Date of Award
1-1-2019
Document Type
Dissertation
Degree Name
Ph.D.
Organizational Unit
Daniel Felix Ritchie School of Engineering and Computer Science
First Advisor
Kimon P. Valavanis, Ph.D.
Second Advisor
Matthew J. Rutherford, Ph.D.
Keywords
Flight control, Model uncertainty, Robust control, Unmanned aerial vehicles
Abstract
Unmanned Aerial Vehicles (UAVs) are here and they are here to stay. Unmanned Aviation has expanded significantly in recent years and research and development in the field of navigation and control have advanced beyond expectations. UAVs are currently being used for defense programs around the world but the range of applications is expected to grow in the near future, with civilian applications such as environmental and aerial monitoring, aerial surveillance and homeland security being some representative examples. Conventional and commercially available small-scale UAVs have limited utilization and applicability to executing specific short-duration missions because of limitations in size, payload, power supply and endurance. This fact has already marked the dawn of a new era of more powerful and versatile UAVs (e.g. morphing aircraft), able to perform a variety of missions. This dissertation presents a novel, comprehensive, step-by-step, nonlinear controller design framework for new generation, non-conventional UAVs with time-varying aerodynamic characteristics during flight. Controller design for such UAVs is a challenging task mainly due to uncertain aerodynamic parameters in the UAV mathematical model. This challenge is tackled by using and implementing μ-analysis and additive uncertainty weighting functions. The technique described herein can be generalized and applied to the class of non-conventional UAVs, seeking to address uncertainty challenges regarding the aircraft's aerodynamic coefficients.
Publication Statement
Copyright is held by the author. User is responsible for all copyright compliance.
Rights Holder
Michail G. Michailidis
Provenance
Received from ProQuest
File Format
application/pdf
Language
en
File Size
139 p.
Recommended Citation
Michailidis, Michail G., "Nonlinear Controller Design for UAVs with Time-Varying Aerodynamic Uncertainties" (2019). Electronic Theses and Dissertations. 1553.
https://digitalcommons.du.edu/etd/1553
Copyright date
2019
Discipline
Applied mathematics, Electrical engineering, Engineering