Research
Space exploration Flight Mission Control Lab.
Space exploration Flight Mission Control Lab.
Our lab conducts research not only from a theoretical perspective but also with a strong emphasis on practical applications to ensure mission success. In the field of interplanetary mission design and analysis, our work covers Lunar, Mars, Jupiter, and Asteroid missions, CubeSat missions, asteroid deflection, and mission requirements generation and analysis. In astrodynamics, we focus on trajectory and orbit optimization, spacecraft orbit and attitude determination and control, as well as mission design and analysis for Low Earth Orbit (LEO) and Geostationary Earth Orbit (GEO). In spacecraft ground system design, development, and operations, our expertise includes ground system engineering, ground system requirements generation and analysis, interface control, and the design, development, and operation of flight dynamics systems.
Interplanetary (Lunar, Mars, Jupiter, Asteroid etc.) Mission
CubeSat Mission
Asteroid Mission including Deflection
Mission Requirements Generation & Analysis
Trajectory & Orbit Optimization
Spacecraft Orbit & Attitude Determination, Control
LEO, GEO Mission Design & Analysis
Ground System (GS) Engineering
GS Requirement Generation & Analysis, GS Interface Control
Flight Dynamics System (FDS) Design, Development & Operation, etc.
17104 경기도 용인시 기흥구 덕영대로 1732 경희대학교 우주과학과/우주탐사학과
© 2025 우주탐사 비행임무관제 연구실. 모든 권리 보유.
Dept. of Astronomy & Space Science / School of Space Research, Kyung Hee University, 1732, Deogyeong-daero, Giheung-gu, Yongin-si, Gyeonggi-do 17104, Republic of Korea
© 2025 Space exploration Flight Mission Control Lab. ALL RIGHT RESERVED.