Advanced Meteorological Imager (AMI) Development for GEO-KOMPSAT-2A
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1 1 st KMA International Meteorological Satellite Conference Advanced Meteorological Imager (AMI) Development for GEO-KOMPSAT-2A 16 November 2015 Koon-Ho YANG Korea Aerospace Research Institute 1
2 Agenda National Satellite Development Plan Follow-on Satellites of COMS GEO-KOMPSAT-2 System Architecture GEO-KOMPSAT-2A (GK2A) - Missions - Satellite Overview - GK2A Instruments - Electrical Testbed - Structure Thermal Model Advanced Meteorological Imager (AMI) - AMI Requirements - AMI Design - AMI Development Status 2
3 National Satellite Development Plan 1993 KITSAT KISTAT KOMPSAT STSAT KOMPSAT /2010 STSAT COMS(GEO-KOMPSAT-1) 2012 KOMPSAT KITSAT-1 Lunar Lander 2020 Lunar Orbiter 2013 STSAT KOMPSAT KOMPSAT GEO-KOMPSAT-2B 2018 GEO-KOMPSAT-2A 2018 CAS CAS KOMPSAT-3A 3
4 Follow-on Satellites of COMS [GEO-KOMPSAT-2A] Instruments - Advanced Meteorological Imager (AMI) - Korean Space Weather Monitor (KSEM) Mission Lifetime : 10 years Launch Mass : 3.5 ton [COMS] Instruments - Meteorological Imager (MI) - Geostationary Ocean Color Imager (GOCI) - Ka-band Communication Payload Mission Lifetime : 7 years Launch Mass : 2.5 ton [GEO-KOMPSAT-2B] Instruments - GOCI-II - Geostationary Environment Monitoring Spectrometer (GEMS) Mission Lifetime : 10 years Launch Mass : 3.2 ton 4
5 GEO-KOMPSAT-2 System Architecture NMSC : National Meteorological Satellite Center SOC : Satellite Operation Center KOSC : Korean Ocean Satellite Center ESC : Environment Satellite Center LRIT: Low Rate Information Transmission HRIT : High Rate Information Transmission TM/TC : Telemetry/Telecommand 5
6 GEO-KOMPSAT-2A Missions Meteorological Mission - Continuing and Enhancing COMS meteorological observation mission - Monitoring weather and climate phenomena with enhanced measurement cycle - Monitoring more accurately high-impact weather events with high spatial resolution Space Environment Monitoring Mission - Monitoring of space weather phenomena : Measurement of energetic particle flux and magnetic field in the GEO-orbit : Monitoring of GK2A spacecraft charging 6
7 GEO-KOMPSAT-2A Overview Mission Lifetime : 10 years Orbital Location : East (GEO) Launch Mass : 3.5 ton Launch : May 2018 by Ariane 5 Solar Array Power : End of Life S-band Horn Ant. (ODCS) X-band Horn Ant. (ODCS) AMI Sensor Unit L-band Horn Ant. (ODCS) Star Trackers (AOCS) X-band Medium Gain Ant. (ODCS) KSEM PDs Solar Array Wing KSEM CM KSEM MG Deployed Boom AOCS : Attitude & Orbit Control Subsystem ODCS : Observation Data Communication KSEM : Korean Space Environment Monitor PD : Particle Detector MG : Magnetometer CM : Charging Monitor 7
8 GEO-KOMPSAT-2A Instruments Advanced Meteorological Imager (AMI) - Manufacturing & Assembling Phase - Contractor : Harris Corporation (former ITT Exelis) ABI PFM Korean Space Environment Monitor (KSEM) - Energetic Particle Detector, Magnetometer, Charging Monitor - Engineering Qualification Model Development Phase - Contractor : Kyung Hee University (Korea) 8
9 GEO-KOMPSAT-2A Development Schedule System Requirement Review(SRR) Meeting : (Completed) System Design Review(SDR) Meeting : ~ (Completed) Preliminary Design Review(PDR) Meeting : ~ (Completed) Critical Design Review(CDR)/EQSR Meeting : ~ (Completed) AMI Delivery : KSEM Delivery : GK2A Pre-Ship Review(PSR) Meeting : GK2A Launch :
10 GK2 ETB (Electrical Test Bed) 10
11 GK2 STM (Structure Thermal Model) 11
12 AMI Requirements 12
