High Accuracy Pseudolite-based Navigation System: Compensating for Right-H Circularly Polarized Effect May 1, 2006· Haeyoung Jun Changdon Kee · 0 min read DOI Last updated on May 1, 2006 Authors Haeyoung Jun Ph.D Authors Changdon Kee Professor ← Enhanced method for single-antenna GPS-based attitude determination Jun 1, 2006 의사위성을 이용한 비행실험 Apr 14, 2006 →