This paper designs a tail-sitter UAV that combines the advantages of a fixed-wing UAV and a rotary-wing UAV. Based on the designed model, a study that the attitude of the moving-mass UAV under the different conditions of the moving load in the horizontal cruise phase is carried out. The results show that the stability of the flight attitude of the whole aircraft in the cruise phase is verified. And the study is essential to ensure the safety of the whole tail-sitter UAV.
Research on pitch angle control of a small moving-mass tail-sitter UAV with moving load
Ninth International Conference on Mechanical Engineering, Materials, and Automation Technology (MMEAT 2023) ; 2023 ; Dalian, China
Proc. SPIE ; 12801
2023-10-25
Aufsatz (Konferenz)
Elektronische Ressource
Englisch