Model predictive control of TRMS

Harshath, K.; Manoharan, P. S.; Varatharajan, M.

doi:10.1109/pestse.2016.7516455

Cited by 10 publications

(4 citation statements)

References 3 publications

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“…The mathematical model of the 2-DOF helicopter model was derived according to work done in [23]. The 2-DOF helicopter platform is shown in Figure 1, where it was derived based on the following assumptions [1]:…”

Section: -Dof Helicopter System Modelingmentioning

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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Section: -Dof Helicopter System Modelingmentioning

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 torques generated at the pitch and yaw axes are a function of the voltages applied to the motors [23], The generalized forces vector is given by [23]:…”

Section: -Dof Helicopter Modelingmentioning

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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“…The system presented in [3] works by using hand gestures as input. It first detects and pre-processes the image of the hand [4][5][6], and then crops it to the necessary size for analysis. The features of the hand are extracted and classified, and finally, the gesture is converted into speech.…”

Section: Introductionmentioning

confidence: 99%

Control System Based on Hand Gesture Recognition Using Mems Accelerometers

Manoharan,

Kumar,

Indhumathi

et al. 2023

IJEAST

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This paper aims to propose a methodology to assist individuals with physical disabilities by utilizing MEMS technology. This technology can be used to help non-verbal people communicate without words or assist those with partial paralysis to control their surroundings. The gesture identification is achieved using MEMS accelerometers. When a gesture is made, the accelerometers register the movement, which is then interpreted by a microcontroller. The microcontroller recognizes the gesture by comparing it to pre-programmed signals and assigns it a unique code. Additionally, there is a control module that includes an RF receiver. The RF receiver can detect the unique code from the user module. The ATMEGA microcontroller used in the control module to trigger specific functions based on the user's preferences and requirements. The proposed model is implemented in real time under various testing conditions.

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Model predictive control of TRMS

Cited by 10 publications

References 3 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

Control System Based on Hand Gesture Recognition Using Mems Accelerometers

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