The Flight Dynamics and Control Laboratory (FDCL) was established in 1989 by Prof. Min-Jea Tahk (founder). Recently, Prof. Chang-Hun Lee joined FDCL in 2019. Since 1989, FDCL has been successfully fostering students, engineers, and professors in the field of flight dynamics and control, and playing key roles in national aerospace research and development programs.
FDCL is carrying out research on guidance, navigation, and control for various aerospace vehicles including missiles, unmanned aerial vehicles, space launch vehicles, and space airplane, etc. Our main focus is on guidance and control of guided missiles, flight control systems of unmanned aerial vehicles, as well as big data analytics & machine learning in aerospace applications. Computational guidance and control and trajectory optimization techniques are also being investigated.

FDCL은 미사일, 무인 항공기, 우주 발사체, 우주 비행기 등 다양한 항공우주 차량에 대한 유도, 항법 및 제어에 대한 연구를 수행하고 있습니다. 우리의 주요 초점은 유도 미사일의 유도 및 제어, 무인 항공기의 비행 제어 시스템, 항공우주 애플리케이션의 빅 데이터 분석 및 머신 러닝에 있습니다. 전산 유도 및 제어, 궤적 최적화 기술도 연구되고 있습니다.

Optimal Guidance and Its Applications in Missiles and UAVs

Time-to-Go Polynomial Guidance Laws under Off-Axis Seeker Constraints

Real-Time Feasible Optimal Deployment Strategy for Carrier-Type Missiles in Multi-Target Engagements

Uncertainty-Aware Adaptive Sampling in MPPI for Robust UAV Path-Following

Receding-Horizon Midcourse Guidance for Variable-Flow Ducted Rocket Missiles

Semi-Analytical Guidance for Velocity Maximization of Gliding Vehicles Using Proportional Navigation and Sparse Waypoints

Polynomial Based Impact-Time-Control Guidance Law Integrating Optimal Characteristics

Optimal Landing Guidance of Reusable Launch Vehicles with Dual-convex Optimization

Look-angle-based Agile Turn Guidance for All-aspect Target Interception

Review of Data-Driven Computational Guidance for Unmanned Aerospace Vehicles

An Impact Point Guidance for a Launch Vehicle with Aerodynamics Control

A Data-Driven Learning Guidance Strategy for Target Interception with Terminal Time Constraint

On the Reachability of 3-Dimensional Paths with a Prescribed Curvature Bound

Generative Adversarial Imitation Learning-based Continuous Learning Computational Guidance

Fault-Tolerant Control Allocation in Coaxial Dodecacopter Using Quadratic Programming-based on ACS Analysis

Convex Optimization based Landing Guidance and Control Algorithms for Reusable Orbital Rockets

Computational Predictor-Corrector Homing Guidance for Constrained Impact

Non-iterative Convex Programming-based Optimal Guidance with Field-of-View and Acceleration Limits

Guidance Scheme for Gun-Launched Gliding Guided Projectiles

Generalized Time-to-Go Inversion Guidance with Impact Time and Angle Constraints

A New Trust-Region Constraint Method for Sequential Convex Programming Framework for Entry Guidance

Proportional Navigation Guidance with Virtual Targeting for Impact-Angle-Control

Optimal Impact Angle Control Guidance Law Considering Aerodynamic Drag

Performance Analysis of a Ducted Rocket under Various Flight Conditions

Optimal Impact-angle Constrained Guidance with Barrier Constraint

Firing Command Generation for Close-In-Weapon System to Intercept High-Speed Targets

A Study on the Weapon Target Assignment Problem Considering Heading Error

A Disturbance Rejection Control for Urban Air Mobility using Artificial Sensor-based Gaussian Process Regression

Impact Time and Angle Guidance Considering Aerodynamic Drag

Heading Error Shaping Guidance Laws Using Generalized Finite-Time Convergence Error Dynamics

Attitude Takeover Control for Noncooperative Space Targets Based on Gaussian Processes with Online Model Learning

Attitude Hold Proportional Navigation Guidance for Interceptors with Off-axis Seeker

New Adaptive Mesh Refinement Strategy for Entry Guidance via Sequential Convex Programming

Adaptive Weight Model Predictive Path Integral Control for Multi-constrained Missile Guidance

