FLIGHT DYNAMICS AND CONTROL
LABORATORY
in Department of Aerospace Engineering @ Seoul National University
RESEARCH AREA
Flight Dynamics and Control Laboratory (FDCL) performs research on the topics closely related to guidance and control systems for aerospace vehicles. Experimental as well as theoretical research is conducted in the areas of aircraft/spacecraft attitude controller design, aircraft vision-based landing and collision avoidance, guidance and control of Unmanned Aerial Vehicle (UAV), missile guidance and control, launch vehicle trajectory optimization, formation flying of multiple UAV or Satellite, etc. Experimental facility include various fixed-wing unmanned aircraft, rotor-craft (quad-rotor & helicopters), and HILS system.

[Guidance, Navigation, and Control Algorithm for Lunar Orbiter]

[Missile Guidance]

[Model Predictive Control for Terrain-following Flight]

[Experimental Facility]
PROJECT
ADVISOR
Prof. Youdan Kim

RECENT PUBLICATIONS
Missile Autopilot Design via Neural Koopman Embedding
Control Barrier Function Based Terrain and Path Following Control of Unmanned Aerial Vehicle Considering Attitude Constraint
Sliding Surface-Based Integral Reinforcement Learning for Optimal Tracking Control of Quadcopters Considering Uncertainties
Media
FDCL in the Press
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2025-05-14
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2025-05-14
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2025-05-14