-
-
Duality-based high-fidelity fuel-optimal impulsive trajectory generation for spacecraft rendezvous and formation flying
-
Development of a ground test facility for hardware-in-the-loop validation of multiple spacecraft operations
-
Enhancement of Spacecraft Attitude and Orbit Control Using Neuro-Fuzzy Approximation of the Optimal Controllers,
-
Precise orbit determination with satellite laser ranging observations using a batch filter based on particle filtering
-
Guidance, navigation, and control system simulations via integrated orbit and attitude hardware-in-the-loop simulator for satellite formation flying
-
Development and Experiment of Hardware-in-the-Loop Simulator for Autonomous Formation Flying Satellite
-
Mobile vehicle navigation by integrating global positioning system, inertial navigation system and polydioptric vision sensor
-
Development of Spaceborne GPS Receiver with Onboard Orbit Determination Using the Unscented Kalman Filter
-
Design of Optimal Trajectories for a Lunar Mission and Earth-Crossing object Deflection
-
Dynamics and Control of Spacecraft Formations: Reconfiguration and Tracking
-
Application of the Batch Filter based on the Sigma Point Sampling to Satellite Orbit Determination
-
Orbit Determination and Attitude Maneuver using the Earth Magnetic Field Measurements for Small Satellite
-
GPS Analysis of Crustal Velocities within Korean Peninsula and the East Asia
-
Precision Orbit Determination of the Low Earth Orbiting Satellite Using the GPS measurement
-
A Study on the Real Time Orbit Determination of Geostationary Satellite for Time Synchronization Service
-
비선형 제어기법을 이용한 인공위성 궤도 조정
-
Station-keeping for a satellite cluster in the same geostationary orbital arc
-
ζ Aur형 쌍성계에서 Stromgren구가 선 윤곽형성에 미치는 효과
