Research outputs
Selected research outputs
- Enhancing RTK-based relative navigation for CubeSats rendezvous: An ADOP perspective on integer ambiguity resolution (Journal article - 2025)
- Highly Efficient Real-Time Kinematic-Based Precise Relative Navigation for Autonomous Rendezvous CubeSat (Journal article - 2024)
- Precise in-orbit relative navigation technique for rendezvous mission of CubeSats using only GPS receivers (Journal article - 2024)
- Development of Hardware-in-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer (Journal article - 2023)
- Probabilistic Determination Algorithm for Detumbling and Angular Rate Convergence using a Three-Axis Magnetometer (Journal article - 2022)
- In-Orbit Results and Attitude Analysis of the SNUGLITE Cube-Satellite (Journal article - 2020)
2025
Enhancing RTK-based relative navigation for CubeSats rendezvous: An ADOP perspective on integer ambiguity resolution
Shim, H., & Kee, C. (2025). Enhancing RTK-based relative navigation for CubeSats rendezvous: An ADOP perspective on integer ambiguity resolution. Acta Astronautica, 236, 1181-1197. doi:10.1016/j.actaastro.2025.08.001
Efficient GNSS-Based Attitude Determination and Integer Ambiguity Resolution for 3U CubeSats
Bae, Y., Shim, H., & Kee, C. (2025). Efficient GNSS-Based Attitude Determination and Integer Ambiguity Resolution for 3U CubeSats. In 2025 IEEE Aerospace Conference (pp. 1-9). IEEE. doi:10.1109/aero63441.2025.11068415
Onboard Implementation and Validation of RTK-Based Relative Navigation System for CubeSats
Shim, H., Kim, B. -G., Bae, Y., & Kee, C. (2025). Onboard Implementation and Validation of RTK-Based Relative Navigation System for CubeSats. In 2025 IEEE Aerospace Conference (pp. 1-10). IEEE. doi:10.1109/aero63441.2025.11068564
Propellant-Free Rendezvous Mission of SNUGLITE-III CubeSat: Orbit Control Using Aerodynamic Forces
Hwang, J. W., Shim, H., Bae, Y., Kee, C., & Kim, J. (2025). Propellant-Free Rendezvous Mission of SNUGLITE-III CubeSat: Orbit Control Using Aerodynamic Forces. In 2025 IEEE Aerospace Conference (pp. 1-12). IEEE. doi:10.1109/aero63441.2025.11068680
Analysis of Relative Motion after Inter-Satellite Separation for SNUGLITE-III Autonomous Formation Flying Mission
Hwang, J. -W., Shim, H., Bae, Y., & Kee, C. (2025). Analysis of Relative Motion after Inter-Satellite Separation for SNUGLITE-III Autonomous Formation Flying Mission. Journal of the Korean Society for Aeronautical & Space Sciences, 53(1), 77-89. doi:10.5139/jksas.2025.53.1.77
2024
Verification and Hardware Implementation of Single-Frequency RTK-Based Precise Relative Navigation for SNUGLITE-III CubeSat
Shim, H., Bae, Y., Kee, C., & Koo, I. H. (2024). Verification and Hardware Implementation of Single-Frequency RTK-Based Precise Relative Navigation for SNUGLITE-III CubeSat. In The International Technical Meeting of the The Institute of Navigation (pp. 787-798). Institute of Navigation. doi:10.33012/2024.19486
Highly Efficient Real-Time Kinematic-Based Precise Relative Navigation for Autonomous Rendezvous CubeSat
Shim, H., & Kee, C. (2024). Highly Efficient Real-Time Kinematic-Based Precise Relative Navigation for Autonomous Rendezvous CubeSat. NAVIGATION: Journal of the Institute of Navigation, 71(3), navi.661. doi:10.33012/navi.661
Low-Cost Satellite Angular Velocity Determination Method Through Optical Flow Tracking Based on Flownet
Seongjin, P., Hwang, J. W., Shim, H., & Kee, C. (2024). Low-Cost Satellite Angular Velocity Determination Method Through Optical Flow Tracking Based on Flownet. In 52nd IAF Student Conference (pp. 258-269). International Astronautical Federation (IAF). doi:10.52202/078379-0020
