Microsoft PowerPoint LULCws-ALOS23.pptx
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1 ALOS 2/3 の概要について 第 2 回 JAXA 土地被覆ワークショップ 2012 年 5 月 25 日 田殿武雄 1, 鈴木新一 2, 今井浩子 2 1 地球観測研究センター 2 ALOS 2 プロジェクト 宇宙航空研究開発機構
2 ALOS シリーズ 宇宙を活用した安心 安全で豊かな社会の実現のため 公共の安全確保 国土保全 管理 食糧 安全で豊かな社会の実現のため資源 エネルギーの確保 地球規模の環境問題 ( 低炭素社会の実現 ) の解決等のニーズに応え 陸域 海域観測を行うことを目的とする 平成 18 年 1 月 平成 23 年 5 月 平成 25 年度平成 27 年度以降 だいち (ALOS) ALOS 2 ( 合成開口レーダ ) ( 光学 & 合成開口レーダ ) ALOS 3 ( 光学センサ ) 夜間 悪天候でも 最大 490km の広観測幅 最高分解能 1m~3m の合成開口レーダを搭載 ALOS-2 ( 合成開口レーダ (SAR)) ( 平成 25 年度打上げ ) だいち (ALOS) ( 光学センサ & 合成開口レーダ (SAR)) ( 平成 18 年 1 月 ~ 平成 23 年 5 月 ) 最大 50km の広観測幅 最高分解能 0.8m の光学センサを搭載 ALOS-3 ( 光学センサ ) ( 平成 27 年度以降打上げ ) 2
3 ALOS-2 Mission ALOS-2 has superior performance compared with ALOS. ALOS-2 will achieve significant contributions to: Disaster Monitoring i - quick access to damaged areas and continuous monitoring - InSAR for deformation Land Monitoring - generate systematic archive - sea ice monitoring Agricultural Monitoring - evaluation of irrigated rice fields Natural Resource Exploration - detecting oil slick over sea -analysis of geology gy and topography p Global Forest Monitoring - deforestation monitoring Potential Use -maritime safety 3
4 ALOS-2 Satellite ALOS-2 in-orbit configuration Specification Y Z X Data relay antenna L-band SAR (PALSAR-2) Observation mode Stripmap: 3 to 10m res.,50 to 70 km swath ScanSAR: 100m res., 350km/490km swath Spotlight: 1 3m res.,25km swath Solar Arrays Orbit Sun-synchronous orbit Altitude: 628km Local sun time : 12:00 +/- 15min Revisit: 14days Orbit control: +/-500m Life time 5 years (target: 7 years) L-band SAR antenna X-band downlink antenna Launch Downlink JFY2013, H-IIA launch vehicle X-band: 800Mbps(16QAM) 400/200Mbps(QPSK) Ka-band: 278Mbps (Data Relay) Experimental Compact InfraRed Camera (CIRC) 4
5 Improvement on ALOS-2 ALOS ALOS 2 Recurrent cycle 46 days 14 days Observable area approx. 870km (Right looking) approx. 2320km (Left & Right looking) Spatial 10m (Stripmap) 1-3m (Spotlight), Resolution 3m/6m/10m / (Stripmap) p) Downlink 138Mbps (X-band) & Data Relay Satellite 800Mbps (X-band) & Data Relay Satellite 5
6 PALSAR-2 Imaging Mode 70 Rg Az observation area: approx.1160km (right or left) 50 km Stripmap swath:50 or 70km 350 km 25 km x 25km Spotlight swath:25km x 25km ScanSAR swath:5scans 350km 7scans 490km Observable area : Right or left-looking by spacecraft maneuvering at 30 degrees off-nadir with electric beam steering using active phased array antenna (incidence angle from 8 to 70 degrees). 6
7 ALOS-2 Observable Area (Strip map mode) Observation area: looking Observation area: left looking Stripmap mode: Swath:50km or 70km 7
8 ALOS-2 Observable Area (ScanSAR mode) Next Orbit (100min later of first orbit) ScanSAR S is very effective ec e for wide area observations such as: First Orbit Disaster monitoring (Flood, Earthquake, etc.) Oceanographic observation (Sea ice monitoring, etc.) ScanSAR Mode (Swath: 350km or 490km) Observable area of ScanSAR Mode (right looking case) 8
