Development of in-house drillstring dynamics model and field validation
Real time estimation of downhole parameters during drillstring
Estimation of along-drillstring friction factors across the well bore
Development of automated tool face control towards the realization of nan automated closed loop geo-steering system
Image Source: Wyoming State Geological Survey (public domain)
Predicting the onset of bit wear in rotary percussive drilling
Optimization of the drilling process in rotary percussive drilling with only the surface parameters
Developed a novel mathematical formulation to study the dynamics and stability characteristics of TDS
Designed a new model-order reduction technique for TDS
Increased the delay margin of the system with optimization-based and hybrid stabilization schemes
Experimentally validated the proposed theories using a rotary inverted pendulum, an inverted pendulum on a cart and a 3D-hovercraft
Applied the proposed schemes for studying human balance and supply chain models
Lead a feasibility study to demonstrate novel communications and optical imaging systems for small satellites
The team consisted 70 students across different majors from graduate and undergraduate levels
Divided the mission into sub-constellations of 4 satellites each with a primary goal to achieve cost optimization
Computationally validated control-system configurations especially for formation-flying in MATLAB
Supervised feasibility study for diffraction based optical system design
Developed a vibration Isolator for attenuating vibrations in the frequency range of 10 – 200 Hz (often referred to as μ–vibrations) for a target payload weight of 15 – 30 kg
Onboard vibrations affect the quality of the images obtained from optical payloads; therefore, it is imperative to isolate the payload from the onboard disturbances that come from various sources such as Reaction Wheel Assembly (RWA), Cryo–Cooler, etc
The developed vibration isolator was a passive vibration isolator consisting of viscoelastic materials
Lead an international team in a first of its kind feasibility study for a nanosatellite constellation
Analyzed the financial and schedule risks associated with the development of a nanosatellite constellation
Minimized the risk probability and achieved a 25% cost optimization against the proposed amount of $6 million
Recognized as one of the top works for the year 2011 at the Mission Idea Contest organized by the University of Tokyo and Axel Space Inc.
Executed the work at KAIST, South Korea
Founding team member of STUDSAT and team lead for designing the structures and mechanisms sub-system
STUDSAT – the first Indian pico-satellite (< 1 kg) launched in July 2010 was a venture of amateur undergraduate students
Performed static and dynamic analysis of the structure; and engineered the basic layout of various sub-systems
Validated the structural design from heat transfer point of view by performing static and transient thermal analysis so that all the components of STUDSAT are within the temperature limits
Devised a strategy to increase the Revenue Management Share (RMS) from the Value Added Services (VAS) from existing 12% to the 30% in a time period of 5 years
Analyzed the the VAS data and predicted the future growth for the RMS from VAS with appropriate recommendations for the company.
Developed a comprehensive system to provide the physical parameters (weight, the center of gravity & mass moment of inertia) of an airborne object with an accuracy of 20 microns
Experimentally validated the design of critical components of the system that support and absorb the dynamics of loads acting on the entire system
Characterized the TIFR – Near Infrared Camera, mounted on the telescope at Mt. Hanley, Ladakh
Obtained dark current of the CCD sensor and readout noise of the electronic circuit
Performed image processing using Interactive Data Language (IDL)
Analyzed the images obtained from using different filters attached to the sensor
Using the data collected, established the relationship of dark current and readout noise with the image