Sabtu, 11 Desember 2010

AKURASI CITRA QUICKBIRD UNTUK KEPERLUAN PETA DASAR PENDAFTARAN TANAH

Metode terrestris dan fotogrametris yang digunakan untuk pengadaan peta dasar pendaftaran tanah tidak mampu memenuhi dan mencakup seluruh wilayah Indonesia. Tersedianya peta dasar pendaftaran tanah yang lengkap akan membantu proses pendaftaran tanah oleh Badan Pertanahan Nasional. Dengan kemajuan teknologi di bidang pemetaan dan satelit, dapat dibuat peta skala besar dari citra satelit sepanjang memenuhi ketelitian yang ditetapkan.
Koreksi geometrik citra dilakukan dengan metode transformasi koordinat menggunakan dua variasi titik sekutu yang berasal dari GCPs lapangan dan GCPs citra mentah. Hasil transformasi koordinat berupa parameter transformasi dan koordinat hasil transformasi yang terdiri dari koordinat GCPs citra dan koordinat detail citra. Disamping itu dilakukan pengukuran terrestris sebagai data acuan untuk memperoleh koordinat detail lapangan. Analisis ketelitian menggunakan Root Mean Square Error (RMSe) dan standar deviasi untuk mengetahui ketelitian titik dan jarak dari citra. Sedangkan analisis perbandingan digunakan untuk mengkaji toleransi luas. Ketelitian yang diperoleh dari citra kemudian diperbandingkan dengan standar ketelitian dari Badan Pertanahan Nasional.
Ketelitian posisi titik (RMSe) yang diperoleh dari penelitian ini antara 0,44 m sampai 0,48 m, RMSe jarak antara 0,53 m sampai 0,62 m dan persentase perbedaan luas yang dihasilkan antara metode terrestris dan citra adalah 0,08 % sampai 5,03%. Ketelitian titik sekutu 0,1 mm pada peta hanya dapat digunakan untuk peta dasar pendaftaran tanah skala 1:10000. Sedangkan ketelitian planimetrik 0,3 mm pada peta dan ketelitian kartometri 0,5 pada peta dapat dipenuhi ketelitiannya untuk peta dasar pendaftaran tanah skala 1:2500 dan 1:10000. Citra Quickbird dapat digunakan secara visual dengan baik pada skala 1:3000.

Selasa, 16 November 2010

Mengenal Satelit WorldView-2

WorldView-2 Satellite Sensor

DigitalGlobe's WorldView-2 Satellite, launched October 8, 2009, provides 0.5m Panchromatic (B&W) mono and stereo satellite image data. Click here to watch the WorldView-2 launch (courtesy Boeing).


With its improved agility, WorldView-2 is able to act like a paintbrush, sweeping back and forth to collect very large areas of multispectral imagery in a single pass. WorldView-2 alone is able to collect nearly 1 million km2 every day, doubling the collection capacity of our constellation to nearly 2 million km2 per day. And the combination of WorldView-2’s increased agility and high altitude enables it to typically revisit any place on earth in 1.1 days. When added to the satellite constellation, revisit time drops below one day and never exceeds two days, providing the most same-day passes of any commercial high resolution constellation.
The WorldView-2 sensor provides a high resolution Panchromatic band and eight (8) Multispectral bands; four (4) standard colors (red, green, blue, and near-infrared 1) and four (4) new bands (coastal, yellow, red edge, and near-infrared 2), full-color images for enhanced spectral analysis, mapping and monitoring applications, land-use planning, disaster relief, exploration, defense and intelligence, and visualization and simulation environments.
Coastal Band (400 - 450 nm): This band supports
vegetation identification and analysis, and supports bathymetric studies based upon its chlorophyll and water penetration characteristics. Also, this band is subject to atmospheric scattering and will be used to investigate atmospheric correction techniques.
Yellow Band (585 - 625 nm): Used to identify "yellow-ness" characteristics of targets, important for vegetation applications. Also, this band assists in the development of "true-color" hue correction for human vision representation.
Red Edge Band (705 - 745 nm): Aids in the analysis of vegetative condition. Directly related to plant health revealed through chlorophyll production.
Near Infrared 2 Band (860 - 1040 nm): This band overlaps the NIR 1 band but is less affected by atmospheric influence. It supports vegetation analysis and biomass studies.
The WorldView-2 imaging payload is the second such system engineered and manufactured by ITT Space Systems Division for DigitalGlobe. Once deployed, it will operate at an altitude of 770 kilometers, and the advanced on-board imaging system will capture pan-sharpened, multispectral images (with better than 0.5-meter resolution) from almost 500 miles above the Earth. These images supply unprecedented detail and geospatial accuracy, further expanding the applications for satellite imagery in both commercial and government markets. Added spectral diversity provides the ability to perform precise change detection and mapping.
In addition to numerous other technical improvements, WorldView-2 also has the ability to accommodate direct tasking, which will allow select customers around the world to load imaging profiles directly up to the spacecraft and execute delivery of the data directly down to their own ground stations.

