Astrodynamics and Control Laboratory (ACL)
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  • News
  • Research
  • Projects
    • Previous projects
    • Current projects
  • People
    • Professor
    • PhD students
    • MS students
  • Publications
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    • Domestic conferences
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  • Orbit determination of Korea regional navigation satellite system based on inter-satellite link

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  • A preliminary design of a 5-DOF hardware simulator for spacecraft formation flying

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  • Implementation of LARES spin model and its analysis

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  • Fuel optimization for altitude maintenance of Low-Earth-Orbit(LEO) spacecraft by combining direct and indirect methods

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  • Performance analysis and general-purpose module development of root-finding algorithms for spacecraft trajectory design

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  • Relative position determination in real-time using inter-satellite laser ranging

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  • An Analytical Method for the Altitude Maintenance of LEO Satellite with Constrained Eccentricity Using the Low-Thrust

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  • A Satellite Attitude Scenario for Image Validation Using Stellar Sources

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  • Reconfiguration trajectories with collision avoidance constraint under gravitational field

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  • Analysis of scaling parameters of the batch unscented transformation in satellite orbit determination using satellite laser ranging data

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  • Performance Analysis of Formation Flying Satellites Interferometry using Image Quality Metrics

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  • Optimal Lunar trajectory design considering spacecraft’s visibility from Deajeon ground station at TLI and LOI maneuver

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  • Suboptimal space launch vehicle trajectory generated by state dependent Riccati equations

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  • Analysis of Attitude Synchronization Control for Spacecraft Formation Flying via Hardware-In-the-Loop Simulation

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  • Approximate analytical solutions to fuel-optimal reconfiguration problems in perturbed relative motion between satellite

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  • Batch Unscented Transformation for Satellite Orbit Determination Using A Satellite Laser Ranging

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  • Real-time relative navigation for autonomous formation flying satellites

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  • Development of a hardware-in-the-loop simulator for spacecraft attitude control using thrusters

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  • Fuel Optimization for Low Earth Orbit Maintenance

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  • Multiple revolution Lunar Trajectory Design using Impulsive Thrust Engine

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