Review and current study on new approach using PID Active Force Control (PIDAFC) of twin rotor multi input multi output system (TRMS)

Meon, Mohd Suhairil; Mohamed, Tengku Luqman Tengku; Ramli, Mohd Hanif Mohd; Mohamed, M. Z.; Manan, Nor Fazli Adull

doi:10.1109/shuser.2012.6268848

Cited by 6 publications

(4 citation statements)

References 17 publications

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“…′ and ′ are measurable quantities that can be measured using a torque sensor and an accelerometer, respectively. As a DC motor was assumed as the actuator, equation (19) can be expressed as:…”

Section: Figure 4 Schematic Diagram Of the Afc Techniquementioning

confidence: 99%

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Practical Real-Time Implementation of a Disturbance Rejection Control Scheme for a Twin-Rotor Helicopter System Using Intelligent Active Force Control

2021

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Section: Figure 4 Schematic Diagram Of the Afc Techniquementioning

confidence: 99%

“…Regarding rotorcraft UAVs [18], some research works have been reported in [19] and [20], which combined the AFC strategy analytically with a PID controller to stabilize the 2-DOF helicopter model and compensate for the disturbances. The simulated results showed the effectiveness and robustness of the AFC-based technique.…”

Section: Introductionmentioning

confidence: 99%

Practical Real-Time Implementation of a Disturbance Rejection Control Scheme for a Twin-Rotor Helicopter System Using Intelligent Active Force Control

2021

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“…The basic idea of the AFC technique is the appropriate estimation of the mass/inertia parameter of the dynamical system and measurements of the acceleration and force/torque signals generated by the system as shown in Figure 13. Some research works have been reported in [176], [177] that analytically utilized the AFC-based technique with a PID controller to control the TRMS model and compensate for the applied disturbances. The works presented a comparative study of system performance by analyzing the output responses based on PID-AFC, PID-AFC-ANN, and PID-AFC-FL schemes.…”

Section: External Disturbancesmentioning

confidence: 99%

Control Strategies and Novel Techniques for Autonomous Rotorcraft Unmanned Aerial Vehicles: A Review

2020

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This paper presents a review of the various control strategies that have been conducted to address and resolve several challenges for a particular category of unmanned aerial vehicles (UAVs), the emphasis of which is on the rotorcraft or rotary-wing systems. Initially, a brief overview of the important relevant definitions, configurations, components, advantages/disadvantages, and applications of the UAVs is first introduced in general, encompassing a wide spectrum of the flying machines. Subsequently, the focus is more on the two most common and versatile rotorcraft UAVs, namely, the twin-rotor and quadrotor systems. Starting with a brief background on the dual-rotor helicopter and a quadcopter, the full detailed mathematical dynamic model of each system is derived based on the Euler-Lagrange and Newton-Euler methods, considering a number of assumptions and considerations. Then, a state-of-the-art review of the diverse control strategies for controlling the rotorcraft systems with conceivable solutions when the systems are subjected to the different impediments is demonstrated. To counter some of these limitations and adverse operating/loading conditions in the UAVs, several innovative control techniques are particularly highlighted, and their performance are duly analyzed, discussed, and compared. The applied control techniques are deemed to produce a useful contribution to their successful implementation in the wake of varied constraints and demanding environments that result in a degree of robustness and efficacy. Some of the off-the-shelf developments in the rotorcraft systems for research and commercial applications are also presented.

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“…However, manual tuning of the PID controller requires a greater human effort which is a major drawback. In [6], Meon M.S. proposed a PID active force control method which estimated the external torque disturbances and used soft computing techniques to optimize the PID response.…”

Section: Introductionmentioning

confidence: 99%

Robust Optimal Sliding Mode Control of Twin Rotor MIMO System

Chithra¹,

Thomas²

2016

IJERT

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The twin rotor MIMO system is a laboratory setup resembling the dynamics of a helicopter. It is a complicated non linear system with heavy cross coupling effects between the propellers commonly used for verification of control methods and observers. In this paper the robustness and tracking capabilities of the decoupled system are evaluated and compared using PID controllers, LQI controller and a robust optimal controller. It was observed that the robust optimal controller exhibited superior performance to the output feedback and optimal controllers.

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Review and current study on new approach using PID Active Force Control (PIDAFC) of twin rotor multi input multi output system (TRMS)

Cited by 6 publications

References 17 publications

Practical Real-Time Implementation of a Disturbance Rejection Control Scheme for a Twin-Rotor Helicopter System Using Intelligent Active Force Control

Practical Real-Time Implementation of a Disturbance Rejection Control Scheme for a Twin-Rotor Helicopter System Using Intelligent Active Force Control

Control Strategies and Novel Techniques for Autonomous Rotorcraft Unmanned Aerial Vehicles: A Review

Robust Optimal Sliding Mode Control of Twin Rotor MIMO System

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