• SAR Satellite Constellation Control Center

    • Functionality analysis of Synthetic Aperture Radar (SAR) satellite control center
    • Conceptual design of SAR satellite control center
    • Develop precise orbit determination module for SAR satellite constellation
  • Multiple Satellite System Orbit Determination

    • Satellite Laser Ranging(SLR) Based Satellite Orbit Determination
    • Inter-satellite Link(ISL) Based Satellite Orbit Determination
    • Real-time On-board Orbit Determination using Kalman Filter
    • Navigation System Hardware Simulator Development/Applications
  • Lunar Exploration

     

    Space Flight Dynamics Software Development for Korean Lunar Exploration 
    – Build FDS for the Korean Lunar exploration program
    – Develop of data simulation module for processing/generating DSN data & error corrections
    – Develop of DSN-based orbit determination module
    – Achieve 1km-level orbit determination precision
    – Develop event prediction module for predicting various celestial phenomena 

    Lunar Mission Design and Analysis using CubeSat and Smartphone-sat 
    – Preliminary Lunar CubeSat/phonesat mission design

    Development of GMAT components III 
    – General Mission Analysis Tool (GMAT)
    – Visualization of launch trajectory
    – Accurate celestial event location capability through SPICE kernel
    – High-fidelity low-thrust trajectory optimization capability based on Gauss-Legendre-Radau collocation method
  • CANYVAL-C

    CANYVAL-C mission is aimed at scientific validation of photographing the sun’s corona.
    This mission is the application of Virtual Telescope technology that uses several discrete satellites as a space telescope.
    The mission requires development of inertial alignment hold technology, spacecraft formation flying GNC technology and inter-satellite link technology.
    CANYVAL-C is a subsequent mission of CANYVAL-X, technical experiment mission of virtual telescope, and expects further projects of solar science and X-ray objective science mission.

    The CANYVAL-C system consists of two CubeSats, ‘PUMBAA’ and ‘TIMON’. PUMBAA, the occulter, is a 2U CubeSat that covers the sun for corona imaging.

    TIMON, the detector, is an 1U CubeSat that takes a coronagraph with an optical camera.
    The CubeSats are planned to be launched in July, 2019.

  • Asteroid Deflection

    • Design interplanetary trajectory to target asteroid
    • Develop techniques to deflect a potentially hazardous asteroid
  • On-board Ephemeris Generator

    • Supporting Korea Lunar Pathfinder Mission
    • Develop algorithm of Ephemeris data compression.
    • Verify the algorithm through simulations.
    • Develop on-board ephemeris generation algorithm for Korean Lunar Exploration.
    • Develop software for compressed ephemeris data that will be used on Ground station.
    • Implement the algorithm to GMAT
  • Satellite Orbit Determination using Optical Observation

    • Develop of initial orbit determination software using elevation/azimuth angle
    • Develop of precise orbit determination software using batch least-square algorithm and optical observation model
    • Performance analysis of precise orbit determination using Optical Wide-field Patrol (OWL) observation data

    OWL-Net Mongol site