최근 본 자료

추천 연관자료

• Spacecraft Formation Reconfiguration using Impulsive Control Input
• Aerodynamics Investigation for Prospective Spacecraft Vehicle in the Transitional Regime
• An Earth-Moon Transfer Trajectory Design and Analysis Considering Spacecraft’s Visibility from Daejeon Ground Station at TLI and LOI Maneuvers
• Spacecraft Guidance Algorithms for Asteroid Intercept and Rendezvous Missions
• Precise attitude determination strategy for spacecraft based on information fusion of attitude sensors: Gyros/GPS/Star-sensor