9 PALSAR-2 Specification High ScanSAR ScanSAR Spotlight Ultra Fine Fine sensitive nominal wide Bandwidth 84MHz 84MHz 42MHz 28MHz 14MHz 28MHz 14MHz Rg Az: Resolution 3m 6m 10m 100m(3 looks) 60m(1.5 looks) 3 1m Rg Az: 350km 490km Swath 50km 50km 70km 25 25km 5scan 7scan Polarization SP SP/DP SP/DP/FP/CP SP/DP NESZ -24dB -24dB -28dB -26dB -26dB -23dB -23dB Rg 25dB 25dB 23dB 25dB 25dB 20dB S/A Az 20dB 25dB 20dB 23dB 20dB 20dB SP : HH or VV or HV, DP : HH+HV HV or VV+VH VH, FP : HH+HV+VH+VV HV VH VV, CP : Compact pol (Experimental mode) Spotlight : Ultra Fine: High sensitive: Fine: ScanSAR nominal : ScanSAR wide: Detail observation of damaged area Basemap Flood / Coast monitoring Global forest monitoring ScanSAR InSAR (28MHz) Ice monitoring, Ship detection 9
10 PALSAR-2 Simulated Image Example: Identification of urban buildings around Tokyo Disneyland) PALSAR-2 enables to create maps with a scale of 1 to 100,000 and to identify roads. ALOS/PRISM Optical Image (2.5m) 0 The shapes of the buildings in red circles can be identified. 1 km 10
11 Quick Tasking and Quick Processing Command will be ready within 60 minutes for emergency observation. Disa ster <30min <60min <30min JAXA Tracking Network ALOS-2 SC controller Emergency 求調Request 整要Mission Planner Mod ify Plan Uplink TT&C CMD reg. SC maneuvering SAR Observation User Information System SC Control & Mission Ops System AOCS MDHS Record/Repro 800Mbps Visualization Product delivery Data Prcessor L0 processing L1 processing Demodulator Demod DRTS DT DRC <30min <30min Mbps <60min Emergency product will be ready within 60 minutes after downlink. 11
12 Basic Observation Scenario (global) Systematic acquisition is crucial to achieve mission requirements. Ascending Fine(10m) HH+HV (Global) Descending Ultra Fine(3m) HV (Global) Descending ScanSAR HH+HV (Deformation) Ascending High Sensitive(6m) (Full Polarimetry Descending Fine(10m) HH+HV (Deformation) Descending ScanSAR HH+HV (Forest) Ascending ScanSAR HH+HV (Polar) Descending Fine(10m) HH+HV (Forest) Descending ScanSAR HH+HV (Wetland) Several patterns of observation mode, time and location will be prepared. 12
13 Compact InfraRed Camera (CIRC) CIRC features compact (size, weight) and low power large format non-cooling microbolometer low cost 181mm Y X Z 106mm Parameter Size Detector Mass Specification < 18cm x 10cm x 20cm Microbolometer (SOI diode) < 3kg Power <20W Wavelength Number of pixels Spatial resolution Field of View Dynamic range 8-12 μm 640 x 480 < 200 km (< 0.33 mrad) 12 x 9 ( km) 180 K K 206mm NEdT 0.2 K@300 K 13
14 ALOS-2 PFM Integration and Testing (satellite bus) SAR antenna RF testing in a vacuum chamber ALOS-2 Research Announcement (RA) will release on July
15 ALOS-3 衛星システムの概要 HISUI ( マルチ ) HISUI ( ハイパー ) PRISM-2 ( パンクロ後方視 ) PRISM-2 ( パンクロ直下視 ) 軌道上想定図 軌道種類 : 太陽同期準回帰軌道 回帰日数 : 60 日 ( 概回帰 5 日 ) 降交点通過太陽地方時 : 10:30 設計寿命 : 5 年 センサ PRISM 2 直下視後方視 HISUI( 経済産業省開発 ) ハイパーマルチ 地上分解能 (GSD) / 観測幅 / バンド 0.8m / 50km / 1 バンド <2.5m ( 検討中 ) / 50km ( 検討中 ) / 1 バンド 30m / 30km / 185 バンド ( μm) 5m / 90km / 4 バンド ( μm) 15
