TY - GEN
T1 - Lift-plus-Cruise Aircraft Modeling, Guidance, Adaptive Control,and Flight Simulation
AU - Khamvilai, Thanakorn
AU - Lewis, Jeffrey
AU - Iyer, Venkatakrishnan
AU - Horn, Joseph
AU - Johnson, Eric
AU - Taylor, Brian
N1 - Publisher Copyright:
© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2024
Y1 - 2024
N2 - In the rapidly evolving sectors of Unmanned Aircraft Systems (UAS) and Urban Air Mobility (UAM), there is an increasing need for technologies that can cater to both Department of Defense (DoD) and commercial applications. These applications range from logistics and supply delivery to disaster relief, search and rescue operations, air taxi services, and operations in underdeveloped areas. This paper presents the development and testing of an adaptive flight control system for lift-plus-cruise eVTOL aircraft, aimed at providing a smooth transition from hover/low-speed flight to forward/high-speed flight. The proposed framework consists of the aircraft model, the guidance system that translates pilot inceptor commands to control inputs, and the neural network adaptive controller that stabilizes the aircraft. The simulation is performed to demonstrate the robustness and adaptability of the system for UAM in diverse operational contexts.
AB - In the rapidly evolving sectors of Unmanned Aircraft Systems (UAS) and Urban Air Mobility (UAM), there is an increasing need for technologies that can cater to both Department of Defense (DoD) and commercial applications. These applications range from logistics and supply delivery to disaster relief, search and rescue operations, air taxi services, and operations in underdeveloped areas. This paper presents the development and testing of an adaptive flight control system for lift-plus-cruise eVTOL aircraft, aimed at providing a smooth transition from hover/low-speed flight to forward/high-speed flight. The proposed framework consists of the aircraft model, the guidance system that translates pilot inceptor commands to control inputs, and the neural network adaptive controller that stabilizes the aircraft. The simulation is performed to demonstrate the robustness and adaptability of the system for UAM in diverse operational contexts.
UR - https://www.scopus.com/pages/publications/85203025551
UR - https://www.scopus.com/pages/publications/85203025551#tab=citedBy
U2 - 10.2514/6.2024-3625
DO - 10.2514/6.2024-3625
M3 - Conference contribution
AN - SCOPUS:85203025551
SN - 9781624107160
T3 - AIAA Aviation Forum and ASCEND, 2024
BT - AIAA Aviation Forum and ASCEND, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation Forum and ASCEND, 2024
Y2 - 29 July 2024 through 2 August 2024
ER -