Trim Strategy, Control Model, and Flight Dynamics Characteristics of Canard Rotor/Wing Aircraft in Transition Mode
The transition mode of canard rotor/wing (CRW) aircraft is complex and important. During the transition flight, components that generate lift are transferred from one to another, in addition, the redundancy of control system may induce control conflict even plane crash if they don't cooperate w...
Main Authors: | Honggang Gao, Zhenghong Gao, Yang Na, Chao Pang |
---|---|
Format: | Article |
Language: | English |
Published: |
IEEE
2019-01-01
|
Series: | IEEE Access |
Subjects: | |
Online Access: | https://ieeexplore.ieee.org/document/8716669/ |
Similar Items
-
Vortex Dynamics Study and Flow Visualization on Aircraft Model with Different Canard Configurations
by: Setyawan Bekti Wibowo, et al.
Published: (2021-04-01) -
Parametric Investigation of Canards on a Flying Wing UAV Using the Taguchi Method
by: Stavros Kapsalis, et al.
Published: (2023-03-01) -
Low-Boom Design for Supersonic Transport with Canard and Forward-Swept Wings Using Equivalent Area Design Method
by: Yuki Kishi, et al.
Published: (2023-08-01) -
Design of Variable Amplitude Flapping Wing Aircraft and Realization of Multiple Flight Modes
by: Yueyang Hou, et al.
Published: (2021-01-01) -
Numerical Investigation of the Rotor-Rotor Aerodynamic Interaction for eVTOL Aircraft Configurations
by: Riccardo Piccinini, et al.
Published: (2020-11-01)