Modelling and Control of H-Shaped Racing Quadcopter With Tilting Propellers

Alkamachi, Ahmed; Erçelebi, Ergün

doi:10.22190/fume170203005a

Cited by 12 publications

(6 citation statements)

References 16 publications

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“…Several optimization methods are used to adjust the PID controller parameters used in the tri-copter. For example, grey wolf optimization is used in study [12], particle swarm optimization (PSO) is used in study [13], genetic algorithm is also implemented in that aspect in studies [14,15].…”

Section: Introductionmentioning

confidence: 99%

Design, Modeling, and Control of Tiltable Tri-Rotors UAV

Yahia,

Alkamachi

2024

JESA

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Section: Introductionmentioning

confidence: 99%

Design, Modeling, and Control of Tiltable Tri-Rotors UAV

Yahia,

Alkamachi

2024

JESA

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“…There is various version of quadcopter that had been developed found in research literature such as micro or nano sized quadcopter usually used in swarm and surveillance [1][2][3], aerial cinematography type, where the quadcopter able to lift a specific camera [4,5]. Moreover, there are also sport FPV H-type frame quadcopter where it specialized in racing [6,7].…”

Section: Introductionmentioning

confidence: 99%

“…The project focuses on modelling the DJI F450 quadcopter, and design the specific controller using PID. There are many types of control system method in controlling the altitude of the quadcopter based on these research [6][7][8][9][10][11][12]. The mathematical model of the quadcopter is derived from previous research and the DJI F450 frame parameter was embed into the model.…”

Section: Introductionmentioning

confidence: 99%

Modelling and PID control system integration for quadcopter DJI F450 attitude stabilization

Salma

Osman

2020

IJEECS

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<p><span style="font-family: Times New Roman;">In this paper we focus on the overall overview of the mathematical modelling of the DJI F450 UAV quadcopter, the hardware and software system integration based on PID control system for the attitude feedback. The parameter specification of the DJI F450 is fed into the mathematical model and implement a basic PID for the system. Future research using the DJI F450 model can benefit from this observation by implementing the modelling and tune in their own variable that varies, such as the overall of their weight. The data of PID control system simulation using the quadcopter frame model type DJI F450 parameter. The mathematical model for the quadcopter modelled DJI F450 is developed using Newton-Euler method. Altitude data for the control system is obtain from the analysis data of the Simulink simulation. The simulation is done using the Simulink toolbox inside the MATLAB software. From this paper, we can more understand the step involves in making a full control system of a quadcopter. The mathematical model for other type of quadcopter model can be implemented using the steps with their own parameter and achieve fast development.</span></p>

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“…Along with the widely used free or commercial computer codes for simulation of multibody systems, the dynamic models of a wide range of physical systems are formulated and studied by use of analytical [21][22][23] or numerical techniques. 24 Setting the mathematical model represents the very core of dynamic modeling of such type of systems composed of hydraulic and mechanical subsystems.…”

Section: Introductionmentioning

confidence: 99%

Numerical study of the hydraulic excavator overturning stability during performing lifting operations

Mitrev

Marinković

2019

Advances in Mechanical Engineering

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This article presents a numerical study of the stability of a hydraulic excavator during performing lifting operations. A planar dynamic model is developed with six degrees of freedom, which considers the base body elastic connection with the terrain, the front digging manipulator links, and the presence of the freely suspended payload. Differential equations describing the excavator dynamic behavior are obtained by using the Lagrange formalism. Numerical experiments are carried out to study the excavator dynamic stability under different operating conditions during the motion along a vertical straight-line trajectory. It is shown that the arising inertial loads during the movement of the links along the vertical trajectory, combined with the payload swinging and the motion of the base body, decreases the excavator stability. It was found that the excavator stability during following vertical straight-line trajectory decreases considerably in the lower part of the vertical trajectory. If the stability coefficient is close to 1, the payload swinging can cause the separation of a support from the terrain; nevertheless, the excavator stability can be restored. A method for tire stiffness and damping coefficients estimation is presented. The validation of the dynamical model is performed by the use of a smallscale elastically mounted manipulator.

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Modelling and Control of H-Shaped Racing Quadcopter With Tilting Propellers

Abstract: Abstract. Traditional quadcopter suffers terribly from its underactuation which implies

Cited by 12 publications

References 16 publications

Design, Modeling, and Control of Tiltable Tri-Rotors UAV

Design, Modeling, and Control of Tiltable Tri-Rotors UAV

Modelling and PID control system integration for quadcopter DJI F450 attitude stabilization

Numerical study of the hydraulic excavator overturning stability during performing lifting operations

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