1–20 of 35 hits
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    Stochastic Trajectory and Robust Controller Optimization via Contractive Optimal Control

    Selim, Akan / Cetin, Ahmet T. / Ozkol, Ibrahim et al. | AIAA | 2024

    Robust Trajectory Optimization of Constrained Re-entry Flight

    Selim, Akan / Ozkol, Ibrahim | IEEE | 2023

    Auto-landing Fault-Tolerant Control System Design for a Light Aircraft

    Altunkaya, Ege C. / Ozkol, Ibrahim | AIAA | 2023

      Auto-Landing Fault-Tolerant Control System Design for a Light Aircraft

      Altunkaya, Ege C. / Ozkol, Ibrahim | TIBKAT | 2023

    Numerical Investigation of Hybrid Rocket Nozzle Heat Transfer and Test Validation

    Ozturk, Sule / Ozkol, Ibrahim / Karabeyoglu, M. Arif | IEEE | 2023

    Thermal Buckling Analysis of Rectangular Plate Structures by Differential Quadrature Method

    Yavuz, Mustafa Tolga / Ozkol, Ibrahim / Arikoglu, Aytac | IEEE | 2023

    Stabilizing Adaptive Feedback Controller Design for a Helicopter Gun Turret System

    Uyulan, Caglar / Yavuz, Mustafa Tolga / Ozkol, Ibrahim | IEEE | 2023

    Hybrid Rocket Nozzle Erosion with Microaluminum-Added Fuel

    Karakas, Hakki / Kahraman, Busra / Ozkol, Ibrahim et al. | AIAA | 2022

    AUTONOMOUS UNMANNED AERIAL VEHICLE

    Free access
    CANLI GURAY ALI / AKDUMAN IBRAHIM / KURTOGLU ISMAIL et al. | European Patent Office | 2019

      Autonomous unmanned aerial vehicle

      Free access
      CANLI GURAY ALI / AKDUMAN IBRAHIM / KURTOGLU ISMAIL et al. | European Patent Office | 2022

      AUTONOMOUS UNMANNED AERIAL VEHICLE

      Free access
      CANLI GURAY ALI / AKDUMAN IBRAHIM / KURTOGLU ISMAIL et al. | European Patent Office | 2020

    Regression Rate Enhancement of Hybrid Rockets by Introducing Novel Distributed Tube Injector

    Kahraman, Mehmet / Ozkol, Ibrahim / Karabeyoglu, M. Arif | AIAA | 2021

    Enhancement of Fuel Regression Rate for Hybrid Rockets by Introducing Novel Coaxial Tube Injector

    Kahraman, Mehmet / Ozkol, Ibrahim / Karabeyoglu, Arif | AIAA | 2020

      ENHANCEMENT OF FUEL REGRESSION RATE FOR HYBRID ROCKETS BY INTRODUCING NOVEL COAXIAL TUBE INJECTOR

      Kahraman, Mehmet / Ozkol, Ibrahim / Karabeyoglu, Arif | TIBKAT | 2020

    Influence of Micro-Aluminum Addition to Paraffin-Based Fuels on Graphite Nozzle Erosion Rate

    Karakas, Hakki / Kara, Ozan / Kahraman, Busra et al. | AIAA | 2020

      INFLUENCE OF MICRO-ALUMINUM ADDITION TO PARAFFIN-BASED FUELS ON GRAPHITE NOZZLE EROSION RATE

      Karakas, Hakki / Kara, Ozan / Kahraman, Busra et al. | TIBKAT | 2020

    Performance Enhancing Additives for Hybrid Rockets

    Karakas, Hakki / Kara, Ozan / Ozkol, Ibrahim et al. | AIAA | 2019

    Novel Hybrid Rocket Internal Ballistic Configuration with Coaxially Located Tube Injector

    Kahraman, Mehmet / Gegeoglu, Kaan / Ozkol, Ibrahim et al. | AIAA | 2019