1. #56, 10th
‘A’ Main Road,
Ist Block Jayanagar,
Bangalore-560011
Mobile:-+91-9900103709
vasanth.tp82@gmail.com
T. P. Vasanth
CAREER OBJECTIVE
Seeking a career as a hardware engineer in a company that seeks an ambitious and
a career conscious person, where acquired skills and education will be utilized toward
continued growth and advancement.
SUMMARY
• 8 year of Experience in Development and Testing of various Avionics systems and
sub modules. Good knowledge of product development life cycle.
• Worked onsite at THALES (Brest, France) for three months from November 2012
to January 2013.
• Schematic designing in using Cadstar, Orcad and preparation of Part list.
• Coordinating with PCB designer providing relevant information such as
assembly, mechanical details etc.
• Developing Firmware for the sub modules using AT89cXX series of
microcontrollers.
• Preparation of ATP & ATR.
• Integration Testing of the system and offering it to the customer.
• Involved in Debugging and Enhancement of the existing projects.
• Involved in field trials of the system.
• Involved in production of the systems.
• Currently working on ARMDK-30 Tester of SU-30 Aircraft.
• Developed ATS for 8 power supply boards
• Developed ATS using DO254 standard
• Carrier board design for iMX6 SOM board.

2. EXPERIENCE
• 8 years of experience in hardware development & testing of Avionics Systems.
• Involved in hardware development and testing of Ground navigation systems. Good
knowledge of system integration and excellent trouble shooting electronics
circuits.
• Worked as an hardware engineer in Prudent Communication Systems from 11th
February 2008 to 20th
February 2012.
• Working as a Design engineer hardware in AvioHelitronics from 21st
February
2012.
• Worked onsite at THALES (Brest, France) for three months from November 2012
to January 2013.
SOFTWARE KNOWLEDGE
Programming Languages : C, C++.
Operating System : Windows.
Assembly Language : Microprocessors (8085, 8086), Microcontroller (8051)
Software tools : ORCAD, CADSTAR, AUTO CAD, QT
PROJECTS AT PRUDENT
1) Title: Commutated Aerial Direction Finder
Team size: 6
Duration: Feb 2008 to Jan 2009
Role: Involved in system level design starting from specification till field trials.
• Developed VHF and UHF Radio Module which would demodulate AM and FM
signals.
• Developed Oscillator Module which would generate LO signals to Radio
Modules.

3. • Developed Antenna switching unit.
• Developed Commutator Block which would switch between 16 diploes
positioned at an angular distance of 22.5 ° each covering totally 360°.
• Schematic diagram and part list preparation.
Description: CADF is an abbreviation for Commutated Aerial Direction Finder. It is used to
measure azimuthally direction of arriving aircraft. The RF signals used for communication
between aircraft and ATC tower in VHF and UHF band is used to find direction of aircraft.
2) Title: TACAN SPARES
Team size: 2
Duration: Feb 2009 to Dec 2010
Role: Developed plug-in cards for TACAN ground based system
• Developed synthesizer module which would generate frequency from
962MHz to 1213MHz.
• Developed Front End Unit which included Cavity filter and IF conversion.
• RF Interrogator which would simulate Aircraft signals locally to check the
system.
• Documentation of the above modules.
Description: TACAN stands for "Tactical Air Navigation" and is a system which,
working in the UHF band, between 962MHz to 1214MHz. TACAN system is used as one
of the navigational aids. With the help of TACAN transponder and Air borne equipment
pilot can continuous get information of range and angle of the aircraft. The airborne
equipment consists of an interrogating transmitter and a receiver which includes suitable
demodulating circuits to enable the information contained in the beacon's response to be
extracted.
3) Title: ILST SU30
Team size: 6
Duration: Jan 2010 to Jan 2011
Role: It was previously designed system for another Aircraft with slightly different
specification which had to be improved to suit SU-30 MKI.

