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Les dernières missions DATA DICTIONARY à pourvoir

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Développeur ABAP FIORI SAPUI5

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Consultant SAP

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CONSULTANT EXPERT SAP

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34 - MONTPELLIER
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Consultant SAP ABAP FIORI

SAP ABAP SAP FIORI
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95
120 jours ouvrés
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Consultant Technico-fonctionnel SAP MM/SD

SAP MM SAP SD SAP ABAP ABAP
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Commercialisation d'un générateur de programmes SAP ABAP (contrat d'apporteur d'affaires)

SAP ABAP SAP NETWEAVER SAP ABAP SAP ECC
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Administrateur SAP BC - Toulouse - F/H

SAP SAP BC SAP HANA SAP ABAP
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Développeur SAP ABAP

SAP ABAP SAP ECC
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1 mois
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Développeur ABAP (SAP ISU)

SAP ABAP SAP IS-U
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92 - La Défense
6 mois
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Exemple d'expériences de Vaishali,
freelance DATA DICTIONARY résidant dans les Hauts-de-Seine (92)

  • Role: Technical Lead

    Global 7000/8000 Flight Control System Remote Electronics Unit (REU) Client: Bombardier
    Jan 2017 - Jan 2018

    Description:

    The principle functions of the REU are to provide closed loop control of the Aileron, Elevator, Rudder, and Multi-function Spoiler. The REU also provides ancillary functions such as fault monitoring, status; maintenance support, rigging, and stabilizer trim control (via MCE).
    The Command Lane CSCIs are embedded within the Analog Devices ADSP-21469 Digital Signal Processor (DSP) in the Command Lane. The Monitor Lane CSCIs are embedded within the TMS320F28335 DSP in the Monitor Lane.
    Each lane processes independent sensor inputs and provides independent control of the actuators.For the REU, a Command / Monitor architecture is being implemented to address safety and redundancy. The architecture will mitigate un-commanded or erroneous surface commands. The Command Lane and Monitor Lane will perform the same calculations. The dissimilar hardware architectures for Command and Monitor Lane DSPs and dissimilar processor specific tool chain will mitigate common mode failures.

    Responsibilities:

    Technical:
    • Responsible for creating the problem Report for development issues.
    • Responsible for analysis of the problem Report and provided the Proposed solution for the problem.
    • Involved in implementation and verification of Problem Report.
    • Involved in writing the Software Requirements Specification (SWRS), software design document (SWDD), Data dictionary, Interface Control Document (ICD) documents.
    • Involved in code and requirement reviews (SWRS, SWDD, Data dictionary, ICD).
    • Responsible for updating the daily basis status to customer and presenting the status in customer call.
    • Responsible for addressing customer review comments and provided disposition for the comments.
    • Responsible to work with customer QA for review of problem report and clarified all the doubts raised by QA.

    Project Management:
    • Estimation/Allocation/Tracking of work.
    • Creating day to day schedules and work assignments for team.
    • Periodic reporting of project status/health check to internal stakeholders
    • Timely escalation/communication on issues

  • Role: Technical Lead

    Common Software Architecture Client: UTAS
    Jan 2015 - Jan 2016

    Description:
    The Common Software Architecture (CSA) form the common platform on which the application code of products can execute. The CSA provides a structure that covers different functions that were considered common among the products. Each product will have the flexibility to add more tests and utilities that are unique to their product. The combination of the CSA and product created utilities components make up the Service Platform on which the application software can execute. Each RSC offers a configuration table with a set of configuration data. The integrator will configure the service platform components via the Configuration Data for RSC performing a product’s requirements.

    The Computer software architecture (CSA) includes the following CSCIs:

    • BOOT: provides the initial reset control of the micro-board & handle the initial startup and download capabilities.
    • Test Link: provides the test link communications to an external test link tool. Ie., Transfer of data to and from the Unit.
    • System Services: provides the hardware interface and common functions required for the CEI common hardware design.
    • Operating System: provides the periodic scheduling of tasks and the mechanism to communicate data between the tasks.

    Responsibilities:

    • Involved in writing Software Requirements Specification (SRS), Software Design Documents (SDD), Interface Requirements Specifications (IRS) documents.
    • Involved in code and requirement reviews (SRS, SWDD, IRS)
    • Responsible for verification process standardization w.r.t templates, documents.
    • Responsible for Installing, configuration of the test target hardware.

  • Role: SQA

    Aero Product Excellence Group (APEG) Client: UTAS
    Jan 2014 - 2015

    Responsibilities

    • Performed work product sample review for development and verification and validation projects as per
    DO-178B/C.
    • Performed In-process audit for complete SDLC.
    • Performed transition, configuration management and CR audits.
    • Performed thread audit as per FAA JOB Aid checklists.
    • Supported PRE and formal SOI2 and SOI3 audits.
    • Actively participated in Casual analysis and preventive action meetings for defect analysis.

  • As Senior Engineer

    Trigent Software Ltd, Bangalore
    Jan 2014 - Jan 2014

  • Role: Team Lead Team Size: 8

    Aircraft: Embraer-170 (E170)Product: Next Generation Flight Management System (FMS)
    Jan 2014 - Jan 2014

    Employer: Trigent Software Ltd

    Responsibilities

    Project Management:
    • Estimation/Allocation/Tracking of work
    • Creating day to day schedules and work assignments for team
    • Periodic reporting of project status/health check to internal stakeholders
    • Timely escalation/communication on issues

    Technical:
    • Performed High level, low level software requirements review for testability of Scenario Management, Sensor Proxy Management.
    • Test Strategy, Requirements review, test reviews, QA activities
    • Responsible for planning and executing of unit, integration, system level and functional testing on windows platforms based on design, requirement specifications.
    • Responsible for test design, test case development, test execution, test debugging, test configuration, test documentation, test tracing, test reviews and defect tracking for one or more functional area’s
    • Responsible for troubleshooting software and hardware test environment for manual and automated test.
    • Responsible to work with developers to reproduce problems and get them resolved
    • Work on continuous improvements.

  • Role: Software Test Team Lead Team Size: 6

    Aircraft: Embraer-170 (E170)Product: Next Generation Flight Management System (FMS)
    Jan 2012 - Jan 2013

    Employer: Honeywell

    Responsibilities

    Project Management:
    • Estimation/Allocation/Tracking of work
    • Creating day to day schedules and work assignments for team
    • Periodic reporting of project status/health check to internal stakeholders
    • Timely escalation/communication on issues

    Technical:
    • Responsible for process standardization w.r.t templates, documents.
    • Performed High level, low level software requirements review for testability of Platform, Database, Framework, Navigation, Flight plan, Guidance, Trajectory, User Interface functionalities
    • Test Strategy, Requirements review, test reviews, QA activities
    • Responsible for planning and executing of unit, integration, system level and functional testing on windows and Wind River platforms based on design, requirement specifications.
    • Responsible for test design, test case development, test execution, test debugging, test configuration, test documentation, test tracing, test reviews and defect tracking for one or more functional area’s
    • Responsible for Installing, configuration of the test target hardware
    • Responsible for troubleshooting software and hardware test environment for manual and automated test.
    • Responsible to work with developers to reproduce problems and get them resolved
    • Work on continuous improvements.

    Aircraft: Gulfstream (G650)
    Product: Next Generation Flight ...

  • Honeywell Technology Solution, Bangalore

    As Senior Engineer
    Jan 2010 - Jan 2013

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