200 mobile robot agents, or as we call them, 'Jonny bots' welcome you to this page

Hey there, I’m Ayaz, an aerospace engineer who loves tinkering with cool gadgets and software in the world of controls, robotics, and autonomous systems. I am pursuing a Master’s in Aeronautics and Astronautics from the University of Washington and earned my stripes in Aerospace Engineering from the Indian Institute of Space Science and Technology. For more than five years, I worked at the Vikram Sarabhai Space Centre, Indian Space Research Organization, where I’ve had a blast playing with MATLAB, Simulink, Python, C++, and Julia to figure out how things fly in space. From analyzing spacecraft orbits to creating nifty models, I’m all about pushing the boundaries in aerospace tech and finding smart solutions with a bunch of awesome folks.

Download my CV.

Interests
  • Motion Planning
  • Control and Autonomous Systems
  • Robotics and Mechatronics
  • Numerical Modeling and Simulation
Education
  • MS in Aeronautics and Astronautics (Controls), 2025 (Expected)

    University of Washington

  • B.Tech in Aerospace Engineering, 2018

    Indian Institute of Space Science and Technology

Skills

Analysis Packages and Coding Languages
Python, MATLAB, Simulink, C++, Julia
Solidworks, CATIA, AutoCAD, Fusion360
Adams, ANSYS, Fluent
Hands-On
Robot Operating System (ROS), Gazebo
LabVIEW, Arduino, Raspberry Pi, Pixhawk, Microcontrollers
3D printing, Rapid Prototyping, Machining
Design, Analysis and Development
Numerical Modeling and Simulation
Robotics and Mechatronics
Autonomous Control Systesm
Experimental Aerodynamics
Documentation
Microsoft Office Suite
LaTeX

Experience

 
 
 
 
 
Vikram Saranbhai Space Centre, Indian Space Research Organisation
Scientist/Engineer - SD
July 2022 – August 2023 Thiruvananthapuram

Technoloy development engineer
Major accomplishments:

  • Collaborated on a spacecraft orbit propagation software tool in C++ with less than 30m/day error growth by simulating perturbations from multiple sources with adaptive time stepping integration.
  • Integrated CSPICE package for planetary ephemeris, increasing accuracy to over 99.9% as compared to NASA’s GMAT.
  • Collaborated with a cross-functional team in realization of a Mach 6-capable Dynamic Damping test setup.
  • Designed and implemented a pneumatic actuator and control system, enabling angular excitation up to 30 deg.
  • Validated system performance, by reproducing result from open literature with over 99% accuracy in damping data.
  • Organized team meetings for brainstorming and troubleshooting; conveyed requirements to fellow system managers.
  • Delivered a vision-based attitude measurement software package in Python with resolution <0.05 deg.
 
 
 
 
 
Vikram Saranbhai Space Centre, Indian Space Research Organisation
Scientist/Engineer - SC
August 2018 – June 2022 Thiruvananthapuram

Technoloy development engineer
Major Accomplishments:

  • Designed test setups, using numerical modeling and optimization for aerodynamics characterization of flight vehicles.
  • Processed and analyzed large data sets from more than 1000 experimental tests, in Python and MATLAB.
  • Collaborated with a team of researchers from national and international research organizations, in generation of comprehensive experimental data for flight vehicle over Mach 4 crucial for informed decisions on Trajectory planning.
  • 3D printed a TPU-based flexible test article for 50 meters drop tests, to protect internal electronics.
  • Installed Pixhawk-based inertial measurement units, along with storage, and power units for data acquisition.
 
 
 
 
 
APLD Lab
Undergraduate Intern
January 2018 – April 2018 Thiruvananthapuram

Topic –“Strut based injection strategies for Scramjet with emphasis on impinging jet”

Performed experimental investigations on the effect of impinging jets on the mixing behavior. Carried out experiments in Mach 1.7 Open Jet facility at Advanced Propulsion and Laser Diagnostics lab at IIST.

