DocumentCode :
1618522
Title :
Nonlinear trajectory tracking using vectorial backstepping approach
Author :
Bang, Hyochoong ; Lee, Sangjong ; Lee, Haechang
Author_Institution :
Dept. of Aerosp. Eng., Korea Adv. Inst. of Sci. & Technol., Daejeon
fYear :
2008
Firstpage :
169
Lastpage :
174
Abstract :
This paper discussed a nonlinear trajectory tracking problem for stratospheric airship platform and a novel approach of the nonlinear control scheme is applied. Target airship model is the 200 m stratospheric airship platform capable of flying upto 20 km altitude. Full 6-DOF nonlinear dynamics of unmanned airship are defined according to the target airshippsilas configuration including the moving wind field. Based on this airship model, a backstepping design formulation for the trajectory tracking control is described. The tracking control strategy of vectorial backstepping is applied to derive the tracking control law and global asymptotically stability is proved by Lyapunov stability analysis. Finally, numerical simulations have been carried out to assess the performance of the proposed tracking controller.
Keywords :
Lyapunov methods; aircraft control; asymptotic stability; nonlinear control systems; position control; remotely operated vehicles; 6-DOF nonlinear dynamics; Lyapunov stability analysis; global asymptotically stability; moving wind field; nonlinear control scheme; nonlinear trajectory tracking; stratospheric airship platform; trajectory tracking control; unmanned airship; vectorial backstepping approach; Aerospace control; Aerospace engineering; Backstepping; Control systems; Lyapunov method; Nonlinear control systems; Nonlinear equations; Target tracking; Trajectory; Vehicle dynamics; Backstepping Control; Lighter-Than-Air Vehicle; Nonlinear Control; Stratospheric Airship Platform; Trajectory Tracking;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation and Systems, 2008. ICCAS 2008. International Conference on
Conference_Location :
Seoul
Print_ISBN :
978-89-950038-9-3
Electronic_ISBN :
978-89-93215-01-4
Type :
conf
DOI :
10.1109/ICCAS.2008.4694544
Filename :
4694544
Link To Document :
بازگشت