Project Experience 1:
B787 – Integrated Flight Control system
Aug 2008 – Till Date
Honeywell Tech. Solutions, Bangalore, India
VALFAC, DFTS, FTD,SSL,VALDOC, HSS
Description of the Project:
The B787 IFCS has three sub-functions such as Primary flight Control Function, High Lift Function and Auto flight Function. The PFCF directly controls the elevator, stabilizer, rudder, spoiler, flaperon, and aileron surfaces. The HLF is used to increase the wing camber for takeoffs and landings and to improve stall characteristics. The wing camber is increased by extending the slats and/or flaps. The AFF provides functions necessary for the automatic control and/or flight director guidance of the 787 airplane to selected flight path and airspeed targets.
·Define technical integration strategy, Develop Integration Plans, Develop integration test scripts, Develop and implement integration test scenarios, conduct and document integration tests, Track integration test results and retest status
·Technical Lead for System Test Procedures Testing Team (STP)
·Coordinate with Onsite team and offsite team for smooth execution.
·Key Member in VALFAC Setup and Soft Bench setup
·Plan and develop New SYS-TPP for the newly added Requirements.
·Competency development drive in AFCS – Regular weekly discussion