Research on Modeling of the Tilt Tri-rotor Unmanned Aerial Vehicle’s Dynamic

Abstract

Abstract. According to the basic principles of fixed-wing aircraft and multi-rotor design, combined with power requirement of the tilt tri-rotor UAV three flight modes, gives the tilt tri-rotor UAV power system model to solve the tilt tri-rotor UAV electric UAV power system matching problem, and to apply the theory completed a tilt tri-rotor UAV production, flight test was carried out to verify the theory. The experimental results analysis, tilt-rotor aircraft power system model in this paper can meet the general tilt rotor UAV power system design requirements. This achievement can provide theoretical references such UAV power system design.

Research on Innovative Trim Method for Tiltrotor Aircraft Take-Off Based on Genetic Algorithm

“…Tiltrotor aircraft which is capable of taking-off/landing vertically and cruise at high speed simultaneously combines the advantages of rotorcraft and fixed-wing aircraft. These characteristics make tiltrotor aircraft a research hotspot for recent years [1][2][3]. Tilt rotors provide the aircraft with the ability of vector tension, which not only expands its operating conditions but also entangles its flight control [4,5].…”