13 AMI Specification (1/2) Bands nadir SNR (Min.) 1/4 1/2 3/4 4/4 Dynamic Range VIS0.4 1km ~720W/m 2 /sr/um VIS0.5 1km ~710W/m 2 /sr/um VNIR VIS km ~620W/m 2 /sr/um VIS0.8 1km ~320W/m 2 /sr/um NIR1.3 2km ~114W/m 2 /sr/um MWIR LWIR NIR1.6 2km ~77W/m 2 /sr/um IR3.8 2km - 2.7K 0.18K ~400K IR6.3 2km K 0.10K ~300K IR6.9 2km K 0.10K ~300K IR7.3 2km K 0.10K ~320K IR8.7 2km K 0.10K ~330K IR9.6 2km K 0.10K ~300K IR10.5 2km K 0.10K ~330K IR11.2 2km K 0.10K ~330K IR12.3 2km K 0.12K ~330K IR13.3 2km K 0.30K ~305K 13
14 AMI Specification (2/2) FD (Full Disc) NH (Northern Hemisphere) ENH LA (Local Area) (Extended Northern Hemisphere) 14
15 GK2A AMI vs COMS MI GK2A AMI COMS MI Spectral Bands 16 channels 5 channels Spatial Resolution 0.64μm : 0.5km Other VIS/NIR : 1.0km IR : 2km 0.675μm : 1km Other VIS/NIR : N/A IR : 4km Observation Duration Full Disc 10minutes Full Disc 30minutes Lifetime 10 years 7 years On-board calibration Visible/IR IR 3 times Better Spectral Resolution 2 times Better Spatial Resolution 3 times Better Observation Duration Longer Lifetime 15
16 AMI Design 16
17 AMI Configuration (Photo Courtesy of Harris Corporation) 17
18 Field-of-View : 0.9 X 1.9 AMI Optical Design Large NS FOV : Slower Scan Rate, Higher SNR Field-of-Regard : 22 degrees (i.e. +/- 11 degrees) Two scan mirrors(ns, EW) SiC with silver coating Lower inertia and power Less disturbance : Scan parallel to equator w/o image rotation Two beam-splitters(s1,s2) VNIR, MWIR/LWIR FMA telescope Aperture 270mm Collecting sufficient photons for good SNR (Graphic Courtesy of Harris Corporation) 18
19 On-board Calibration - IR Band 3-bounce internal calibration target (ICT) Robust against stray-light and contamination Very high Emissivity : Located at anti-nadir Observe the black body target at the start of every operational timeline iteration 3-Bounce Black Body (Graphic Courtesy of Harris Corporation) 19
20 On-board Calibration - Visible Band Sola Calibration Target : Spectralon Diffuser Solar Calibration Cover open only when calibrating Solar calibration can occur any day of the year at 6:00~6:15 AM (Spacecraft local time) (Graphic Courtesy of Harris Corporation) Visible Light Diffuser (Spectralon ) (Photo Courtesy of Harris Corporation) 20
21 AMI Scan Pattern AMI Scan Pattern AMI Raster Scan : Constant time interval across swath boundary NS swath & Stare support vicarious calibration Angled swath can compensate for spacecraft yaw error (Graphic Courtesy of Harris Corporation) 21
22 Development Status of AMI 22
23 AMI manufacturing Status Summary Subcontracts and Material item procurements : On-schedule 8 out of 10 Major subcontract components : Delivered 2 out of 10 Major subcontract components : On-schedule Optical bench structure, Cable assemblies, Thermal blankets, Scanner sub assemblies, Active cooler, and IR calibration target completed Aft Optics and Optical port sub assemblies in build and testing process Optical Bench under assembly (Photo Courtesy of Harris Corporation) 23
24 AMI Enhanced Simulator Development AMI Enhanced Simulator Delivered to KARI on 3 rd August, 2015 Being used for the validation of AMI test GK2A system level Performed the interface test with PIU (Payload Interface Unit) of GK2A AMI enhanced simulator-piu Interface Test AMI enhanced simulator 24
25 AMI Development Schedule Effective Date of Contract(EDC) : (Completed) Kick-off Meeting : (Completed) System Requirement Review(SRR) Meeting : (Completed) Preliminary Design Review(PDR) Meeting : (Completed) Critical Design Review(CDR)/EQSR Meeting : ~ 3.3 (Completed) Test Readiness Review(TRR) Meeting : Pre-Environmental Review(PER) Meeting : Pre-Ship Review(PSR) Meeting : AMI Delivery :
26 Thank you!
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