabilization; Attenuation; Equations; Frequency; Hydrogen; Low-frequency noise; Noise robustness; Optimal control; Performance analysis; Robust control; Vehicle dynamics; Micro Air Vehicle; Robust Control; Strengthened Discrete Optimal Projection Equation;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation, Robotics and Vision, 2006. ICARCV '06. 9th International Conference on
Conference_Location
Singapore
Print_ISBN
1-4244-0341-3
Electronic_ISBN
1-4214-042-1
Type
conf
DOI
10.1109/ICARCV.2006.345174
Filename
4150084
Link To Document