의사위성을 이용한 비행실험 Apr 14, 2006· Taikjin Lee Ghangho Kim Hyoungmin So Changdon Kee · 0 min read Last updated on Apr 14, 2006 Authors Taikjin Lee Ph.D Authors Ghangho Kim Ph.D Authors Hyoungmin So Ph.D Authors Changdon Kee Professor ← High Accuracy Pseudolite-based Navigation System: Compensating for Right-H Circularly Polarized Effect May 1, 2006 A New Technology for GNSS Signal Fast Acquisition within Three Seconds, Applicable to Current GNSS Receivers Jan 1, 2006 →