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.