Direnc Atmaca
Tagline:Doctoral Researcher at TU Delft | Fault-Tolerant Control | Adaptive and Nonlinear Control Systems | Automatic Flight Control
Delft, Netherlands
About Me
I am a Doctoral Researcher at TU Delft, actively involved in the Flying-V project. My primary research interests lie in the areas of nonlinear and adaptive fault-tolerant control systems and piloted simulator testing for handling quality research. I am interested in the applications of such systems for improving the handling qualities of the Flying-V aircraft.
Also, I have a background in nonlinear feedback guidance systems, with a particular focus on their applications in efficient low-thrust orbit transfers.
I'm grateful for the opportunity to collaborate with the dedicated Flying-V team, and I welcome connections with professionals and enthusiasts in the aerospace field.
Thank you for visiting my profile. If you'd like to engage in discussions or explore potential collaborations related to these research interests, please feel free to connect.
Education
Doctor of Philosophy - PhD
from: 2023, until: 2027Field of study:Aerospace EngineeringSchool:Delft University of TechnologyLocation:Delft, NL
DescriptionFlying-V Flight Control
Master of Science
from: 2020, until: 2023Field of study:Space and Astronautical EngineeringSchool:Sapienza University of RomeLocation:Rome, IT
DescriptionThesis: Nonlinear Feedback Guidance for Earth Orbit Transfers
Bachelor of Science
from: 2015, until: 2020Field of study:Mechanical EngineeringSchool:Middle East Technical UniversityLocation:Turkey
DescriptionThesis: Package Tracker with Vibrational Energy Harvester for Fully Autonomous Operation.
Publications
Near-Optimal Feedback Guidance for Low-Thrust Earth Orbit Transfers
Journal ArticlePublisher:Aerotecnica Missili & SpazioDate:2024Authors:D. AtmacaM. Pontani
Research Interests
- Fault-Tolerant Control
- Nonlinear Control Theory
- Fault Identification
- Incremental Nonlinear Dynamic Inversion
- Two-Stage Kalman Filters
- Higher-Order Sliding Modes
- Automatic Flight Control
- Aircraft Handling Qualities
- Flight Simulation
Work Experiences
Doctoral Researcher
from: 2023, until: presentOrganization:TU Delft | Aerospace EngineeringLocation:Delft, South Holland, Netherlands
Description:In my capacity as a Doctoral Researcher at TU Delft, I specialize in Nonlinear and Adaptive Fault-Tolerant Flight Control Systems. My primary focus centers around the application of Adaptive Incremental Nonlinear Dynamic Inversion (INDI), particularly in the context of the cutting-edge Flying-V aircraft project here at TU Delft.
AOCS, GNC, and Mission Design
from: 2022, until: 2023Organization:FreelancerLocation:Rome, Italy
Description:As a freelancer, I provided support and expertise in AOCS, GNC, and Mission Analysis areas. During this time, I had the opportunity to work on some exciting projects, one of which was about solar sail spacecraft design and analysis to maximize payload fraction for different mission categories and included the following tasks:
• Performed a feasibility study for solar-sail spacecraft to maximize payload capacity
• Simulated different mission scenarios including Earth-to-Moon and Earth-to-Mars
• Optimized a trade-off between sail size, transfer time, and payload capacityOptics and Surveillance Systems Intern
from: 2019, until: 2019Organization:Baykar TechnologiesLocation:Istanbul, Turkey
Description:• Performed optical and structural design of unmanned combat aerial vehicle (UCAV) components
• Created research reports on UCAV optics and surveillance systems
• Optimized the optical systems on the UCAV to improve surveillance performance
Journal Contributions
Skills
- Fault-Tolerant Control
- Fault Identification
- Advanced Kalman Filtering
- Automatic Flight Control Design
- State and Parameter Estimation
- Aircraft Handling Qualities
- Attitude and Orbit Control
- MATLAB
- Simulink
- Python
Projects
Martian Rover Modelling and Path Planning
date: 2022Description:This project includes the modelling, path finding and localization for a rover on the Mars surface near the Jezero crater.
The complete design consists of the following steps:
• Kinematic modelling and simulation of the rover in order to move from an initial pose to a final pose to perform sampling operations
• Creating an A* algorithm that finds the most optimal path in order to move around the Jezero crater by avoiding the hazardous regions previously determined using a digital elevation model
• Estimating the quality of the onboard odometer by reconstructing the true paths that are generated in the prior steps through dead reckoning
• Reconstructing the same paths by using an Extended Kalman Filter that takes a combination of odometer and LIDAR readings as input. The LIDAR readings are obtained through the pre-located landmarks on the Mars surface and are used to increase the accuracy of the path reconstructionCollision Avoidance for a Quadrotor Swarm Through Control Barrier Certificates
date: 2022Description:This project includes the modeling of 5 quadrotors equipped with proper control systems to track a particular trajectory as well as control barrier enforcement to guarantee safe operation.
The complete design includes the following objectives:
• Modeling the system dynamics of each quadrotor on MATLAB/Simulink
• Generating reference trajectories for each quadrotor that are guaranteed to lead to collisions
• Designing a hierarchical proportional-derivative control system to track the generated trajectories
• Synthesizing Control Barrier Certificates by using Exponential Control Barrier Functions
• Enforcing the Control Barrier Certificates on pairwise quadrotors to prevent collisions through a quadratic program that generates a safe control action by taking the system dynamics, barrier functions and nominal control as input
• Validating that the quadratic program minimizes the difference between the nominal and safe control action while preventing collisionsRobotic Gimbal Design for a Spacecraft Orbiting Mars
date: 2021Description:A space manipulator is designed for a spacecraft in the Martian orbit to perform independent pointing of a stereo camera.
The complete design includes the following steps:
-
Fixed Base Assumption
• Modelling of the manipulator using Denavit-Hartenberg formulation
• Obtaining the Jacobian and the dynamical equations of motion
• Trajectory generation in order to track a particular location on the martian surface
• Design of a proper control system to obtain the desired trajectory and to reject the disturbances acting on the spacecraft -
Free Base Assumption
• Modelling of a virtual manipulator following the Denavit-Hartenberg formulation (S. Dubowski and Z. Vafa, 1987)
• Trajectory generation for the virtual manipulator
-
Ground Tracking of a Spacecraft Orbiting the Moon
date: 2021Description:• Tracked a spacecraft orbiting the moon by a using ground station located on Earth
• Implemented different sensors that measure distance and velocity at different accuracies
• Fused the sensor outputs using a Kalman Filter to obtain a new and more accurate time history of the state vector
• Replicated the results using the Weighted Least Squares (WLS) method to compare the results with the Kalman Filter
• Reproduced the results by assuming the ground station is located on the Moon instead of the EarthPackage Tracker with Vibrational Energy Harvester for Fully Autonomous Operation
date: 2019Description:This project has been developed as a multi-disciplinary senior design project. The goal was to design a package tracker that harnesses the vibrational energy available in the environment to power a tracking system without depending on an external power source. The project included three students from aerospace engineering, electrical and electronics engineering and mechanical engineering programs.
My responsibilities in this project were as follows:
•Dynamical modelling of the vibrational energy available inside a cargo vehicle
•Designing a electromagnetic transducer to harness the vibrational energy and to convert it to electrical energy
•Optimizing the transducer design to match the energy and power requirements of the tracking deviceThe objectives of this project were as follows:
•Modelling the vibrations of a cargo vehicle considering 7 degrees of freedom
•Designing a transducer to harness the vibrational energy and to convert it to electrical energy
•Generating RF signals from the electrical energy using power electronics