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2.1 Introduction and Overview
The Airborne Multi-Spectral Scanner (AMSS) is a scanning spectrometer which flies on a Beechcraft-200 aircraft and provides spectral information similar to that which will be provided by the Global Imager (GLI) scheduled to be launched on the ADEOS-II platform in 1999.
The AMSS spectrometer acquires high spatial resolution imagery in the range of 0.40 to 12.45 microns. Total of 59 spectral bands are available in this range. AMSS Record and Prcessing System was configured for each mission to record a pre-selected group of 46 signal No. in 14-bit resolution.
The AMSS spectrometer is mated to a scanner sub-assembly which collects image data with an IFOV of 2.5 mrad, giving a ground resolution of 5 meters in 54 spectral bands and IFOV of 5.0 mrad, giving a ground resolution of 10 meters in 5 spectral bands from 2000 meters altitude , and a cross track scan width of +/- 40 degrees.
AMSS Instrument/Platform Specifications (1)
Wavelength Range /Center Wavelength | Bandwidth | IFOV | SNR,NEDT, at 50% albedo, 300k |
400 - 800 nm | 10-30 nm (variable) | 2.5*1.25 mrad | 23000-500 |
800 - 890 nm | 10-30 nm (variable) | 2.5*1.25 mrad | 6000-1300 |
890 - 1000 nm | 10-30 nm (variable) | 2.5*1.25 mrad | 1200-100 |
1050 nm | 20 nm | 5.0 mrad | 120 |
1240 nm | 20 nm | 5.0 mrad | 80 |
1650 nm | 200nm | 5.0 mrad | 420 |
2215 nm | 270nm | 5.0 mrad | 80 |
3.715 nm | 0.33um | 5.0 mrad | 0.15 |
7.5 um | 0.5 um | 2.5 mrad | 0.15 |
8.30 um | 0.5 um | 2.5 mrad | 0.11 |
10.85 um | 1.0 um | 2.5 mrad | 0.07 |
11.95 um | 1.0 um | 2.5 mrad | 0.08 |
AMSS Instrument/Platform Specifications (2)
System Parameters | Scanning Method | Conical Scan |
Scan Rate | 41.6 Hz |
Swath angle | +/-40 deg |
Dispersion Method | 0.4-1.0 micrometer: 2grating |
1.0-12 micrometer: filter |
Instrument Mass | 200 Kg |
Instrument Size | 846*568*533(mm) |
Data Processing | Quantization | 14 bit |
Recording Media | 1 VLDS |
Data Rate | 4 MByte/s |
Max. No. of bands to be recorded | 46 |
Flight Parameters | Platform | Beechcraft-200 aircraft |
Flight Altitude | 1000 - 8000 m |
Ground Speed | 150 kt |
Visible Calibration | Integrating sphere on the ground |
Infrared Calibration | Two black bodies on board |
Return to AMSS Contents
Earth Observation Research Center
National Space Development Agency of Japan
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