의사위성을 이용한 비행실험Apr 14, 2006·Taikjin LeeGhangho KimHyoungmin SoChangdon Kee· 0 min readLast updated on Apr 14, 2006 AuthorsTaikjin LeePh.DAuthorsGhangho KimPh.DAuthorsHyoungmin SoPh.DAuthorsChangdon KeeProfessor Emeritus← High Accuracy Pseudolite-based Navigation System: Compensating for Right-H Circularly Polarized Effect May 1, 2006A New Technology for GNSS Signal Fast Acquisition within Three Seconds, Applicable to Current GNSS Receivers Jan 1, 2006 →