Display and Graphics (D & G), TSC, V&V, Visual Basics, C and C++, TATS, EASE, PVCS, ASPIRE, JIRA, Verification and Validation Engineer, 8 months, Touch Screen Controller (TSC) is an interface to pilot, which will merge the functionality of different interface like MCDU (Multi-purpose Control Display Unit which will perform the functionality like loading flight plan, performance initialization), SMC (which will perform the function like engine oil display, hydraulic fluid display, window control like 2/3 window, full window) and Audio panel (it performs the function like tuning to frequency). TSC is display interface to pilot that uses graphics functionality to handle flight management system and provide user friendly environment to pilot. TSC is further divided to different process like TGF, TDL and TFM that handle graphics, datalink, and flight management process., Identifying the Strategy test plan and correspondingly Analysis of requirements from SRD, Test Development in the Simulated environment, To design the test case with all possibilities and outcomes., Test case execution and debugging., Host execution (Simulation of the test cases), Target execution., Raise bug on JIRA if any software issue is present. EFIS (Electronic Flight instrument system), Window 7, SIMULATOR TSO VISTA 7.41, Hardware and Software Integration Testing and System Testing, Verification and Validation Engineer, 3.9 years, EFIS (Electronic Flight instrument system) is a flight deck instrument display system in which the display technology used is electronic rather than electromechanical. Typical EFIS comprise of PFDs, MFDs, Navigation displays, Weather Radar and Radio communication display. EFIS is subset of FMS. Below are some of display I have worked so far. Weather Radar: This module deal with weather condition when aircraft on air state using many unidirectional and omnidirectional antennas. EICAS: Engine indication and crew alert system gives complete state of engine and its health to pilot. this system even gives detail relationship and impact of other systems like audio radio to engine. Autopilot: This system provides complete guidance for pilot for smooth and safe flight, this system takes input from other system and work co-ornately, Genesys aero system has made their certified autopilot and used by their own costumer., Identifying the Strategy test plan and correspondingly Analysis of requirements from SRD, Test Development in the Simulated environment, To design the test case with all possibilities and outcomes., Test case execution and debugging., Host execution (Simulation of the test cases), Target execution., Raise bug on JIRA if any software issue is present. Honeywell Aircraft Navigation and Communication Radios, Source Insight, HSS, Simics, DOORS, Code Composer, Visual Studio, Developer, C++ Programming, Hercules TMS570, 1.5 years, The Honeywell digital remote-mounted radio system encompasses all primary radio navigation and communication functions very high frequency (VHF) omni-directional receiver (VOR), automatic direction finder (ADF), distance measuring equipment (DME), instrument landing system (ILS), VHF communication radio into a single, easy to install system. The system also includes a digital audio system providing audio, interphone, and passenger address systems, improving the audio performance of the aircraft as well as the pilot’s overall comfort and workload., Involved Development for Honeywell’s KTR-2280 MMDR., Developing the Source code for the Low-Level Requirements., Extensively worked for Developing requirement documents., Debugging the fault log for the failure responses from hardware., Performing Developer test for the required functionality., Performing the Peer Reviews for code implemented., Performing Requirement Reviews with respect to Software standards and procedures. VHF Radio RTA50E, DeosTM Kernel, DOORS, Code Composer, Visual Studio, Borland C++, Atlassian JIRA, SCR Manager, Microsoft Compiler, Developer, C++/C/Assembly, T1024 Host Processor and TMS320C6652 Digital Signal Processor, 1.5 years (till now working), The VHF Data Link (VDL) Mode 2 radios support Controller Pilot Data Link Communications – sending information between aircraft and ground stations. The latest upgrade to the VHF data link communications has been the addition of Mode 2 data, or VDL Mode 2 capability. VDL Mode 2, in its broadest sense, is the term that is used to describe a suite of air-ground protocols that increase the data rate of the air-ground link to 31,500 bits per second. VDL Mode 2 allows transitioning from an infrastructure that relies on character-oriented ACARS protocols for end-to-end delivery of messages to one that uses bit-oriented Aeronautical Telecommunications Network (ATN) protocols using the same VHF ground and aircraft radios. The RTA-44D / 50D VDR systems are airborne VHF communications transceivers that provide voice and data communication between on-board aircraft systems, other aircraft systems, and ground-based systems. Each operates in analog DSB-AM analog voice mode, VHF ACARS data modes (Mode A and Mode 0), and VDL Mode 2 data mode. It also provides future support for VDL Mode 3 digital voice and data modes. The RTA-44D / 50D Mode 2 capability also supports the bit-oriented ATC applications such as Controller Pilot Data Link Communications (CPDLC) that rely on ATN infrastructure for end-to-end delivery of messages without a need for changes., Involved Development for Honeywell’s RTA50E VHF Radio., Developing the Source code for the Low-Level Requirements for Application Software., Extensively worked for Developing requirement documents., Debugging the fault log for the failure responses from hardware., Performing Developer test for the required functionality., Performing the Peer Reviews for code implemented., Performing Requirement Reviews with respect to Software standards and procedures., Performing Code Review as per coding standard and functionality