  • Designed and fabricated strut with different impingement angles using Solidworks.
  • Devised a scheme for optimum seeding required to achieve efficient Mie scattering.
  • Programmed a LabView code to run the open jet facility, taking into consideration valve operations, camera trigger, laser trigger and secondary flow injection.
  • Developed an image processing based MATLAB code for calculation of mixing area using the Mie scattering images and further post processing of the data.

Accomplish­ments

Simulink Onramp
See certificate
MATLAB Onramp
See certificate
The Ultimate LabView 2020 Course
See certificate

Projects

*
LLMs for Path Planning for Mobile Ground Robots
This project introduces robotic path planning using OpenAI’s GPT-3.5, enabling translation of human-like instructions for precise navigation. Through artificial potential fields and pygame visualization, it facilitates adaptable 2D navigation. Bridging natural language and robotics, it enhances path planning efficiency and adaptability.
LLMs for Path Planning for Mobile Ground Robots
BlackBoat
The BlackBoat project, initiated in September 2021, focused on innovating remote control capabilities for autonomous pump-jet boats. Employing advanced remote control systems, it ensured precise navigation, maintaining a consistent trajectory in challenging water currents at speeds exceeding 15 km/h. Strategic surface treatment protected onboard electronics, laying a foundation for enhanced remote-controlled marine systems.
BlackBoat
Prediction of Long Term Evolution of Satellite Orbit
Collaborated on development of a software tool designed to perform long-duration spacecraft orbit propagation. My role included implementing an adaptive integration scheme to control error growth and incorporating perturbations like non-spherical Earth gravity, third-body effects, atmospheric drag, and solar radiation pressure. I interfaced the tool with JPL ephemerides using the ‘CSPICE’ package to integrate planetary and lunar state vector data. This project was successfully validated against NASA’s GMAT program, showcasing my expertise in aerospace software development and validation.
Prediction of Long Term Evolution of Satellite Orbit
Ulkayaan – A Rendezvous and Landing mission to Comet 46P/Wirtanen.
Conceptualized a rendezvous and landing mission to comet 46P/Wirtanen. Preliminary trajectory designed using methods of Hohmann transfer and Lambert conics. Landing approach designed through successively shrinking triangular orbits, followed by semi-circular arcs and a terminator circular orbit. Carried out spacecraft system integration, allocating space for necessary payloads and subsystems.
Ulkayaan – A Rendezvous and Landing mission to Comet 46P/Wirtanen.
Design, Modelling and Control of an Automated TIG Welding Machine
An automated TIG welding system has been designed with a robotic arm featuring precise degrees of freedom, cross slide, carriage, manipulator arms, nozzle, and bed. The machine is coded for actions like rapid traverse, linear and circular motion, and rotation of the welding head. Actuation systems are modeled using Matlab Simulink with PID control. SolidWorks integration aids in design, and the simulation offers a 3D representation. The system finds applications in seam welding fuselage and pressure vessel welding in industries like power plants and refineries.
Design, Modelling and Control of an Automated TIG Welding Machine
Flight Simulator.
In this project, I integrated an Xbox controller and FlightGear visualization with the MATLAB/Simulink Non-Linear model of the Research Civil Aircraft Model (RCAM). I incorporated an optimization-based trimming module to facilitate control adjustments. Results demonstrate successful replication of user control inputs, stable flight under trim conditions. Despite challenges such as small joystick travel and manual trimming complexities, managed to effectively adjust the aircraft’s trim in the event of an engine shutdown, demonstrating the resilience of the system.
Flight Simulator.

Recent Publications

Quickly discover relevant content by filtering publications.
(2023). Boundary Layer Transition Studies on a Winged Body Reentry Vehicle through Heat Flux Measurements in Shock Tunnel. 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.

Cite DOI URL

(2023). Scramjet Engine Intake Studies in High Enthalpy Impulse Facility. 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.

Cite DOI URL

Contact

Contact for Ideas and Suggestions