Integrated PID controller design for an unmanned aerial vehicle with static stability

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Integrated PID controller design for an unmanned aerial vehicle with static stability

This paper presents an integrated guidance and control (IGC) design method for an unmanned aerial vehicle with static stability which is described by a nonlinear six-degree-of-freedom (6-DOF) model. The model is linearized by using small disturbance linearization. The dynamic characteristics of pitc...

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Bibliographic Details
Main Authors:	Li, R., Shi, Y., Xu, Honglei
Format:	Journal Article
Published:	Cambridge University Press 2013
Online Access:	http://hdl.handle.net/20.500.11937/52221

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