Projects
Ongoing Projects
Study on Learning-Based Control with Domain-Information Incorporation for Autonomous and Intelligent Systems (NRF, 2023. 06 - 2025. 02)
International Collaboration Project with Cranfield Univ. (NRF International Mobility Project, 2023. 10 - 2024. 09)
BK 21 (Research and Education Center for Intelligent Wearable Robots) (BK21, 23.09 - 24.08)
Past Projects (SATM, Cranfield University)
- Time Synchronisation for CUAS&UTM (UK Innovate)
- High Air Drone Operation (HADO, UK Innovate)
Past Projects (FDCL, SNU)
- A Study on Launch Acceptable Region (LAR) of Air-Launched Guided Vehicles (LIG-Nex1)
Design of missile guidance law and LAR analysis.
Design of guidance Filter
- A Development of Control Algorithm for VTOL-Fixed Wing UAVs (Agency for Defense Development)
MPC Design for altitude/path tracking
Attitude Control for Convertible vehicle with Limited Maneuverability (CCV-A, STT)
- A Study on Control system Using Strapdown Seeker with Multi-division Field-of-View,(Agency for Defense Development)
Design of missile guidance law and capturability analysis regarding FOV limit.
Target Detection and tracking algorithm
Development of Engagement simulator for the seeker-integrated guided missile.
- Development of An Analysis Simulation Program for Guided Weapon Systems (Hanwha)
Design of guidance and control algorithm for evasive maneuvers of anti-ship missiles
Design of ship defense system
Development of an engagement simulator using Matlab/Simulink in GUI environment.
- Guidance and Control Study for Take-off and Landing on a Ship(Agency for Defense Development)
Design of take-off and landing Guidance and Control
Risk Evaluation and Decision Making Process for Landing Operation
Development of software in the loop system (SILS) for automatic carrier landing system using X-Plane and Matlab/Simulink
- Integrated Autopilot Design for Fast Velocity-varying Missiles(Agency for Defense Development)
Design of attitude controller of fast velocity-varying missile using nonlinear control scheme.
Design of acceleration controller of fast velocity-varying missile using nonlinear control scheme.