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RESUME
NAME : Rajeshkanna V
Mobile no : +91-9611722422
E-mail : rajeshkannavg@gmail.com
OBJECTIVE
To pursue a challenging and innovative career in an organization that gives me the scope to
contribute my best and excel in the field through learning and experience.
Experience summary:
As a Software Engineer having 7+ years of experience in Avionics and Automotive domain:
 Good experience in Requirement and Simulink Matlab model based testing.
 Responsible for preparation and review of test cases and test procedure.
 Experience in Manual and Automation Testing.
 Experience in Configuration management tools- Serena PVCS Dimensions, SVN, PREP,
Rational Synergy, Rational Change, Clear Quest, Team track and Doors.
 Having experience in DO-178B standards.
 Having strong Analytical, Communication and Problem Solving Skills
 Proficient in developing the scripts using C# to automate the manual work.
 Involved in various stages of test life cycle like Writing and Executing test cases, test
procedures, code review, requirement review and Matlab model review.
 Good experience in Client Interaction and Support
Professional Experience :
 Presently working as a Assistant Manager with RNTBCI (Renault Nissan Technology &
Business centre India), Chennai from March 2015 to till date.
 Worked for 2.8 years as a Senior Engineer with UTC Aerospace Systems, Bangalore
from July 2012 to March 2015.
 Worked for 3.7 years as an Engineer with HCL Technologies Ltd, Bangalore from October
2008 to July 2012.
TECHNICAL SKILLS
Languages : C, C#.Net
Development Tools : Visual Studio 2005, MATLAB, SIMULINK, Lab view, NI Test
stand , PC Lint ,WinIdea, Seehau debugger & ATEasy,Reqtify
Configuration Tools : PVCS Dimensions, PREP, Doors, Team Track
Rational Synergy & Change, Clear Quest & SVN
CERTIFICATIONS:
 Microsoft Certified Professional in Windows Application(C#.net) and Web
Application(Asp.net)
 QAI E-learning Certification for “Basics of Software Engineering”.
 Completed the certification on ScrumMaster.
 Certified on ISTQB-Foundation Level.
PROJECT ACHIEVEMENTS:
 Recognized with “Appreciation Award “for the outstanding performance in the DS6000
projects for the Rockwell Collins Client in HCL Technologies.
 Recognized with "Spot Award" for taking ownership in performing Dry Runs for Pilatus
Safety of Flight milestone and executing them in UTC Aerospace systems.
Roles and Responsibilities:
 Responsible for developing Test Cases and Test Procedures as per requirements, SCR
and Simulink Matlab Model.
 Responsible for performing & managing the MIL( Matlab Model in Loop testing) validation
process.
 Performing Peer Reviews for test cases, test procedures and SCR.
 Performing Peer review for software requirements, SDD, Code and Matlab simulink
Model.
 Involved in the preparation of Software Verification Cases and Procedures (SVCP) and
supports the SOI#3 Audit.
 Involved in the Tool Qualification process for PC Lint tool. PC lint tool is used to detect
the MISRA Rule violation.
 Involved in Performing Structural Coverage Analysis(SCA) for the developed Test Scripts
with LDRA.
 Responsible for managing the projects for other pipe-line customers and for preparing the
Weekly Activity Report(WAR).
 Customer Orientation and Interaction in case of inconsistency in requirement/ target
machine.
 Leading a group of engineers in completing a module, additional responsibilities involve
technical support and work allocation.
 Involved in Technical Portal creation for the new joiners.
TOOLS DEVELOPED :
 Developed a Data and control coupling tool using C# and DXL scripts.
 Developed a SCA & Result Extraction Tool to track the result metrics of structural
coverage analysis & log files.
 Developed an Automation Work Allocation tool which extracts the reviewer name from
the concurrence checklists.
 Developed a Data type Validation tool which extracts the data type for all the signals
from the Matlab model implementation.
 Developed an Automatic TC Development tool which is used to create the test cases
automatically.
