Working on relay products :Relay is used to determine the current/volatge of the corresponding phasees , if the Current/volatge is excedding the setting ,relay has to trip the ckt and reclose the ckt once the fault is no more .its a 16 bit based Micrrocontroller appliaction , relay has the feature to communicate with SCADA using RS485 Communication protocol .It has the future to keep the settings permanently storing in eeprom by using i2C protocol .relay has divided into 2 parts HMI & measurement controller , HMI & measurement controller are communicated using SPI communication .Role: Developer.Responsibilities: writing and testing the code as per the requirement with adhering quality standards. Reviewing the code of others as per the requirement. Company:JVS Electronics2.organization: Honeywell Technology soln lab Years of exp:5.6 years Project: Displaying weather information in the Cockpit.Description: Uplink weather functionality used to display the weather information on Display Unit. Uplink software retrieve the Weather Data from the weather sensors via RS422 Driver & stores in the shared memory for each product(Lighting, storm,...),When Pilot requests for specific weather information, Uplink s/w will fetch the Data from shared memory & validates and then display on DU using Open GL libraries.; writng and testing the code as per the requirment with adhoring quality standards. Reviewung the code of others as per the requirment .

Taken care of regresrion testing for BGP componet of the cisco IOS .everyweek getting the cisco IOS release for the router .Doing the regression testing and repoting the test report to the Client.4.ADA:(10 months)As an S; Project: Onboard 1553B data acquisition software.Description: Light Combat Aircraft (LCA) uses the MIL-STD-1553B Aircraft internal time division command / response multiplex data bus for integrating the Avionics systems and subsystems. The communication between the Avionics Systems and subsystems will be available on MIL-STD-1553B bus. This MIL-STD-1553B data acquisition and recording unit is designed to acquire and store the data from both the busses available on Aircraft in real time for a minimum period of 90 minutes (approx.). The data collected by the interface board will be transferred to flash memory by the processor board. The data recorded is replayed to the ground-based retrieval system using TCP/IP (Ethernet) interface. The analyzed data is displayed in the graphical as well as in the text format for corresponding buses. In the graphical mode the parameters are plotted for their engineering values verses the time as well as one parameter verses other parameter.Responsibility: Implementing the requirement In C.Operating System: windows/DOSSkills: C, MIL - 1553B protocol.