Spacecraft Mission and Control Lab.
@ Department Aeronautical and Astronautical Engineering, Korea Aerospace University
@ Department Aeronautical and Astronautical Engineering, Korea Aerospace University
Civil/Military Applications using Satellite System
Mission & System Design & Performance Analysis
Requirement Generation
AOCS FSW Development for Satellite Attitude Control
Attitude Estimation using Sensor Fusion
Attitude Control using Variable Actuators e.g. RWs, CMGs, MTQs and Thrusters
Trajectory Design for Rendezvous & Docking
Relative Navigation using Proximity Sensors
Guidance and Control for Far/Close Rendezvous