 Developed a segregation tool which is used to segregate the test procedure into different
folder for the batch execution.
 Used to develop the DXL scripts (Requirements and test case without linkage and
search for a string and retrieve with test case ID) to automate the manual work in
DOORS.
 Develop the excel-Macro to verify the Review checklist and for the comparison of “pair of
cells” in two different sheets.
PROJECT EXPERIENCE:
Project : IDFR (Ice Detector Family Redesign)
Client : Lear, Pilatus, Embraer, Bombardier.
Environment : iSystem Emulator, Hardware Target and enhanced test fixture.
Skill/Tools : Lab view, NI -Test Stand, I-System Debugger, Team Track, PVCS, SVN and
Doors.
Project Details:
The Ice Condition Detector is a one-piece, probe-type device designed to detect the
presence of icing conditions. It provides a signal correlating to ice accretion on aircraft surfaces.
When ice detector detects ice, it activates the anti-ice systems, signals the aircraft systems to
adjust the stall warning angles to compensate for the effect of ice accretion on the surfaces and
notifies on the Crew Alerting System (CAS).
Goodrich 0871 series Ice Detectors use a magnetostrictive technology to drive the sensing probe
to resonate at its natural frequency. As ice accretes on the probe, a shift in resonance frequency
occurs and an ice signal is activated when the frequency reaches the set point.
Project : SWAAT (Stall Warning Angle of Attack)
Client : Bombardier.
Environment : iSystem Emulator, Hardware Target and enhanced test fixture.
Skill/Tools : Seehau application, PVCS, SVN, Doors.
Project Details:
The function of the software is to provide stall warning functionality based on the AOA
vane position. It is also responsible for detecting hardware, software and stall system faults and
annunciating these faults over its output. The two major components of SWAAT are Angle of
Attack (AOA) vane assembly and the stall Warning Computer(SWC).The AOA Vane assemble
mechanically measures the local flow angles and provides aircraft AOA to the SWC. The SWAAT
interfaces with the aircraft through discrete and ARINC-429 inputs and outputs.
Project : RCI DS6000 Verification & Validation
Client Name : Rockwell Collins Inc.
Skill/Tools : Model Based Development Environment, Simulink, VAPS XT, Python
Scripting, DO-178B Level A and Level B Requirement, ARINC 429 protocol,
Doors, PVCS Dimensions, SVN, PREP, Clear Quest
Simulator : VISTA (Virtual Integrated Software Test Bed for Avionics)
Project Details:
The DS6000 Display Control System (DS6000-DCS) Verification activity involves
Requirements Based Testing and MCDC/Structural Coverage Analysis for the DS6000–DCS
software. The DCS applications are developed in accordance with RTCA DO-178B level A and B
development standards. The verification activities will be performed in accordance with RCI
provided standards, procedures, and plans to will meet the requirements of DO178B- Level A and
Level B. The Display and Crew Alerting system has interfaces to many systems within the overall
DS6000-DCS avionics system. ARINC661 is the primary interfaces between external applications
and displays.
Project : Braking and Antiskid Control System
Client Name : CRANE Aerospace and Electronics
Skill/Tools : ATEasy Framework, DO-178B Level A and Level B Requirement, Doors,
ARINC 429, AFDX, Doors, Rational Synergy and Rational Change.
Project Details:
The A400 Brake Control System Verification activity involves DO- 178B Level-A
Requirements Based Testing. The A400M Braking and Antiskid Control System will be an
advanced brake-by-wire system that will interface with the aircraft Integrated Modular Avionics
(IMA) architecture. The benefits of this system include optimum braking performance combined
with weight savings and excellent fault tolerance.
