A Dual-Fan Aircraft Use l-sOAT for Pitch control: Modelling and Simulation
- Resource Type
- Conference
- Authors
- Wang, JingHao; Teng, XiChao; Li, Zhang; Yu, QiFeng; Liu, XueCong
- Source
- 2022 International Symposium on Control Engineering and Robotics (ISCER) ISCER Control Engineering and Robotics (ISCER), 2022 International Symposium on. :111-117 Feb, 2022
- Subject
- Computing and Processing
Atmospheric modeling
Dynamics
Rotors
Stability analysis
Pitch control (position)
Vehicle dynamics
Aircraft
Control
sOAT
Bi-copter
UAV
- Language
In this paper, first an overview and explanation of the lateral single-axis Oblique Active Tilting (l-sOAT) control structure is presented. A complete dynamic model of vertical take-off and landing (VTOL) unmanned aerial vehicles (UAVs) having longitudinal rotor tilting mechanism is developed using a Newton-Euler formulation for l-sOAT mechanism. Then, a theoretical analysis of l-sOAT vehicle control response and stability for pitch motion is described and simulated using the derived dynamic model. The validity of the proposed structure and its dynamic model is verified by simulation experiments.