作者: T. YUNCK , S. WU
DOI: 10.2514/6.1986-404
关键词: Global Positioning System 、 Medium Earth orbit 、 Assisted GPS 、 Position (vector) 、 Precise Point Positioning 、 Satellite navigation 、 Geography 、 Orbiter 、 Remote sensing 、 Decimetre
摘要: A technique is described for employing the Global Positioning System (GPS) to determine position of a low earth orbiter with decimeter accuracy without need user dynamic models. differential observing strategy used requiring GPS receiver on vehicle and network six ground receivers. The uses continuous record change obtained from carrier phase smooth measurements made pseudo-range. result computationally efficient that can deliver down lowest altitude orbits.