최근 본 자료

추천 연관자료

• Collision Avoidance Maneuver Planning Using GA for LEO and GEO Satellite Maintained in Keeping Area
• Satellite load profile in normal operation: (a) 20% mission load profile, (b) 10% mission load with 30° roll maneuver, 2% mission with 56° roll maneuver, and 2% mission with 30° pitch maneuver
• Model Identification and Attitude Control Methodology for the Flexible Body of a Satellite
• Visibility Analysis of Domestic Satellites on Proposed Ground Sites for Optical Surveillance
• Collision Avoidance Using Linear Quadratic Control in Satellite Formation Flying