WorldView-2 Satellite Sensor Characteristics

Launch Date
October 8, 2009
Launch Vehicle
Delta 7920 (9 strap-ons)
Launch Site
Vandenberg Air Force Base
Orbit Altitude
770 kilometers
Orbit Type
Sun synchronous, 10:30 am (LT) descending Node
Orbit Period
100 minutes; 7.25 year mission life, including all consumables and degradables (e.g., propellant)
Spacecraft Size, Mass, & Power
4.3 meters (14 feet) tall x 2.5 meters (8 feet) across, 7.1 meters (23 feet) across the deployed solar arrays; 2800 kilograms (6200 pounds); 3.2 kW solar array, 100 Ahr battery
Sensor Bands
Panchromatic
8 Multispectral (4 standard colors: red, blue, green, near-IR), 4 new colors: red edge, coastal, yellow, near-IR2
Sensor Resolution GSD
Ground Sample Distance Panchromatic: 0.46 meters GSD at Nadir, 0.52 meters GSD at 20° Off-Nadir

Multispectral: 1.8 meters GSD at Nadir, 2.4 meters GSD at 20° Off-Nadir
(note that imagery must be resampled to 0.5 meters for non-US Government customers)
Dynamic Range
11-bits per pixel
Time Delay Integration (TDI)
Panchromatic - 6 selectable levels from 8 to 64
Multispectral - 7 selectable levels from 3 to 24
Swath Width
16.4 kilometers at nadir
Attitude Determination and Control
3-axis stabilized
Actuators
Control Moment Gyros (CMGs)
Sensors
Star trackers, solid state IRU
GPS Position Accuracy & Knowledge
< 500 meters at image start and stop
Knowledge: Supports geolocation accuracy below Retargeting
Agility Acceleration
1.5 deg/s/s
Rate: 3.5 deg/s
Time to slew 300 kilometers: 9 seconds
Onboard Storage
2199 gigabits solid state with EDAC Communications
Image and Ancillary Data: 800 Mbps X-band
Housekeeping
4, 16 or 32 kbps real-time, 524 kbps stored, X-band
Command
2 or 64 kbps S-band
Max Viewing Angle
Accessible Ground Swath Nominally +/-40° off-nadir = 1355 km wide swath
Higher angles selectively available
Per Orbit Collection: 524 gigabits
Max Contiguous Area Collected in a Single Pass: 96 x 110 km mono, 48 x 110 km stereo
Revisit Frequency
1.1 days at 1 meter GSD or less 3.7 days at 20° off-nadir or less (0.52 meter GSD)
Geolocation Accuracy
(CE 90) Specification of 12.2m CE90, with predicted performance in the range of 4.6 to 10.7 meters (15 to 35 feet) CE90, excluding terrain and off-nadir effects

With registration to GCP's in image: <2.0 meters (6.6 ft)

For more information on Characterization of Satellite Remote Sensing Systems, please click on the hyperlink.
DigitalGlobe currently operates the QuickBird satellite, which can collect black-and-white, or panchromatic, images with 0.61-meter resolution at Nadir. The satellite, launched in October 2001, also collects multispectral images with 2.5 meter resolution. WorldView-1 high-capacity, panchromatic imaging system features half-meter resolution imagery. Operating at an altitude of 496 kilometers, WorldView-1 has an average revisit time of 1.7 days and is capable of collecting up to 750,000 square kilometers (290,000 square miles) per day of half-meter imagery. The satellite also is equipped with state-of-the-art geo-location accuracy of <2m without GCP's while with one (1) or two (2) GCP's the geospatial accuracy is <1m and further exhibits stunning agility with rapid targeting and efficient in-track stereo collection.
Please check back for image data for the WorldView-2 satellite.