16 ALOS-3 Mission ALOS-3 will succeed ALOS missions, as well as build advanced techniques for land observation using optical imagers. Disaster Monitoring Updating of geographical information ato as the ebase map, creating ceat gof hazard aadmaps, estimation of precise runoff analysis, evaluation of active faults. Support of disaster management activities via fast access to damaged areas. Land Monitoring Creation and updating of topographic maps in Japan (with 1/25,000 scale or more) and other countries. Agricultural l and Coastal Fishing Monitoring i Monitoring of cropping situation and growing condition, understanding of the damage to wet paddy rice by typhoons, monitoring of outbreak of red tide. Natural Resource Exploration Development of advanced resource exploration methods from space. Global Environmental Monitoring Quantitative verification of deforestation and forest degradation, evaluation of wetlands, research of coral reef, monitoring of glaciers and glacial lakes. 16
17 Major Specifications of ALOS-3 Observation Orbit Life time Panchromatic GSD : 0.8m, Swath : 50km (nadir) Stereoscopic image acquisition by 2 telescopes Multi spectral (VIS NIR, 4Bands) GSD:5m,Swath:90km Hyperspectral (VIS SWIR SWIR, 185Bands ) GSD : 30m, Swath : 30km Thermal infrared (TIR, GSD:200m) *Experimental Sun synchronous orbit Altitude: 618km Local sun time : 10:30 Revisit: 60days 5 years (Target: 7 years) PRISM-2 HISUI Launch H IIA launch vehicle Downlink 400/800Mbps (Via Data Relay Satellite) 400/800Mbps (Direct Transmission) * Multispectral and hyperspectral sensors are develped by METI 17
18 Concept of PRISM-2 Wide swath and high resolution Wide swath (>50km) and high resolution (<1m) is very important when a major disaster occurs, such as Tohoku tsunami. Accurate stereo mapping for large area Accurate stereo mapping by two telescopes with fine resolution enables large scale geographical information including elevation. Wide coverage and high geo-location accuracy Image collection with high duty and high geo location accuracy is necessary to produce base maps to be used in many applications. 18
19 Enhanced Capabilities of PRISM-2 ALOS/PRISM * Pan, nadir ALOS-3/PRISM-2 GSD (Pan) Swath SNR Data quantization Pointing Data downlink Geo-location accuracy 2.5 m 35 km/70 km > 70 8 bit ±1.5 (CT) 240Mbps (Ka-band) 120Mbps (X-band) 6.1m (RMS) 0.8 m 50 km > bit ±60 (cone) 800Mbps (X and Ka-band) Better than PRISM 19
20 Concepts of Image Collection (Global mapping) ALOS 3 collects images continuously along the satellite s track with an extraordinarily high duty cycle (>3,000,000km 2 /day (Pan+Mu)) Continuous image acquisition (for large scale geospatial information) ALOS 3 produces precise digital surface models (DSMs) for large area by stereo pair images acquired with two telescopes. Backwardlooking Nadirlooking 20
21 Concepts of Image Collection (Disaster monitoring) ALOS 3 enables to direct the sensor s view to any points in a wide area (±60 ) by satellite body pointing to achieve timely monitoring i when a disaster occurs. Image acquisition by pointing (for disaster monitoring) N+1 rev. N rev Field of Regard (±60deg) 21
22 ALOS-3 Simulated Image Panchromatic image ((Yokohama, Japan) p ) JAXA Pasco ALOS GSD 2.5m (Jan 19, 2009 JAXA) ALOS-3 ALOS 3 (GSD 0.8m) (Simulated image using airborne image (ADS-40, Dec Pasco) 22
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