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

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2 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)

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

4 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)

5 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

6 Doppler Curve (Processed by LUT)
Satellite S4, orbit MAR :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)

7 Time of Closest Approach (TCA)
Satellite S4, orbit MAR :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)

8 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)

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

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

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

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

13 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


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