Fault tolerant flight control of a UAV with asymmetric damage to its primary lifting surface

Fault tolerant flight control of a UAV with asymmetric damage to its primary lifting surface

Thesis (MScEng)-- Stellenbosch University, 2013. === ENGLISH ABSTRACT: In this thesis the design, analysis, implementation, and verification of a fault-tolerant unmanned aerial vehicle (UAV) flight control system which is robust to structural damage causing the natural flight dynamics of the vehic...

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Bibliographic Details
Main Author: Beeton, Wiaan
Other Authors: Engelbrecht, J. A. A.
Format: Others
Language:en_ZA
Published: Stellenbosch : Stellenbosch University 2013
Subjects:
Aircraft control
Flight control
Fault-tolerance (Engineering)
Inherent stability
Dissertations > Electrical and electronic engineering
Robust control
Drone aircrafts
Drone aircrafts > Aerodynamics
Theses > Electrical and electronic engineering
Online Access:http://hdl.handle.net/10019.1/85625

Internet

http://hdl.handle.net/10019.1/85625

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