BRIJESH B V PRASAD

Howell – De Havilland Canada CL-415/CL-215T2 Amphibious Aircraft Retrofit EIS (Data Acquisition Unit)

• The EIS (Engine instrument system) consists of a Display Unit (DU), Engine Data Acquisition Unit(EDAU), Configuration Management Unit plus NVM, and Data Logging Unit.
• It will be complemented by a pilot input device and interconnecting harness.
• The EIS will interface with CL-415/CL-215T2 Amphibious Aircraft Retrofit engine sensors and other applicable aircraft systems.

Low-level requirements testing of Slat Flap Control Computer.

The Slat Flap Control Computer (SFCC) controls and monitors the slats and flaps. This is released by activation, control, and monitoring of the actuators, which move the slats and flaps. Each SFCC comprises one slat and one flap channel.

Responsibilities:

• Developed test procedure from low-level requirements.
• Developed test script from test procedure.
• Test execution using RTRT Weltest Tool, DOORS for requirement management.

Hardware, Software, and Testing of Network Interface Module.

The NIM is a component of the Guide and Restraint.

System (GRS) for the Airbus A400M aircraft. The A400M. The aircraft is capable of transporting and aerially delivering loads.

Responsibilities:

• Review of test cases and scripts generated for the requirements.
• Review of test results.

Howell – Engine Data Acquisition Unit of Bell, EDAU.

• The EIS (Engine instrument system) consists of a Display Unit (DU), Engine Data Acquisition Unit(EDAU), Configuration Management Unit plus NVM, and Data Logging Unit.
• It will be complemented by a pilot input device and interconnecting harness. The EIS will interface with Bell 412, 212, and 210 engine sensors, and other applicable aircraft systems.

Responsibilities:

• Testing high-level requirements of software using. Hardware equipment.
• Developed test procedure by referring SRS (Software Requirements Specification) document.
• Developed and executed test scripts on the hardware. And tested software developed by the client to ensure. That it met their requirements.

HIL Test of Flight Software.

HSIT Testing from DRDO ADE. IO and

Redundancy management testing.

Responsibilities:

• Testing high-level requirements of software using hardware equipment.
• Developed test procedure by referring to SRS.

(Software Requirements Specification) document.

• Used MATLAB software to execute the scripts.