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Controller Power Supply

Location:
Tirupur, Tamil Nadu, India
Salary:
30,000rs
Posted:
March 25, 2022

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Resume:

CURRICULUM VITAE

Vinodhini.B

D/O,Baskaran.A,

No.29/6,51,Gurusadi Street,

Vadagarai, Periyakulam,

Theni-625601.

Mobile: 915-***-****

Email:- adqldl@r.postjobfree.com

OBJECTIVE:-

To build a career that offers challenge and growth with opportunities to enrich my knowledge and skills while contributing my best to the organization I work for.

ACADEMIC RECORD:-

CLASS / COURSE

NAME OF THE

INSTITUTION

BOARD OF STUDY

YEAR OF PASSING

CGPA /

MARKS%

M.TECH

(C&I)

THIAGARAJAR COLLEGE OF ENGINEERING, MADURAI

ANNA UNIVERSITY

2017

71

B.E

( EEE )

PSNA CET, DINDUGAL

ANNA UNIVERSITY

2014

81.7

XII

T.K.M.S, THENI

TAMILNADU MATRICULATION BOARD

2010

71.9

X

S.R.V.M.S, THENI

TAMILNADU MATRICULATION BOARD

2008

79.5

PROJECT EXPERIENCE:-

Analysis and Implementation of Load Resonant Converter for Constant Current power Supply TEAM SIZE: (UG)

A prototype dc-to-dc energy converter circuit with the loaded-resonant converter was designed for a load and the Energy conversion efficiency of the proposed loaded-resonant topology reaches up to 88.3% had proved . Moreover, testing results were satisfied the performance of the proposed topology.

MRAC Based LQI Control Of 2-DOF Helicopter:(PG)

Helicopters are used where difficult manoeuvres are required. They are more versatile and can take-off and land without a runway. Helicopter is a multi-input multi-output system (MIMO) and highly coupled Non-linear system. So, control of helicopter is a challenging task. Automatic stabilization and control of helicopter is a challenging problem in research.

Since, Helicopter is highly non-linear. Usual practice is to linearized system and design controller for linear operating point. When non-linear is similar, the performance of the controller is questionable. Hence, Adaptive controller is used to adopt the controller gains based on operating point.

In this thesis, MRAC based LQI is implemented for an experimental Two Input Two Out Helicopter model. Effectiveness of the proposed controller is verified by simulation and hardware results and the results are presented. Obtained results indicate, that the MRAC based LQI is able to eliminate the steady state error in all operating points while achieving dynamics comparable to that of MRAC based LQR.

APPRENTICESHIP TRAINING :

·Gone for Graduate Apprenticeship training for a year(April2014-April2015)in

TNEB,Theni Circle

CO-CIRICULLAR ACTIVITIES:

•Won First prize in the ELECTRICAL DEBUGGING event conducted by PSNA college of engineering and technology.

•Participated in the Software contest’12 conducted by the department association.

•Participated in the C Debugging contest’12conducted by the department association.

LEADERSHIP INITIATIVES:

•Holding the position of Class Representative in B.E(UG)

HOBBIES:

•Surfing the INTERNET.

•Playing Chess.

COMPUTER ADROITS:

Language :-Basics of C,C++

Assembly language :-Microcontroller

Technical Package :-MATLAB,Keil u vision,PROTEUS,Logix pro

Platform :-Windows XP, Windows 7.

PERSONAL PROFILE:-

Date Of Birth :-14.12.1992

Age :-25

Sex :-Female

Father’S Name :-Baskaran.A

Mother Tongue :-Tamil

Languages

Read :- English,Tamil, Hindi

Write :- English,Tamil, Hindi

Speak :- English,Tamil

I, VINODHINI.B, do hereby confirm that the information given above is true to the best of my knowledge.

Signature:

Date:22.10.2018

Place: PERIYKULAM (VINODHINI. B)



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