Z-score-based Medium Frequency Pairs Trading Setup
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Trading System capable of reading the correlation between Nifty and BankNifty Implied Volatalities. Implementing XGBoost to predict the profit centers based on the time series data of their volatilities.
Based on Time Series Multivariate Trading strategy. Performing Statistical arbitrage with Nifty and BankNifty options.
Agricultural Predictive Insurance Modelling
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Focus has been on building predictive insurance models for agriculture. This involves deploying an ML model for comprehensive weather prediction using time-series data, to enhance weather forecasting to refine insurance rate predictions for the agricultural sector. Additionally, I am leveraging GeoSpatial data with QGIS and image processing to analyze crop and soil health for insurance risk assessment. The goal is to optimize premium adjustments based on real-time climate insights and the health of crops and soil.
Flight Simulator
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Flight Simulator Enhancement: We enhanced a flight simulator to address a 15% apogee discrepancy found in standard simulations. By integrating Barrowman equations with Computational Fluid Dynamics (CFD) analysis via PyFluent, our system now accurately predicts rocket trajectories and stability, overcoming the limitations of conventional models like OpenRocket. This allows for optimized rocket design considering real-world perturbations.
Ti/Te Investigation from MHD & hybrid models on CCMC
(Feb'25 – Apr'25)
Paper: Link
Multi-fluid sim: Utilizing SWMFv23 with MAGE on CCMC, figuring out limitations in resolving independent ion and electron energy equations within a global multi-fluid MHD framework—to backtrace Ti/Te spatial distributions across bow shock and magnetosheath domains.
Had to further investigate using HYPERS- hybrid model on CCMC. Downstream reconnection‐driven E∥J∥ heating reveals peak electron temperature excursions preceding ion maxima, with ΔTi - Te oscillations dominated by convective transport, evidencing cross‐species energy partitioning during shock events.
FAA Class II Solid Motor Sounding Rocket (@ SA Cup)
(Aug'20 – Jul'23)
Project Technical Report: Link
Built a Sounding Rocket targeting 10,000 ft. using a solid rocket motor capable
of reaching 0.9 Mach. Successfully launched it this year at Spaceport America,
USA. Dealt with exterior ballistics Design + Simulations, while coordinating
mechanical system designs with Avionics, mitigating design conflicts, and
harmonizing delivery timelines.
Developed a PID-controlled payload with real-time pitch correction and
integrated advanced avionics using dual-deployment altimetry and GPS tracking.
Built an SRAD FSW + Flight Simulator capable of predicting trajectory based
on design optimisation done via back-end CFD Simulation.
CANSAT 2022
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Built a Can-sized satellite shall consist of a container, which will descend a tethered payload to 10 meters in 20 seconds, while being attached to the container by a 10-meter-long tether.
The CanSat will be launched to an altitude ranging from 670 meters to 725 meters above the launch site and deployed near apogee to start descending using a parachute at a rate of 15 m/s, with the payload maintaining the orientation of a video camera pointing in the south direction, 45 degrees downward to assure terrain is in the video.
secured a personal best worldwide rank of 7th!
CANSAT GUI
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Designed to interact with an onboard flight computer in real-time. Its main objectives included receiving and displaying telemetry data, sending commands for tasks such as telemetry control and sensor calibration, and integrating various functionalities through Python's PyQt5 framework. The GUI utilized tools like Matplotlib for graphing, OpenStreetView Map with pyqtlet for mapping, and libraries such as csv, time, pyserial, paho-mqtt, and datetime for file generation, timing, serial communications, MQTT protocol integration, and UTC time setting, respectively.
CANSAT 2021
(Aug'20 – Jul'21)
Critical Design Review: Link
Simulated an atmospheric re-entry vehicle in the CANSAT mission with two
Maple Seed-inspired Monowing payloads for live telemetry; developed custom
SRAD Ground Control Software.
- Created and optimized a Mono-wing design using transient simulation for flow
analysis, employing a MATLAB script for maximum torque and efficiency.
CANSAT 2020
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mission was to design a delta wing glider capable of descending down from the container in a helical motion with a radius of 250 meters collecting sensor data for one minute and remain above 100 meters after being released. After which a parachute will deploy to bring down the glider at a rate of 10 m/s.
successfully completed the design of a delta wing glider with my team in the span of 1 month.
