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contributor authorLijia Cao
contributor authorXiaoxiang Hu
contributor authorShengxiu Zhang
contributor authorYunfeng Liu
date accessioned2017-12-16T09:22:14Z
date available2017-12-16T09:22:14Z
date issued2017
identifier other%28ASCE%29AS.1943-5525.0000783.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4241964
description abstractThe sensor-based backstepping control law, which is not sensitive to model uncertainty, uses less model knowledge and the measurements of state derivatives. A flight control law based on a sensor-based backstepping method for unmanned aerial vehicles (UAVs) is proposed in this paper. The nonlinear model uncertainties of a UAV and sensor noise are concerning. Moreover, command filters are used to handle dynamics and saturation effects of the actuators for carrying out the flight control law. The simulation results show the proposed flight control law can guarantee the closed-loop system stability and has better tracking control performance than the block backstepping control law with model uncertainty.
publisherAmerican Society of Civil Engineers
titleRobust Flight Control Design Using Sensor-Based Backstepping Control for Unmanned Aerial Vehicles
typeJournal Paper
journal volume30
journal issue6
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000783
treeJournal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 006
contenttypeFulltext


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