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Simulation and analysis of stability of UAV control system based on PID control under different wind forces
by
Hong, Kaibin
in
Algorithms
/ Control stability
/ Dynamic stability
/ Flight control systems
/ MATLAB/Simulink
/ Physics
/ PID control system
/ Proportional integral derivative
/ Rotors
/ Simulation
/ Stability analysis
/ Structural reliability
/ UAV flight control system
/ Unmanned aerial vehicles
/ Wind forces
/ wind interference
2023
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Simulation and analysis of stability of UAV control system based on PID control under different wind forces
by
Hong, Kaibin
in
Algorithms
/ Control stability
/ Dynamic stability
/ Flight control systems
/ MATLAB/Simulink
/ Physics
/ PID control system
/ Proportional integral derivative
/ Rotors
/ Simulation
/ Stability analysis
/ Structural reliability
/ UAV flight control system
/ Unmanned aerial vehicles
/ Wind forces
/ wind interference
2023
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Do you wish to request the book?
Simulation and analysis of stability of UAV control system based on PID control under different wind forces
by
Hong, Kaibin
in
Algorithms
/ Control stability
/ Dynamic stability
/ Flight control systems
/ MATLAB/Simulink
/ Physics
/ PID control system
/ Proportional integral derivative
/ Rotors
/ Simulation
/ Stability analysis
/ Structural reliability
/ UAV flight control system
/ Unmanned aerial vehicles
/ Wind forces
/ wind interference
2023
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Simulation and analysis of stability of UAV control system based on PID control under different wind forces
Journal Article
Simulation and analysis of stability of UAV control system based on PID control under different wind forces
2023
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Overview
The four-rotor UAV has attracted the attention of various fields and has been applied in more areas due to its advantages of low cost, high reliability and simple structure. Nowadays, more complex environment and interference factors put forward higher requirements for the accuracy and stability of the flight control system of UAV. At present, the most widely used four-rotor UAV flight control system is PID control system. This paper constructs a UAV control system based on PID algorithm to analyse and study the dynamic stability control effect of UAV under different wind impact scenarios. MATLAB is used to simulate and analyze the system, and the future development is expected according to the simulation results.
Publisher
IOP Publishing
Subject
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