Innovative Orbit and Space Mission Design
Metis specializes in flight dynamics design for High Earth Orbit, cislunar, lunar, and planetary missions operating in gravitational environments and operational regimes far more complex than conventional LEO or GEO missions. Our team supports mission development from early concept formulation through flight operations and end-of-mission disposal, with expertise in mission orbit design, transfer trajectory analysis, orbit determination, navigation, long-duration propagation, and operations for spacecraft affected by multi-body dynamics, lunar resonances, challenging long-term orbital behavior, and navigation in complex gravitational environments. Recent accomplishments include developing and operating NASA’s ACS3 Advanced Composite Solar Sail System Flite/FDS Lite flight data system, automating orbit determination solutions, OEM generation, solar-sail attitude modeling, ephemeris prediction, reporting, and CARA uploads. In support of cislunar orbital mechanics, Metis maintains and applies prototyping tools for relative motion in eccentric, high-altitude orbits.
Additional Metis experience includes leading flight dynamics activities for the Lunar Atmosphere and Dust Environment Explorer mission, creating an unprecedented equatorial lunar orbit for the Dark Ages Radio Experiment mission, and proposing innovative lunar-resonant orbit solutions for X-ray spectroscopy on the Arcus mission and in-situ solar plasma studies on HelioSwarm.
