DocumentCode :
3485151
Title :
Trajectory tracking of unmanned aerial vehicle using servomechanism strategy
Author :
Kakirde, Nishant P. ; Davari, Asad ; Wang, Jin
Author_Institution :
MS Control Syst., WVU Tech, USA
fYear :
2005
fDate :
20-22 March 2005
Firstpage :
163
Lastpage :
166
Abstract :
This paper describes the application of servomechanism/output regulation strategy to unmanned aerial vehicles (UAV) for the trajectory tracking. In this paper all the aspects of the UAV tracking control from mathematical modeling to controller implementation are considered. Output regulation strategy is mainly used for the accurate tracking of the reference trajectory. In this paper the kinematic model of UAV is considered for the implementation of controller. Our approach is limited to a single unmanned aerial vehicle trajectory tracking. This strategy enables increased reliability, stability, quality assurance of safety critical UAVs. This output regulation strategy demonstrates the ability of accurate trajectory tracking, so it improves the overall performance of the UAV. In this paper we present the simulation results of implementation of the servomechanism strategy for UAV.
Keywords :
aircraft control; remotely operated vehicles; servomechanisms; stability; tracking; vehicle dynamics; kinematic model; output regulation strategy; servomechanism strategy; trajectory tracking; unmanned aerial vehicle; Control systems; Differential algebraic equations; Helicopters; Kinematics; Nonlinear equations; Partial differential equations; Servomechanisms; Trajectory; Unmanned aerial vehicles; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Theory, 2005. SSST '05. Proceedings of the Thirty-Seventh Southeastern Symposium on
ISSN :
0094-2898
Print_ISBN :
0-7803-8808-9
Type :
conf
DOI :
10.1109/SSST.2005.1460898
Filename :
1460898
Link To Document :
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