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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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Multiple revolution Lunar Trajectory Design using Impulsive Thrust Engine
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Unscented Kalman Filtering for spacecraft attitude and rate determination using magnetometer
