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Global Positioning System Overview

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Presentation on theme: "Global Positioning System Overview"— Presentation transcript:

1 Global Positioning System Overview
Author: Peter H. Dana Herman Li Oct 18, 2004

2 NAVSTAR-2 GPS satellite
What is GPS GPS = Global Positioning System Position, velocity, time Network of min. 24 (29) satellites, orbiting the earth every ~12 hours Funded and controlled by the US DOD Cost: 13 billion US Significant advantage in used in middle east 29 in sky (Saturday), 24 minimum Pass by same area twice a day Unofficial: on Dec 8, 1993 Fully operational: on Apr 27, 1995 Outdoor use only NAVSTAR-2 GPS satellite

3 Space Segment Altitude of 20,000km
Positioned such that 5 – 8 satellites are in range at any time Coded radio signals from 4 satellites can pinpoint location on earth 6 orbital planes Used for position, velocity, time 6 orbital planes, 4 SV each, equally spaced (60 deg apart), inclined at ~55 deg wrt equatorial plane 4 satellites locate 3D position

4 Trilateration 1 satellite – a sphere 2 satellites – a circle
3 satellites – 2 points ECEF XYZ coordinates Distance = Travel Time x Speed of Light Trilateration (based on known position + distance) vs triangulation (based on angle + distance) 1,2,3 satellites Distance formula Assumed location known CLICK!! Where are the satellites Gravatational pull…etc changes orbit Time inaccurate Where are the satellites Time is different in the sky

5 Control Segment 1ns drift / 3 hours 1ns = ~30cm error
5 monitor stations 3 ground antennas Radars located around the world GPS broadcasts received ephemeris and clock correction data to receivers Practically few ns error = ~ 1m 10cm/h, 2.4m/day Radar uploads ephemeris + clock corrections to GPS, GPS broadcasts

6 Positioning Services Precise Positioning Service (PPS)
22m horizontal, 27.7m vertical accuracy 200ns accuracy Standard Positioning Service (SPS) 100m horizontal, 156m vertical accuracy (SA included) 340ns accuracy SA turned off as of May 2, 2000 Have accurate clocks, know where satellites are, need to find the distance PPS – more accurate (explain later) SPS – less accurate SA – degration of SPS in time varying bias (30m – 100m)

7 GPS Satellite Signals Two microwave carrier signals
L1 ( MHz) L2 ( MHz) L5 band coming Speed of light varies Ionosphere slows down lower frequencies more Use L1 & L2 to remove ionosphere effects Difference in arrival time removes error Moisture in Troposphere also slows down signal Reason of L1 + L2 L1 + L2 offset ionosphere Only special receivers has L2

8 GPS Satellite Signals C/A (Coarse/Acquisition) Code
a.k.a Civilian Code Unique pseudo-random-noise (PRN) code modulated on L1 and repeated every 1ms P(Y)-Code (Precise Code) PRN code modulated on both L1 and L2 and repeated every 7 days Codes used for downloading ephemeris every 30 sec and almanac every 12.5 min PRN code unique, 32 Know which satellite signal was from P encrypted with Y = P(Y) Need special hardware to decrypt Anti-spoofing = avoid fake transmission Anti-jamming by using code Ephemeris = short sections of satellite orbits

9 GPS Data 1.5 kbit frame, 5 subframe, 30 sec
25 pages subframe = almanac + other data Almanac, predict where any satellite appears (orbital data for all satellites) Used when starting up unit Complete SV data set includes ionospheric model Send offset of GPS time / UTC time Parity bits provide error detection / limited correction

10 GPS Signals

11 Code Phase Tracking (Navigation)
Uses C/A or P(Y) code Gets pseudo-range, includes eroror and receiver clock error Know: prefect clock, distance = travel time X speed of light

12 Clock synchronization
Satellites have 4 atomic clocks Receivers are cheap, 1us drift / sec Assuming distance from satellites already known, 4th satellite solves the extra variable 4 atomic clock (2x cesium, and 2x rubidium) Satellite = accurate clock Receiver = inaccurate clock

13 Differential Code Phase GPS
Base station (known position) computes corrections for each satellite signal Corrections sent to rover receivers Removes errors except multipath and receiver errors US Coast Guard combats SA

14 Carrier Phase Tracking (Survey)
Requires specially equipped receivers Track L1 and/or L2 carrier signals No time of transmission info Requires differential calculations of receivers within km Sub-cm accuracy possible

15 Differential GPS DGPS – Differential Code Phase GPS
Instantaneous results, less accurate Real-time or post-processed CPD – Carrier Phase Differential Increased accuracy due to increased frequency RTK – Real-time Kinematic ie. Real-time Carrier Phase Time to determine initial full cycles, accurate Time + position already discussed Velocity = change in position over time Or Doppler frequencies.

16 GPS Error Sources PRN code noise (1m), receiver noise (1m)
Selective availability (no longer the case) Uncorrected satellite clock error (1m) Ephemeris data errors (1m) Tropospheric delays (10m) Unmodeled ionosphere delays Multipath (0.5m) Geometric Dilution of Precision (GDOP) Bad when angles between receiver and satellites are similar Bias, Noise, Blunders Uncorrected satellite clock: 10cm/hr Human error, hardware failure

17 GDOP Example

18 User Equipment Segment
GPS receivers and user community Cheap outdoor GPS ~ $180US Outdoor GPS with map ~ $375US Personal GPS with street map ~ $590US Avionics GPS ~ $?? Ability to locate yourself anywhere on the globe: Priceless

19 Now and Beyond WAAS (Wide Area Augmentation System) GLONASS Galileo
FAA + DOT for precision flight approaches Corrected differential messages broadcast by 2 geostationary satellites Glonass: horizontal 57 – 70m vertical 70m, 24 satelliltes, 19km, 3 orbits Galileo: Civil system, 30 satellites, 24km orbit, 3 orbits GLONASS Russian Federation’s satellite navigation system (2006) Galileo European Union and European Space Agency (2008)

20 References Questions: Position, Time & GPS – confusing
A GPS Tutorial FAA GPS FAQ GPS Overview How GPS Receivers Work The Fundamentals of GPS DGPS Explained USNO GPS Timing Operations Garmin Questions: Position, Time & GPS – confusing Why time in 3 different position location methods

21 Time Dilation “Net secular relativistic effect is 38.6s per day
Nominal clock rate is MHz Satellite clocks are offset by – parts in 1010 to compensate effect Resulting (proper) frequency in orbit is Hz Observed average rate of satellite clock is same as clock on the geoid”  “Relativity has become an important practical engineering consideration for modern precise timekeeping systems. These relativistic effects are well understood and have been applied successfully in the GPS.” summaryrpts/41stmeeting/18%20Nelson%20.PPT


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