Janapala Guna teja

• KC-46 Remote Vision Systems (RVS):

It provides situational awareness to operators for aerial refueling operations.

It contains three subsystems.

1. Sensor subsystems:

Panoramic Sensor LRUs.

Two Boom sensor LRUs.

2. Video Graphic Subsystems.

3. Display subsystems.

Roles:

Verification and validation.

Flow meter:

Role. LDRA test engineer.

Tools: Understand C, LDRA.

Client: Baker Hughes.

Responsibilities:

● Perform code reviews and static analysis using the LDRA tool according to MISRA C rules.

Performing instrumented and non-instrumented executions, and generating test reports for all major CSCIs.

Performing hardware and software integration testing.

Generating an instrumented build and Structural Coverage Analysis (SCA) for the code.

Generation of graphs of various outputs using the Simulink tool and analyzing those graphs.

Performing light gray box testing using LDRA Testbed.

Defence projects:

Role : verification and validation engineer

Tools: Understand C, LDRA TB Manager, unit, vision, MATLAB Simulink, DOORS.

Client: DRDO. (Defense Research Development Organization).

Project Overview: The ASM (Air to Surface) missile is an anti-radiation missile used for ground targets. ASM has different CSCIs, such as LC (launch computer), OBC (on-board computer), and MLP (missile launch pad). Flight control systems (FCS).

In this, I worked under MLP CSCI. MLP is used as an interface between LC and OBC. MLP performs health checks of all subsystems and sends them to LC. LC displays the status of all subsystems.

MLP performs pre-launch and auto-launch activities of missiles.

Role: Verification and Validation Engineer.

Tools: Understand C, LDRA TB manager, unit, vision.

Project Name: Enhanced Flight Vision System (EFVS) software.

Role: Tester

Tools: DB monitor, Golden image grabber, ALM, LDRA, DOORS.

Client : Elbit Systems (Israel)

Overview: The EFVS software is the software for the HUD computer unit (CU). Its purpose is to generate the required symbols and images to be displayed on the pilots' Head-Up Display, and the major functional purpose is to increase the pilot’s situational awareness in critical phases of flight and in terrain-constrained environments, maintaining the safety margin by staying ahead of the aircraft.

Responsibilities:

Developed high-level test cases and test procedures against high-level software requirements (SRS).

Black box testing and execution on a hardware target environment.

Performing instrumented and non-instrumented executions, and generating test reports for all major CSCIs.

Generating an instrumented build and Structural Coverage Analysis (SCA) for the code.

Involved in the review of test cases and test results in accordance with DO-178B Level A guidelines.

● Involved in high-level requirements, architecture, and low-level requirements reviews. Reporting the problems and clarification reports to the customer.