Dynamic Modelling and Energy-efficient Trajectory Planning of an Electric Fixed-wing Aircraft

dc.contributor.authorShum, Christopher
dc.date.accessioned2026-05-28T19:15:05Z
dc.date.available2026-05-28T19:15:05Z
dc.date.issued2026-05-28
dc.date.submitted2026-05-14
dc.description.abstractElectrification of air transportation is an emerging technology with the potential to sig- nificantly reduce global greenhouse gas emissions. The Pipistrel Velis Electro, an all-electric fixed-wing light aircraft, is the first battery-electric aircraft to receive type certification in Canada. This technology represents an opportunity to eliminate aircraft exhaust emis- sions and reduce the cost of operation. However, similar to other electric vehicles, electric aircraft are subject to physically-limited energy density compared to liquid fuels, which makes energy-efficient operation critical to maximize their benefits. Toward this goal, the development of computational models based on system-specific performance can enable more precise operational planning. In this thesis, a series of models are developed that represent the aircraft’s subsystems that contribute to energy flow and consumption. First, a set of physics-based models was developed using established governing equations. Analogous black-box data-driven models consisting of feedforward neural networks are then trained to approximate physical relationships for aspects of the system. A neural network is also trained to approximate the residual error of the physics-based system model compared to the measured observations, then combined with the output of the physics-based model in a hybrid architecture to improve accuracy and compensate for system-specific and environment-specific deviation. The models are tuned and validated using real-world data collected from flight testing. The best-performing model is then used to estimate the energy consumption of the aircraft as a function of the change in state and exogenous variables. By mapping the state trajectory to a directed graph, graph-based optimization methods can be utilized. The projected energy consumption is mapped to the graph as edge costs, and a shortest- path algorithm is applied to find the minimum energy path with respect to the decision variables.
dc.identifier.urihttps://hdl.handle.net/10012/23428
dc.language.isoen
dc.pendingfalse
dc.publisherUniversity of Waterlooen
dc.subjectelectric vehicles
dc.subjectmachine learning
dc.subjectoptimization
dc.titleDynamic Modelling and Energy-efficient Trajectory Planning of an Electric Fixed-wing Aircraft
dc.typeMaster Thesis
uws-etd.degreeMaster of Applied Science
uws-etd.degree.departmentSystems Design Engineering
uws-etd.degree.disciplineSystem Design Engineering
uws-etd.degree.grantorUniversity of Waterlooen
uws-etd.embargo.terms0
uws.contributor.advisorMcPhee, John
uws.contributor.advisorFischmeister, Sebastian
uws.contributor.affiliation1Faculty of Engineering
uws.peerReviewStatusUnrevieweden
uws.published.cityWaterlooen
uws.published.countryCanadaen
uws.published.provinceOntarioen
uws.scholarLevelGraduateen
uws.typeOfResourceTexten

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