Subjects: AERONAVES NÃO TRIPULADAS, SIMULAÇÃO (APRENDIZAGEM), VOO (ENGENHARIA AERONÁUTICA), FILTROS DE KALMAN
ABNT
DAUD FILHO, Antonio Carlos. A tilt-wing VTOL UAV configuration study: flight dynamics modeling, simulation, states estimation, control, systems integration and flight testing. 2023. Tese (Doutorado) – Universidade de São Paulo, São Carlos, 2023. Disponível em: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-27032023-153150/. Acesso em: 15 out. 2024.APA
Daud Filho, A. C. (2023). A tilt-wing VTOL UAV configuration study: flight dynamics modeling, simulation, states estimation, control, systems integration and flight testing (Tese (Doutorado). Universidade de São Paulo, São Carlos. Recuperado de https://www.teses.usp.br/teses/disponiveis/18/18161/tde-27032023-153150/NLM
Daud Filho AC. A tilt-wing VTOL UAV configuration study: flight dynamics modeling, simulation, states estimation, control, systems integration and flight testing [Internet]. 2023 ;[citado 2024 out. 15 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-27032023-153150/Vancouver
Daud Filho AC. A tilt-wing VTOL UAV configuration study: flight dynamics modeling, simulation, states estimation, control, systems integration and flight testing [Internet]. 2023 ;[citado 2024 out. 15 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-27032023-153150/