Dynamics and Control of a Multi-Rotor Aircraft

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Dynamics and Control of a Multi-Rotor Aircraft

Despite the fact that aerodynamic loads (forces and moments) induced by airflow relative to a quadrotor vertical take-off and landing aircraft consist of both deterministic and stochastic components, all existing works on controlling the aircraft either ignore these loads or treat them as determini...

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Bibliographic Details
Main Author:	Kava, Sean Anthony
Format:	Thesis
Published:	Curtin University 2016
Online Access:	http://hdl.handle.net/20.500.11937/54059

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