H
Hugh H. T. Liu
Researcher at University of Toronto
Publications - 196
Citations - 2878
Hugh H. T. Liu is an academic researcher from University of Toronto. The author has contributed to research in topics: Control theory & Control system. The author has an hindex of 24, co-authored 188 publications receiving 2180 citations. Previous affiliations of Hugh H. T. Liu include Nanjing University of Aeronautics and Astronautics.
Papers
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Proceedings ArticleDOI
Formation UAV flight control using virtual structure and motion synchronization
N.H.M. Linorman,Hugh H. T. Liu +1 more
TL;DR: The synchronized position tracking controller is incorporated in formation flight control for multiple flying wings with improved performance and effectiveness when the virtual structure approach is utilized to maintain formation geometry.
Journal ArticleDOI
Decentralized Localization of Sparsely-Communicating Robot Networks: A Centralized-Equivalent Approach
TL;DR: It is proved that a robot only needs to consider its own knowledge of network topology in order to produce an estimate equivalent to the centralized state estimate whenever possible while ensuring that the same can be performed by all other robots in the network.
Proceedings ArticleDOI
A cooperative UAV/UGV platform for wildfire detection and fighting
C. Phan,Hugh H. T. Liu +1 more
TL;DR: The potential application of the proposed hierarchical vehicle platform to high-risk missions, specifically in the context of wildfire fighting, is discussed, and the task generation and allocation problems and proposed approaches are presented.
Journal ArticleDOI
Model-Predictive Gust Load Alleviation Controller for a Highly Flexible Aircraft
TL;DR: A unified dynamics framework is developed to represent the full six-degrees-of-freedom rigid body alongwith the structural dynamics, allowing for an integrated control design to account for maneuverability (flying qualities) and aeroelasticity simultaneously, leading to a new and improved configuration for a very flexible aircraft.
Journal ArticleDOI
Aeroservoelastic Design Optimization of a Flexible Wing
TL;DR: A multidisciplinary design optimization framework is developed that integrates control system design with aerostructural design and the inclusion of load alleviation system in design leads to a significant increase in endurance performance.