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Published byCaleb Jacobs
Modified over 4 years ago
ALOS Introduction JAXA/EORC
ALOS (1/2) Spacecraft MassApprox. 4 tons Generated PowerApprox. 7 kW (at End of Life) Design Life3 -5 years Orbit Sun-Synchronous Sub-Recurrent Repeat Cycle: 46 days Sub Cycle: 2 days Altitude: 691.65 km (at Equator) Inclination: 98.16 deg. Attitude Determination Accuracy 2.0 x 10 -4 degree (with GCP) Position Determination Accuracy 1m (off-line) Data Rate 240Mbps (via Data Relay Technology Satellite) 120Mbps (Direct Transmission) Onboard Data Recorder Solid-state data recorder (90Gbytes) 2
ALOS (2/2) InstrumentAcronymProvider Panchromatic Remote-sensing Instrument for Stereo Mapping PRISMJAXA Advanced Visible and Near Infrared Radiometer type 2 AVNIR-2JAXA Phased Array type L-band Synthetic Aperture Radar PALSARMETI/ JAXA 3
Data Acquisition Status Data Acquisition Results (PRISM Nadir, Cloud Cover < 20%) Data Acquisition Results. (AVNIR-2, Cloud Cover < 20%) Data Acquisition Results (PALSAR FBS mode) Data Acquisition Results. (PALSAR WB1 mode) 4 Target : 2006.5.16 ~ 2008.2.29
Data Acquisition Status Data Acquisition Results (PRISM Nadir, Cloud Cover < 20%) Data Acquisition Results. (AVNIR-2, Cloud Cover < 20%) Data Acquisition Results (PALSAR FBS mode) Data Acquisition Results. (PALSAR WB1 mode) 5 Target : 2006.5.16 ~ 2008.2.29
Environmental Application of Remote Sensing: CE 6900 Tennessee Technological University Department of Civil and Environmental Engineering Course Instructor:
Surface Water and Ocean Topography (SWOT) Satellite Mission
NOAA National Geophysical Data Center
Disaster Monitoring (1/3) 1 Wild fire in South California. Observed by AVNIR-2 on October 23, 2007 JST Wild fires struck southern California from October.
CEOS WGISS – 25 February 25-29, 2008 Sanya, Hainan Island, China Geo-Informatics and Space Technology Development Agency (GISTDA) THEOS / Land Surface.
1 JAXA Agency Report May 25, 2007 Satoko Horiyama MIURA JAXA/EORC May 25, 2007 Satoko Horiyama MIURA JAXA/EORC.
1 CEOS/WGISS-21 JAXA Status Report May 17, 2006 Budapest, Hungary Satoko Horiyama MIURA Japan Aerospace Exploration Agency (JAXA)
U.S. Department of the Interior U.S. Geological Survey Agency Report, WGISS #22 September 15, 2006 Lyndon R. Oleson U.S. Geological Survey Center for Earth.
Environmental Remote Sensing GEOG 2021 Lecture 8 Orbits, scale and trade-offs, revision.
Israeli Universal Spacecraft Bus Characteristics and Design Trade-Offs
Remote Sensing & Mineral Exploration
SDMI Imagery Workshop GeoEye High Resolution Imagery Solutions for Alaska SDMI Tara Byrnes GeoEye Statewide Digital.
Resurs-P. Capabilities. Standard products. A. Peshkun The 14 th International Scientific and Technical Conference “From imagery to map: digital photogrammetric.
WorldView-1 By Michael Jones. Abstract The WorldView-1 satellite is one part of what is to be a three satellite constellation. The group includes QuickBird,
Feature Analysis of Groundwater Discharge Points in Coastal Regions around Mt. Chokaisan, Japan by Using ALOS PALSAR DATA FR1.T GIS and Agro-Geoinformatics.
Spencer Anderson Brent Fogleman Daryl Vonhagel. Objectives: C-band (w = 3.8 – 7.5 cm) & X-band (w = 2.4 – 3.8 cm) IFSAR to acquire topographic data.
Remote Sensing Media Aircraft BasedAircraft Based –photography (BW, Color), infrared (BW, Color) –RADAR (SLAR, SAR) –LIDAR (light detection and ranging)
Orbits and Sensors Multispectral Sensors
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