Astrodynamics and Control Laboratory (ACL)
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  • Home
  • News
  • Research
  • Projects
    • Previous projects
    • Current projects
  • People
    • Professor
    • PhD students
    • MS students
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  • Initial orbit association and long-term orbit prediction for low earth space objects using optical tracking data

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  • Adaptive Saturated Neural Network Tracking Control of Spacecraft Theory and Experimentation

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  • Adaptive Control for Spacecraft Rendezvous Subject to Time-Varying Inertial Parameters and Actuator Faults

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  • Sub-optimal cooperative collision avoidance maneuvers of multiple active spacecraft via discrete-time generating functions

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  • A Nonsingular Dual-Primal Algorithm for Fuel-Optimal Impulsive Rendezvous

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  • Development of General-purpose Root-finding Module for General Mission Analysis Tool

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  • Spacecraft attitude control using neuro-fuzzy approximation of the optimal controllers

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  • Perturbative Analysis on Orbital Kinematics of Flybys and Applications to Doppler Observation

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  • Dynamic Optimal Output Feedback Control of Satellite Formation Reconfiguration Based on an LMI Approach

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  • Near-Optimal Continuous Control for Spacecraft Collision Avoidance Maneuvers via Generating Functions

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  • Analysis of Position and Velocity Variations for Hyperbolic Orbits and Application to the Flyby Anomaly

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  • Orbit Determination of Korea Regional Navigation Satellite System Using Inter-Satellite Links and Ground Observations

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  • Development of a hardware-in-the-loop testbed to demonstrate multiple spacecraft operations in proximity

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  • Hardware Simulations of Spacecraft Attitude Synchronization Using Lyapunov-Based Controllers

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  • Guidance and Control for Satellite in-Orbit-Self-Assembly Proximity Operations

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  • Analysis of Position and Velocity Variations for Hyperbolic Orbit and Applications to Doppler Observation

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  • Estimation of necessary laser power to deflect near-Earth asteroid using conceptual variable-laser-power ablation

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  • Precise Orbit Determination using the Batch Filter based on Particle Filtering with Genetic Resampling Approach

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  • Optimal Tracking and Formation Keeping Near a General Keplerian Orbit under Nonlinear Perturbations

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  • Adaptive Tracking Control of Spacecraft Relative Motion with Mass and Thruster Uncertainties

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Updated in 2023. Astrodynamics and Control Lab. (연세대학교 우주비행제어연구실)
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