Individual with constant drive for Excellence on and off the field. An innate drive to understand, model/recreate, analyze, and improve natural (although nature delivers best) and man made processes. Extensive background in designing linear feedback control systems with focus on correct modeling of the physical phenomenon. A relentless researcher and avid learner!
Tutored undergraduate students
. Performed a role of technical team leader with diverse tasks ranging from development of Automated systems to augment production and Assembly of Aircraft to management and upkeep of Aircraft configuration.
. Excelled in Technical investigation of accidents by building data models and analyzing for lingering trends
. Designed and developed production processes for aircraft parts under the Indigenous Part Development program
. Worked on re-design of aircraft nose wheel steering system to assign variable gains for take off and taxi configurations
. Authored technical reports on Aircraft Spin Analysis using mathematical modeling, Failure Reporting and Corrective Action System (FRACAS), and Power Supply System analysis for load shedding in emergency situations
. Worked in collaboration with Chinese experts on recalibration of Aircraft Fuel system pressurization feedback mechanism to ensure inflight restart of the engine.
Studied aircraft design and proposed improvements particularly in Environmental Control System, Power Supply System, and Flight Control System
. Supervised and scheduled Maintenance of Aircraft inventory
. Conducted Technical investigations into aircraft and equipment accidents
. Lead a team of technicians performing O and I level maintenance on aircraft
. Developed 3D model of fighter aircraft using Photo-modeling technique for computational study in case of barrier engagement
After completion of my Course work, I am currently awaiting Final thesis defense. My research work encompasses mathematical modeling of slip stream effects on a flying wing configuration Micro Air Vehicle with respect to its effects on Stability and Control. I have used MATLAB to program a quasi steady state Vortex lattice Method with added propeller slip stream effects to correctly model the airflow over a flying wing. The results have been validated using flight test results for Cessna 172
I have been assigned teaching duties while awaiting final thesis defense
Data Analysis
undefined. Research Publication in AIAA Journal 2008 on 'Active Flow Control Using Dielectric Barrier Plasma Actuators'
. Poster Presentation in ICASE conference 2019 Islamabad Pakistan Titled 'Survey on active flow control using DBD Plasma Actuators'
. Thesis in hand titled 'Implementation of Stability Augmentation System on fixed wing Micro Aerial Vehicle under propeller effects in flying wing configuration'
. Conducted a technical investigation into a fighter aircraft accident (had been happening with recurring frequency for last 20 years) leading to highlighting of a common pilot error/design limitation of the aircraft. The accident of similar nature has not happened since Dec 2016
The research article covered detailed experimental work related to spatial distribution of added momentum using variable electrode geometry