Project : Pneumatic System Controller
Client Name : Meggitt Control Systems
Role : Software Engineer
Skill/Tools : C, Matlab, DOORS, PVCS
Project Details:
Pneumatic System Controller will monitor sensor inputs and various system statuses and
apply these to control logic to determine the appropriate operational mode of the Pneumatic
System components. Regulating Valves will be continuously driven by the PSC to regulate the
pressure and temperature in the bleed manifold to values. Shut-Off Valves will be commanded
open or closed to redirect bleed air as needed by the system. The PSC will use ARINC 429 to
communicate with Avionics and with the Air Conditioning Controller (ACC). The PSC will transmit
complete status of all monitored components to the Avionics and will transmit monitored
temperature and pressure readings to the ACC.
EDUCATION QUALIFICATION:
B.E., Computer Science and Engineering, 2008
Bannari Amman Institute of Technology, Coimbatore, Tamil Nadu
Percentage: 75% with distinction
XII Standard, 2004
S.R.V Higher Secondary School, Namakkal, Tamil Nadu
Percentage: 87%
X Standard, 2002
Kandaswamy kandar Matriculation Higher Sec School, Namakkal, Tamil Nadu
Percentage: 81%
PERSONAL INFORMATION
Name : Rajeshkanna
Date of birth : 14th NOV 1986
Gender : Male
Languages : Tamil, English.
I hereby declare that above given information is true to the best of my knowledge.
Rajeshkanna V
open or closed to redirect bleed air as needed by the system. The PSC will use ARINC 429 to
communicate with Avionics and with the Air Conditioning Controller (ACC). The PSC will transmit
complete status of all monitored components to the Avionics and will transmit monitored
temperature and pressure readings to the ACC.
EDUCATION QUALIFICATION:
B.E., Computer Science and Engineering, 2008
Bannari Amman Institute of Technology, Coimbatore, Tamil Nadu
Percentage: 75% with distinction
XII Standard, 2004
S.R.V Higher Secondary School, Namakkal, Tamil Nadu
Percentage: 87%
X Standard, 2002
Kandaswamy kandar Matriculation Higher Sec School, Namakkal, Tamil Nadu
Percentage: 81%
PERSONAL INFORMATION
Name : Rajeshkanna
Date of birth : 14th NOV 1986
Gender : Male
Languages : Tamil, English.
I hereby declare that above given information is true to the best of my knowledge.
Rajeshkanna V

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Rajeshkanna_Resume

  • 1. RESUME NAME : Rajeshkanna V Mobile no : +91-9611722422 E-mail : rajeshkannavg@gmail.com OBJECTIVE To pursue a challenging and innovative career in an organization that gives me the scope to contribute my best and excel in the field through learning and experience. Experience summary: As a Software Engineer having 7+ years of experience in Avionics and Automotive domain:  Good experience in Requirement and Simulink Matlab model based testing.  Responsible for preparation and review of test cases and test procedure.  Experience in Manual and Automation Testing.  Experience in Configuration management tools- Serena PVCS Dimensions, SVN, PREP, Rational Synergy, Rational Change, Clear Quest, Team track and Doors.  Having experience in DO-178B standards.  Having strong Analytical, Communication and Problem Solving Skills  Proficient in developing the scripts using C# to automate the manual work.  Involved in various stages of test life cycle like Writing and Executing test cases, test procedures, code review, requirement review and Matlab model review.  Good experience in Client Interaction and Support Professional Experience :  Presently working as a Assistant Manager with RNTBCI (Renault Nissan Technology & Business centre India), Chennai from March 2015 to till date.  Worked for 2.8 years as a Senior Engineer with UTC Aerospace Systems, Bangalore from July 2012 to March 2015.  Worked for 3.7 years as an Engineer with HCL Technologies Ltd, Bangalore from October 2008 to July 2012. TECHNICAL SKILLS Languages : C, C#.Net Development Tools : Visual Studio 2005, MATLAB, SIMULINK, Lab view, NI Test stand , PC Lint ,WinIdea, Seehau debugger & ATEasy,Reqtify Configuration Tools : PVCS Dimensions, PREP, Doors, Team Track Rational Synergy & Change, Clear Quest & SVN