4. • Developed digitally programmable variable attenuators which could go
from 0 to 120 dB.
• Manual and Bill of Material(BOM) preparation for production.
• Preparing Acceptance Test Procedure (ATP) and Acceptance test
Record (ATR).
• Involved in production, testing and validation of ILST SU30 Tester.
• Customer offering of the equipment as per ATP & ATR.
Description: The ILS/VOR SIMULATOR (ILST-SU30) Test set is intended to check the
accuracy of basic characteristics of ILS/VOR and Marker channels of multimode receivers of
SU-30 MKI Aircraft. ILST-SU30 tester will simulate localizer, glide slope, VOR, marker signals.
4) Title: ARMDK-30 Tester.
Team size: 2
Duration: Feb 2011 to July 2011
Role: This system was developed by Russians for testing SU-30 Engine parameters.
• Reading the manual and analyzing the system.
• Tracing circuit and preparing circuit diagram.
• Deriving the I/P specification from circuit analysis.
• Preparing test Jig which would simulate all the inputs required by the tester.
• Trouble shooting of ARMDK-30 tester for the reported problem, Fault Analysis
and repairing the unit.
Description: ARMDK-30 Tester is used to test Engine parameters of SU-30 Aircraft during
ground run. This tester shows all necessary data of Aircraft during ground run to know the
performance of Aircraft.
5) Title: RF Tracking System.
Team Size: 2
Duration: August 2011 to December 2011
Role: This is Radio receiver working from 350MHZ to 420MHz.

5. • Software development using embedded C.
• Integration testing.
• Validation of the equipment with respect to customer specification.
Description: RF Tracking system is a radio receiver works exactly as an ordinary radio.
This has a special feature called drift correction, the transmitting frequency is always warring and
receiver automatically locks to this varying transmitter frequency.
PROJECTS AT AvioHelitronics
1) Title: Engine monitoring system.
Team Size: 6
Duration: August 2012 to May 2012
Role: This system measures the parameters like Temperature, RPM, Pressure etc.
Description: This was a part of the project which was integrated in to AHRS system which was
developed by our company.
2) Title: ATS (Automated Test System)
Team Size: 20
Duration: from June 2012 to August 2014
Role: Design and development of ATS for eight power supply boards.
• Requirement analysis.
• COTS equipment selection.
• Design documentation.
• ITA (Interface test adapter) Design.
• Test procedure preparation which is an input for software development
Description: ATS design for eight power supply boards of different avionics systems.
These were DC to DC converters and AC to DC converters. The I/P’s to these power supply
boards are 270VDC, 42VDC, 135V400Hz (single phase), 135V400Hz (three phase).
3) Title: Autotest Module for BGH (Automated Test System)
Team Size: 20

6. Duration: from September 2014 to December 2014
Role: Design and development for Autotest Module for BGH (Generic Microwave bench).
• Component selection.
• Design documentation.
• Test procedure preparation which is an input for software development
Description: BGH is Gneric Microwave test bench developed by client for which we need to
build a test unit which will help us in performing the test of the bench and validate all the
instruments are correct and its connection are correct.
4) Title: DMM and IHH (Digital Moving Map and Integrated Head up and Head down
display)
Team Size: 15
Duration: from January 2015
Role: Design and development of Carrier board and Power supply board.
• Component selection.
• Schematic Design.
• BOM preparation.
• Assembling and testing of Boards.
• Design documentation.
Description: The Digital Moving Map (DMM) device is an electronic information
management (computing) device that helps pilot / flight crew to perform flight management tasks
(or tasks on board) efficiently. One of the purposes is to replace paper based reference material
and documentation used on a flight deck. It displays a variety of aviation data and performs basic
calculations (e.g., performance data, fuel calculations, etc.). The device provides flight crew with
display and state of art user-interface to access the functional capabilities of the DMM system.
This system shall comprise of Ground Processing Station (PC) and Airborne hand held device
called DMM device. Ground processing station configures DMM device and prepares for the
mission.
The Integrated Head Up and Head (IHH) down display is a dual mode visual display system
which includes a heads down display and a heads up display combined in a single unit which
provides primary flight display parameters to pilot. A flat panel AMLCD display attached to

7. housing in the front face serves as HDD, and an HUD display system which consists of LCD,
collimator and combiner for projecting HUD symbology.

8. PERSONAL DETAILS
FATHER’S NAME : Prabhudeva T M.
ADDRESS : #56, 10th
‘A’ Main Road 1st Block
Jayanagar, Bangalore-560011
Land line : (080) 26567239
SEX : Male
DATE-OF-BIRTH : 07-01-82.
NATIONALITY : Indian.
MARITAL STATUS : Married.
EDUCATION : B E in Telecommunication from Bangalore Institute of
Technology (BIT), VTU, Karnataka in 2006 with 60% marks.
DECLARATION:
I hereby declare that the above-mentioned particulars are
true to the best of my knowledge.
Place: Bangalore
Date: (T. P. VASANTH)