My current research is focused on the development of advanced guidance, navigation, and control systems for fully actuated unmanned aerial vehicles (UAVs) that can interact with structures at high altitudes. The aim of this research is to address the complexities and uncertainties that arise when controlling UAVs in contact with structures. To achieve this goal, the use of a tiltrotor configuration is considered, which allows for full actuation of the platform. The ultimate objective of this… Show more My current research is focused on the development of advanced guidance, navigation, and control systems for fully actuated unmanned aerial vehicles (UAVs) that can interact with structures at high altitudes. The aim of this research is to address the complexities and uncertainties that arise when controlling UAVs in contact with structures. To achieve this goal, the use of a tiltrotor configuration is considered, which allows for full actuation of the platform. The ultimate objective of this research is to enable safe and efficient operation of fully actuated UAVs in complex environments, thereby creating new opportunities for both industrial and societal applications. Show less

A methodology for identifying the wake dynamics of a cylinder was developed by constructing a reduced-order model from time-resolved flow data obtained through PIV measurements at Reynolds 1000. The resulting Galerkin model incorporates mathematical constraints, providing a more comprehensive understanding of the flow physics underlying the system. This approach represents a significant contribution to the field, as it enables the exploration of the fundamental dynamics of fluid flow in a novel… Show more A methodology for identifying the wake dynamics of a cylinder was developed by constructing a reduced-order model from time-resolved flow data obtained through PIV measurements at Reynolds 1000. The resulting Galerkin model incorporates mathematical constraints, providing a more comprehensive understanding of the flow physics underlying the system. This approach represents a significant contribution to the field, as it enables the exploration of the fundamental dynamics of fluid flow in a novel way and has the potential to facilitate the development of more precise models for predicting the behavior of similar nonlinear dynamic systems. Show less

The project titled "Control of Air Conditioning System with Large Hysteresis" is my master's research project with the aim of modeling and control of nonlinear systems. Initially, the system is analyzed by defining the mathematical hysteresis model and validated by verifying the numerical consistency. Later, the inverse model is developed to establish the feedforward control mechanism in Matlab Simulink. Now currently working to develop the state-space model of the nonlinear system by studying… Show more The project titled "Control of Air Conditioning System with Large Hysteresis" is my master's research project with the aim of modeling and control of nonlinear systems. Initially, the system is analyzed by defining the mathematical hysteresis model and validated by verifying the numerical consistency. Later, the inverse model is developed to establish the feedforward control mechanism in Matlab Simulink. Now currently working to develop the state-space model of the nonlinear system by studying the system with the help of system identification and evaluation toolbox. Show less

The project entitled "Analysis and Control of Flow-field in a Dual Mode Ramjet engine" is my bachelor's thesis project under Dr. Amit Thakur. In this project, the 2D RANS CFD simulation of a DMRJ engine in non-reacting, Ramjet, and Scramjet modes of operation using Ansys Fluent module is carried out. Analysis of combustion modes and validation of results were performed. Active flow control method was also enforced.

Worked in the field of Vibration under Dr. C. V. Chandrashekara on the defective simple structures extensively using MATLAB software analytically, then simulated using ANSYS Modal analysis and finally validated results using Siemens LMS TestLab software (Impact Module). Various dynamic characteristics of the beam are studied demonstrating the effectiveness of the defect in the structure.