Accession Number:

ADA614967

Title:

Expected Position Error for an Onboard Satellite GPS Receiver

Descriptive Note:

Master's thesis

Corporate Author:

AIR FORCE INSTITUTE OF TECHNOLOGY WRIGHT-PATTERSON AFB OH GRADUATE SCHOOL OF ENGINEERING AND MANAGEMENT

Personal Author(s):

Report Date:

2015-03-01

Pagination or Media Count:

112.0

Abstract:

The Global Positioning System GPS constellation provides ranging information that delivers inexpensive, high precision positioning for terrestrial users. Satellites in Low Earth Orbit LEO can use an onboard GPS receiver resulting in meter-level navigation solution accuracy. There are limitations to using GPS for positioning for satellites above LEO. The number of GPS satellites whos signal can be received decreases as the receivers altitude approaches that of the GPS constellation. Above the GPS constellation, the available GPS signals for ranging will originate from satellites on the opposite side of Earth. This research calculates the available GPS signals to the receiver and determines the expected position error, while considering the effects from a low signal to noise ratio, poor geometry, and signal shift caused by high relative velocity.

Subject Categories:

  • Electrical and Electronic Equipment
  • Navigation and Guidance

Distribution Statement:

APPROVED FOR PUBLIC RELEASE