  • 2. CERTIFICATIONS:  Microsoft Certified Professional in Windows Application(C#.net) and Web Application(Asp.net)  QAI E-learning Certification for “Basics of Software Engineering”.  Completed the certification on ScrumMaster.  Certified on ISTQB-Foundation Level. PROJECT ACHIEVEMENTS:  Recognized with “Appreciation Award “for the outstanding performance in the DS6000 projects for the Rockwell Collins Client in HCL Technologies.  Recognized with "Spot Award" for taking ownership in performing Dry Runs for Pilatus Safety of Flight milestone and executing them in UTC Aerospace systems. Roles and Responsibilities:  Responsible for developing Test Cases and Test Procedures as per requirements, SCR and Simulink Matlab Model.  Responsible for performing & managing the MIL( Matlab Model in Loop testing) validation process.  Performing Peer Reviews for test cases, test procedures and SCR.  Performing Peer review for software requirements, SDD, Code and Matlab simulink Model.  Involved in the preparation of Software Verification Cases and Procedures (SVCP) and supports the SOI#3 Audit.  Involved in the Tool Qualification process for PC Lint tool. PC lint tool is used to detect the MISRA Rule violation.  Involved in Performing Structural Coverage Analysis(SCA) for the developed Test Scripts with LDRA.  Responsible for managing the projects for other pipe-line customers and for preparing the Weekly Activity Report(WAR).  Customer Orientation and Interaction in case of inconsistency in requirement/ target machine.  Leading a group of engineers in completing a module, additional responsibilities involve technical support and work allocation.  Involved in Technical Portal creation for the new joiners. TOOLS DEVELOPED :  Developed a Data and control coupling tool using C# and DXL scripts.  Developed a SCA & Result Extraction Tool to track the result metrics of structural coverage analysis & log files.
  • 3.  Developed an Automation Work Allocation tool which extracts the reviewer name from the concurrence checklists.  Developed a Data type Validation tool which extracts the data type for all the signals from the Matlab model implementation.  Developed an Automatic TC Development tool which is used to create the test cases automatically.  Developed a segregation tool which is used to segregate the test procedure into different folder for the batch execution.  Used to develop the DXL scripts (Requirements and test case without linkage and search for a string and retrieve with test case ID) to automate the manual work in DOORS.  Develop the excel-Macro to verify the Review checklist and for the comparison of “pair of cells” in two different sheets. PROJECT EXPERIENCE: Project : IDFR (Ice Detector Family Redesign) Client : Lear, Pilatus, Embraer, Bombardier. Environment : iSystem Emulator, Hardware Target and enhanced test fixture. Skill/Tools : Lab view, NI -Test Stand, I-System Debugger, Team Track, PVCS, SVN and Doors. Project Details: The Ice Condition Detector is a one-piece, probe-type device designed to detect the presence of icing conditions. It provides a signal correlating to ice accretion on aircraft surfaces. When ice detector detects ice, it activates the anti-ice systems, signals the aircraft systems to adjust the stall warning angles to compensate for the effect of ice accretion on the surfaces and notifies on the Crew Alerting System (CAS). Goodrich 0871 series Ice Detectors use a magnetostrictive technology to drive the sensing probe to resonate at its natural frequency. As ice accretes on the probe, a shift in resonance frequency occurs and an ice signal is activated when the frequency reaches the set point. Project : SWAAT (Stall Warning Angle of Attack) Client : Bombardier. Environment : iSystem Emulator, Hardware Target and enhanced test fixture. Skill/Tools : Seehau application, PVCS, SVN, Doors. Project Details: The function of the software is to provide stall warning functionality based on the AOA vane position. It is also responsible for detecting hardware, software and stall system faults and annunciating these faults over its output. The two major components of SWAAT are Angle of Attack (AOA) vane assembly and the stall Warning Computer(SWC).The AOA Vane assemble
