Presentation Summary How Beacons are Located Using Low Earth Orbit (LEO) Satellites Requires Highly accurate Orbit information and Very Stable Beacon Oscillator.

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Presentation transcript:

Presentation Summary How Beacons are Located Using Low Earth Orbit (LEO) Satellites Requires Highly accurate Orbit information and Very Stable Beacon Oscillator Description Of Doppler Shift Ambiguity Resolution (side “A” or “B” Determination)

Satellite Types Two types of satellites: w LEO satellites in near-polar orbit w Geosynchronous earth orbiting (GEO) satellites (cannot provide Doppler info)

Determining Beacon Locations From LEO Doppler Data T1 T2 T3 850 km 3400 km Distress Beacon GEOMETRY FOR OVERHEAD PASS Frequency High Actual Low Time DOPPLER SHIFT CAUSES FREQUENCY TO APPEAR HIGHER THAN ACTUAL DOPPLER SHIFT CAUSES FREQUENCY TO APPEAR LOWER THAN ACTUAL TIME OF CLOSEST APPROACH (AND ACTUAL FREQUENCY)

Processor and On-Board Memory COSPAS-SARSAT Processor and On-Board Memory SAR Processor Extracts the beacon ID Measures the signal’s frequency Time tags the frequency measurement On-Board Memory Stores the processed data Continually transmits the stored data (typical hold time is several hours) 406 MHz Beacon SAR Processor LUT Ground Station Local User Terminal

Doppler Curve (Processed by LUT) Satellite S4, orbit 12587 1991 MAR 05 18:16:31.80 Doppler Curve (Processed by LUT) Max Elevation 60o 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 Time (secs) Frequency (kHz)

Time of Closest Approach (TCA) Satellite S4, orbit 12587 1991 MAR 05 18:16:31.80 Time of Closest Approach (TCA) TCA Occurs at Zero Doppler Shift 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 Time (secs) Frequency (kHz)

Typical Doppler Curves Doppler Frequency vs. Time -10 -8 -6 -4 -2 2 4 6 8 10 5 15 20 Time (minutes) Frequency (KHz) TCA Pass 1 (High Elevation) Pass 2 (Low Elevation)

First Location (A / B Ambiguity) Gnd Trk Pass 1 (time is measured along gnd trk) 1A 1B Longitude Latitude TCA

A / B Ambiguity Resolved Gnd Trk Pass 1 Gnd Trk Pass 2 1A 1B 2A 2B Longitude Latitude

Two Pass, Merged Location Gnd Trk Pass 1 Gnd Trk Pass 2 1B 2B Longitude Latitude Merged Location

Ground Track and Field of View T2 -T1 = 101 minutes D longitude – 25 Deg.

Resolving Location Ambiguity 1 LEGEND: ground tracks of successive spacecraft orbits 1A, 1B Real and Image solutions from pass 1 2A, 2B Real and Image solutions from pass 2 2 2B 1B 2A 1A Two Pass Solution for a Beacon Located in Brazil