2026-09-20T06:43:22Zhttps://api.drum.lib.umd.edu/server/oai/request

oai:drum.lib.umd.edu:1903/267002022-03-12T11:08:26Zcom_1903_2206com_1903_1654com_1903_2col_1903_2737col_1903_3

Xu, Huan Thompson, Derek Digital Repository at the University of Maryland University of Maryland (College Park, Md.) Aerospace Engineering 2021-02-13T06:30:53Z 2021-02-13T06:30:53Z 2020 https://doi.org/10.13016/ulnk-f0vk http://hdl.handle.net/1903/26700 The advancements in electric motor propulsion and battery technologies have made the implementation of electric power in aerial transportation increasingly feasible. As such, the interest and development of electric vertical takeoff and landing (eVTOL) aircraft has become a greater portion of the market. This increase drives a need for research into control of the eVTOLs to ensure safe flight through the transition from hover to forward flight. This paper proposes a control strategy using the transition dynamics in a gain scheduling LQR attitude controller to robustly control the vehicle at any point throughout transition. The proposed control strategy is tested through implementation in nonlinear 3DOF and 6DOF simulations. The robustness of the controller is tested through simulating transition and virtual mission profiles. en ROBUST CONTROL OF AN EVTOL THROUGH TRANSITION WITH A GAIN SCHEDULING LQR CONTROLLER Thesis Aerospace engineering eVTOL Gain Scheduling LQR open.access