  • 4. mechanically measures the local flow angles and provides aircraft AOA to the SWC. The SWAAT interfaces with the aircraft through discrete and ARINC-429 inputs and outputs. Project : RCI DS6000 Verification & Validation Client Name : Rockwell Collins Inc. Skill/Tools : Model Based Development Environment, Simulink, VAPS XT, Python Scripting, DO-178B Level A and Level B Requirement, ARINC 429 protocol, Doors, PVCS Dimensions, SVN, PREP, Clear Quest Simulator : VISTA (Virtual Integrated Software Test Bed for Avionics) Project Details: The DS6000 Display Control System (DS6000-DCS) Verification activity involves Requirements Based Testing and MCDC/Structural Coverage Analysis for the DS6000–DCS software. The DCS applications are developed in accordance with RTCA DO-178B level A and B development standards. The verification activities will be performed in accordance with RCI provided standards, procedures, and plans to will meet the requirements of DO178B- Level A and Level B. The Display and Crew Alerting system has interfaces to many systems within the overall DS6000-DCS avionics system. ARINC661 is the primary interfaces between external applications and displays. Project : Braking and Antiskid Control System Client Name : CRANE Aerospace and Electronics Skill/Tools : ATEasy Framework, DO-178B Level A and Level B Requirement, Doors, ARINC 429, AFDX, Doors, Rational Synergy and Rational Change. Project Details: The A400 Brake Control System Verification activity involves DO- 178B Level-A Requirements Based Testing. The A400M Braking and Antiskid Control System will be an advanced brake-by-wire system that will interface with the aircraft Integrated Modular Avionics (IMA) architecture. The benefits of this system include optimum braking performance combined with weight savings and excellent fault tolerance. Project : Pneumatic System Controller Client Name : Meggitt Control Systems Role : Software Engineer Skill/Tools : C, Matlab, DOORS, PVCS Project Details: Pneumatic System Controller will monitor sensor inputs and various system statuses and apply these to control logic to determine the appropriate operational mode of the Pneumatic System components. Regulating Valves will be continuously driven by the PSC to regulate the pressure and temperature in the bleed manifold to values. Shut-Off Valves will be commanded
  • 5. open or closed to redirect bleed air as needed by the system. The PSC will use ARINC 429 to communicate with Avionics and with the Air Conditioning Controller (ACC). The PSC will transmit complete status of all monitored components to the Avionics and will transmit monitored temperature and pressure readings to the ACC. EDUCATION QUALIFICATION: B.E., Computer Science and Engineering, 2008 Bannari Amman Institute of Technology, Coimbatore, Tamil Nadu Percentage: 75% with distinction XII Standard, 2004 S.R.V Higher Secondary School, Namakkal, Tamil Nadu Percentage: 87% X Standard, 2002 Kandaswamy kandar Matriculation Higher Sec School, Namakkal, Tamil Nadu Percentage: 81% PERSONAL INFORMATION Name : Rajeshkanna Date of birth : 14th NOV 1986 Gender : Male Languages : Tamil, English. I hereby declare that above given information is true to the best of my knowledge. Rajeshkanna V
  • 6. open or closed to redirect bleed air as needed by the system. The PSC will use ARINC 429 to communicate with Avionics and with the Air Conditioning Controller (ACC). The PSC will transmit complete status of all monitored components to the Avionics and will transmit monitored temperature and pressure readings to the ACC. EDUCATION QUALIFICATION: B.E., Computer Science and Engineering, 2008 Bannari Amman Institute of Technology, Coimbatore, Tamil Nadu Percentage: 75% with distinction XII Standard, 2004 S.R.V Higher Secondary School, Namakkal, Tamil Nadu Percentage: 87% X Standard, 2002 Kandaswamy kandar Matriculation Higher Sec School, Namakkal, Tamil Nadu Percentage: 81% PERSONAL INFORMATION Name : Rajeshkanna Date of birth : 14th NOV 1986 Gender : Male Languages : Tamil, English. I hereby declare that above given information is true to the best of my knowledge. Rajeshkanna V