Nonlinear Three-Dimensional Guidance for Impact Time and Angle Control with Field-of-View Constraint

Identification of Uncertain Parameter in Flight Vehicle Using Physics-Informed Deep Learning

Mission Profile Analysis of Point-to-Point Rocket Cargo Transportation System using Trajectory Optimization

Optimal Midcourse Guidance for Dual-Pulse Rocket Using Pseudospectral Sequential Convex Programming

Thrust Integrated Trajectory Optimization for Multi-pulse Rocket Missiles using Convex Programming

MPPI-Based Computational Guidance for Impact Time Control with Practical Constraints

Fixed Range Horizon MPPI-based Missile Computational Guidance for Constrained Impact Angle

Multi-phase and Dual Aero/Propulsive Rocket Landing Guidance using Successive Convex Programming

Three-Dimensional Bearing-Only Target Following via Observability-Enhanced Helical Guidance

Aerodynamically Controlled Missile Flight Datasets and its Applications

Investigation on Energy-Effective Guidance-to-Collision Strategies for Exo-Atmospheric Interceptors

New Weapon Target Assignment Algorithms for Multiple Targets Using Rotational Strategy and Clustering Approach

Optimal Encirclement Guidance

Nonlinear Optimal 3-D Impact-Angle-Control Guidance against Maneuvering Targets

Dynamic Estimation and Compensation of Time Delay for Missiles with Strapdown Seeker

Convex Optimization-based Entry Guidance for Spaceplane

New Look-Angle Tracking Guidance Strategy for Impact Time and Angle Control

A Unified Formulation of Optimal Guidance-to-Collision Law for Accelerating and Decelerating Targets

Collision-geometry-based Optimal Guidance for High-speed Target

Nonlinear Optimal Impact-Angle-Constrained Guidance with Large Initial Heading Error

Trajectory Shaping Guidance Law Design using Constraint-Combining Multiplier

A New Guidance Algorithm against High-Speed Maneuvering Target

A Practical Optimal Guidance Scheme under Impact Angle and Terminal Acceleration Constraints

Collision-Geometry-Based Generalized Optimal Impact Angle Guidance for Various Missile and Target Motions

A New Cooperative Homing Guidance of Anti-ship Missiles for Survivability Enhancement

Optimal Intermittent Maneuver of Homing Missiles for Target Observability Improvement

Schwarz Inequality Method for Weighted Minimum Effort Terminal Control of Multi-Dimensional Systems

Optimal Three-Dimensional Impact Time Guidance with Seeker's Field-of-View Constraint

Distributed Cooperative Guidance for Multi-Vehicle Simultaneous Arrival without Numerical Singularities

Investigation on Physical Meaning of Three-Loop Autopilot

Energy-Optimal Waypoint-Following Guidance Considering Autopilot Dynamic

Stage Optimization of Anti-air Missiles Using Practical Guidance Laws

Nonlinear Autopilot Design for Endo-and Exo-Atmosphere Interceptor Thrust Vector Control

A New Collision Control Guidance Law Based on Speed Control for Kill Vehicles

Minimum-Effort Waypoint-Following Guidance

Study on Parasite Effect with Strapdown Seeker in Consideration of Time Delay

A Collision Geometry-based Guidance Law for Course-Correction-Projectile

Practical Generalized Weighted Optimal Guidance Law with Impact Angle Constraint

Optimal Impact Angle Guidance for Exo-Atmospheric Interception Utilizing Gravitational Effect

Optimal Proportional-Integral Guidance with Reduced Sensitivity to Target Maneuvers

New Insights into Guidance Laws with Terminal Angle Constraints

New Application of Data Analysis using Aircraft Fault Record Data

Optimality of Error Dynamics in Missile Guidance Problems

Gravity Turn-Assisted Optimal Guidance Law

Impact Time Control Based on Time-to-Go Prediction for Sea-Skimming Anti-Ship Missiles

Zero-Effort-Miss Shaping Guidance Laws

New Design Methodology for Impact Angle Control Guidance for Various Missile and Target Motions

Connections between Linear and Nonlinear Missile Autopilots via Three Loop Topology