Precise in-orbit relative navigation technique for rendezvous mission of CubeSats using only GPS receivers
Shim, H., Kim, O. -J., Yu, S., Kee, C., Cho, D. -H., & Kim, H. -D. (2024). Precise in-orbit relative navigation technique for rendezvous mission of CubeSats using only GPS receivers. CEAS Space Journal, 16(1), 117-137. doi:10.1007/s12567-023-00488-x
2023
Operation Results of SNUGLITE-II CubeSat: Convective 3D Observation and Precise Attitude Determination Using GPS Carrier Measurements
Shim, H., Koo, I. H., Bae, Y., Park, J., Jeong, H., Lee, J., . . . Koo, C. H. (2023). Operation Results of SNUGLITE-II CubeSat: Convective 3D Observation and Precise Attitude Determination Using GPS Carrier Measurements. Journal of the Korean Society for Aeronautical & Space Sciences, 51(10), 721-734. doi:10.5139/jksas.2023.51.10.721
Single Frequency RTK Relative Navigation for Autonomous Formation Flying Mission of SNUGLITE-III CubeSat
Shim, H., Bae, Y., Hwang, J. W., Kee, C., & Koo, I. H. (2023). Single Frequency RTK Relative Navigation for Autonomous Formation Flying Mission of SNUGLITE-III CubeSat. In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation (pp. 1474-1486). Institute of Navigation. doi:10.33012/2023.19371
Real-time Software Verification Technique of Attitude Determination and Control System for CubeSat
Shim, H., Bae, Y., & Kee, C. (2023). Real-time Software Verification Technique of Attitude Determination and Control System for CubeSat. Journal of the Korean Society for Aeronautical & Space Sciences, 51(3), 207-216. doi:10.5139/jksas.2023.51.3.207
Verification of Space GPS Receiver Navigation Performance Based on Full-Orbit Navigation Solutions of CubeSat
Park, J., Shim, H., Bae, Y., Kee, C., & Yu, S. (2023). Verification of Space GPS Receiver Navigation Performance Based on Full-Orbit Navigation Solutions of CubeSat. In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. doi:10.33012/2023.18600
Development of Hardware-in-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer
Shim, H., Kim, O. -J., Park, M., Choi, M., & Kee, C. (2023). Development of Hardware-in-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer. IEEE Access, 11, 73164-73179. doi:10.1109/access.2023.3294565
2022
Probabilistic Determination Algorithm for Detumbling and Angular Rate Convergence using a Three-Axis Magnetometer
CHOI, M., KIM, O. -J., KIM, H., SHIM, H., & KEE, C. (2022). Probabilistic Determination Algorithm for Detumbling and Angular Rate Convergence using a Three-Axis Magnetometer. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 65(2), 76-83. doi:10.2322/tjsass.65.76
2020
In-Orbit Results and Attitude Analysis of the SNUGLITE Cube-Satellite
Kim, O. -J., Shim, H., Yu, S., Bae, Y., Kee, C., Kim, H., . . . Choi, Y. (2020). In-Orbit Results and Attitude Analysis of the SNUGLITE Cube-Satellite. Applied Sciences, 10(7), 2507. doi:10.3390/app10072507
Verification of Space GPS Receiver Navigation Performance Using a Cube Satellite
Yu, S., Kim, O., Shim, H., Bae, Y., Kee, C., Kim, H., . . . Choi, W. (2020). Verification of Space GPS Receiver Navigation Performance Using a Cube Satellite. In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. doi:10.33012/2020.17174
2018
Development and Verification of Attitude Determination and Control Algorithm for "SNUGLITE" Cube Satellite
Choi, M., Yu, S., Kim, O. -J., No, H., Shim, H., & Kee, C. (2018). Development and Verification of Attitude Determination and Control Algorithm for "SNUGLITE" Cube Satellite. In The International Technical Meeting of the The Institute of Navigation (pp. 56-71). Institute of Navigation. doi:10.33012/2018.15534