Drone Altitude Control Using Proportional Integral Derivative Technique and Recycled Carbon Fiber Structure

Redha, Amenah E. Mohammed; Abduljabbar, Riyadh Bassil; Naghmash, Majid S.

doi:10.1007/978-3-030-82616-1_6

Cited by 2 publications

(1 citation statement)

References 22 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…For example, the small drone might fly in a strong, steady breeze and maintain its reference point by leaning into the wind at a given inclination. As a result, we should create a ground position controller that detects when the quadcopter deviates and makes the necessary adjustments to return it to its original X-Y coordinates [12]. Position inaccuracy is connected with roll and pitch motion due to the coupling of forward, backward, left, and right motions with roll and pitch procedures.…”

Section: The Architecture Of the Control System (Hovering Control)mentioning

confidence: 99%

Improving the Size of the Propellers of the Parrot Mini-Drone and an Impact Study on its Flight Controller System

Kadhim

Abdulsadda

2023

IJRCS

View full text Add to dashboard Cite

Unmanned Aerial Vehicles (UAVs) are widely used in transportation, delivery, surveillance and surveillance applications. The development of stable, resilient, and accurate flight based on turbulence and turbulence will likely become a key feature in the development of unique flight control systems. In this research, we studied the control system of a small Parrot mini drone, the Mambo drone, which was designed using the MATLAB program, while we added turbulence to the drone by changing the weight of the original plane in the design, where we increased the weight and calculated the vertical projection area of the propellers of the plane several times until we got the best space for the propellers able to carry more extra weight. We imposed an increase in the drone's weight due to bad conditions that the plane experienced during its flight, such as snow or dust falling on it. In order to make the aircraft bear these weather conditions without falling and colliding, we calculated an appropriate increase in the area of the aircraft wing, and we actually applied it in the MATLAB-R2021a Simulink program, and we got good results using simulation as well as in real-time inside the laboratory, turbulence was added in the simulation program. The new design of the propellers demonstrated the aircraft's ability to carry an additional payload of approximately one-third of the aircraft's weight, as shown in the roads chapter. In future work, we propose to use this design on larger aircraft with fixed propellers and to study the effects of other weather conditions on UAVs, such as the effect of temperature, humidity, and others.

show abstract

Section: The Architecture Of the Control System (Hovering Control)mentioning

confidence: 99%

Improving the Size of the Propellers of the Parrot Mini-Drone and an Impact Study on its Flight Controller System

Kadhim

Abdulsadda

2023

IJRCS

View full text Add to dashboard Cite

show abstract

Enhanced Nonlinear Control for Trajectory Tracking Control of a Quad-Copter System Using Redfox Algorithm

Mughees,

Ahmad,

Nawaz Jadoon

2024

IEEE Access

View full text Add to dashboard Cite

Drone Altitude Control Using Proportional Integral Derivative Technique and Recycled Carbon Fiber Structure

Cited by 2 publications

References 22 publications

Improving the Size of the Propellers of the Parrot Mini-Drone and an Impact Study on its Flight Controller System

Improving the Size of the Propellers of the Parrot Mini-Drone and an Impact Study on its Flight Controller System

Enhanced Nonlinear Control for Trajectory Tracking Control of a Quad-Copter System Using Redfox Algorithm

Contact Info

Product

Resources

About