Effects of Time-to-Go Errors on Performance of Optimal Guidance Laws

Command Shaping Guidance Optimal Laws against High-speed Incoming Targets

New Trajectory Shaping Guidance Law for Anti-Tank Guided Missiles

Sinusoidal Function Weighted Optimal Guidance Laws

Biased PNG for Target Observability Enhancement against Nonmaneuvering Targets

Optimal Resource Management Algorithm for UAV Missions in Hostile Territories

Agile Missile Autopilot Design using Nonlinear Backstepping Control with Time-Delay Adaptation

Command Shaping Guidance Law Based on Gaussian Weighting Function

Augmented Polynomial Guidance with Impact Time and Angle Constraints

Interception angle control guidance using proportional navigation with error feedback

Augmented polynomial guidance with impact time and angle constraints

Polynomial guidance laws considering terminal impact angle and acceleration constraints

Optimality of error dynamics in missile guidance problems

Generalized formulation of weighted optimal guidance laws with impact angle constraint

Impact time control based on time-to-go prediction for sea-skimming antiship missiles

Nonlinear optimal impact-angle-constrained guidance with large initial heading error

Three-dimensional bearing-only target following via observability-enhanced helical guidance

Distributed cooperative guidance for multivehicle simultaneous arrival without numerical singularities

Optimal three-dimensional impact time guidance with seeker’s field-of-view constraint

Time-to-go polynomial guidance with trajectory modulation for observability enhancement

Design of impact angle control guidance laws via high-performance sliding mode control

New insights into guidance laws with terminal angle constraints

Connections between linear and nonlinear missile autopilots via three-loop topology

New design methodology for impact angle control guidance for various missile and target motions

New look-angle tracking guidance strategy for impact time and angle control

Minimum-effort waypoint-following guidance

Nonlinear optimal 3-D impact-angle-control guidance against maneuvering targets

Gravity-turn-assisted optimal guidance law

Agile missile autopilot design using nonlinear backstepping control with time-delay adaptation

Min-Jea Tahk

Antonios Tsourdos

Han-Lim Choi

Seong-Min Hong

Ju-Hyeon Hong

Zakwan Skaf

Chang-Kyung Ryoo

KEUM-SEONG KIM

H. Jin Kim (김현진, Hyoun Jin Kim)

Chang-Hun Lee

School of Aerospace, Transportation, and Manufacturing

Associate Professor

Impact-time-control guidance law for anti-ship missiles

Optimal guidance laws with terminal impact angle constraint

Guidance law to control impact time and angle

Time-to-go weighted optimal guidance with impact angle constraints

Nonsingular sliding mode guidance for impact time control

Target tracking problems subject to kinematic constraints

UAV collision avoidance based on geometric approach

Impact-time-control guidance with generalized proportional navigation based on nonlinear formulation

Bias-shaping method for biased proportional navigation with terminal-angle constraint

Coevolutionary augmented Lagrangian methods for constrained optimization

Optimal impact angle control guidance law considering the seeker’s field-of-view limits

Large angle attitude control of spacecraft with actuator saturation

Recursive time-to-go estimation for homing guidance missiles

Generalized input-estimation technique for tracking maneuvering targets

Differential game based air combat maneuver generation using scoring function matrix

Flight Dynamics and Control Laboratory (FDCL)

교수님 소개

이창훈

연구실 소개

연구실 키워드

알럼나이가 간 회사

연구실 지원 방법

대우 조건

연도별 논문 인용수

저널 & 학회 논문 출판 수

연구실 논문 목록

Time-to-Go Polynomial Guidance Laws under Off-Axis Seeker Constraints

Real-Time Feasible Optimal Deployment Strategy for Carrier-Type Missiles in Multi-Target Engagements

Uncertainty-Aware Adaptive Sampling in MPPI for Robust UAV Path-Following

연구실 보유 특허

대학별 입시끈

우리 연구실 모집

교수님 소개

이창훈

연구실 키워드

알럼나이가 간 회사

연구실 지원 방법

대우 조건

연도별 논문 인용수

저널 & 학회 논문 출판 수

연구실 논문 목록

Time-to-Go Polynomial Guidance Laws under Off-Axis Seeker Constraints

Real-Time Feasible Optimal Deployment Strategy for Carrier-Type Missiles in Multi-Target Engagements

Uncertainty-Aware Adaptive Sampling in MPPI for Robust UAV Path-Following

연구실 보유 특허

최근 3년간 연구실적 높은 연구실

대학별 입시끈

우리 연구실 모집