Mengenal Satelit WorldView-1

WorldView-1 Satellite Sensor

WorldView-1, DigitalGlobe's earth imaging satellite, completed a successful launch from Vandenberg Air Force Base, California, U.S.A., at 11:35 Hrs Pacific Daylight Time (PDT) on September 18th, 2007. The Delta II rocket lifted off in good weather and the WorldView-1 satellite is "currently undergoing a calibration and check-out period," according to DigitalGlobe. The first panchromatic image data should become available before October 18th, 2007.
To view a video of the WorldView-1 satellite launch, click here.
The high-capacity, panchromatic imaging system features half-meter resolution imagery. Operating at an altitude of 496 kilometers, WorldView-1 has an average revisit time of 1.7 days and is capable of collecting up to 750,000 square kilometers (290,000 square miles) per day of half-meter imagery. The satellite is also equipped with state-of-the-art geo-location capabilities and exhibits stunning agility with rapid targeting and efficient in-track stereo collection.

WorldView-1 Satellite Sensor Characteristics

Scheduled Launch Date
September 18, 2007
Launch Vehicle
Boeing Delta 7920 (9-strap-ons)
Launch Location
Vandenberg Air Force Base, California, USA
Orbit Altitude
496 Km
Orbit Inclination
sun-synchronous
Spacecraft Size, Mass & Power
3.6 meters (12 feet) tall x 2.5 meters (8 feet) across,
7.1 meters (23 feet) across the deployed solar arrays
2500 kilograms (5500 pounds)
3.2 kW solar array, 100 Ahr battery
Equator Crossing Time
10:30 AM (descending node)
Revisit Time
1.7 days at 1 meter GSD or less
5.9 days at 20° off-nadir or less (0.51 meter GSD)
Swath Width
17.6 Km at nadir
Full Scene
17.6 Km x 14 Km or 246.4 Km 2 at nadir
Orbit Time
94.6 minutes
Dynamic Range
11 bits per pixel
Resolution
0.50 meters GSD at nadir

0.55 meters GSD at 20° off-nadir
(note that imagery must be re-sampled to 0.5 meters for non-US Government customers)
Sensor Bands
Panchromatic
Metric Accuracy
Accuracy: <500 meters at image start and stop
Knowledge: Supports geolocation accuracy below
Geolocation Accuracy
(CE 90%)
Specification of 12.2 m CE90, with predicted performance in the range of 3.0 to 7.6 meters (10 to 25 feet) CE90, excluding terrain and off-nadir effects

With registration to GCPs in image: 2.0 meters (6.6 feet)
Retargeting Ability
Acceleration: 2.5 deg/s/s
Rate: 4.5 deg/s
Time to slew 300 kilometers: 9 seconds
Attitude Determination and Control
3-axis stabilized
Actuators: Control Moment Gyros (CMGs)
Sensors: Star trackers, solid state IRU, GPS
Onboard Storage
2199 gigabits solid state with EDAC
Communications
Image and Ancillary Data: 800 Mbps X-band
Housekeeping: 4, 16 or 32 kbps real-time, 524 kbps stored, X-band
Command: 2 or 64 kbps S-band
Max Viewing Angle /
Accessible Ground Swath
60 x 110 km mono
30 x 110 km stereo

Mengenal Satelit Quickbird

QuickBird Satellite Images and Sensor Specifications

Because of our relationship with DigitalGlobe, developer and owner of the QuickBird Sensor, Satellite Imaging Corporation (SIC) acquires QuickBird Satellite Imagery worldwide for our customers seeking high-resolution, digital aerial photographs.

About the QuickBird Satellite Sensor

QuickBird is a high resolution satellite owned and operated by DigitalGlobe. Using a state-of-the-art BGIS 2000 sensor (PDF), QuickBird collects image data to 0.61m pixel resolution degree of detail. This satellite is an excellent source of environmental data useful for analyses of changes in land usage, agricultural and forest climates. QuickBird's imaging capabilities can be applied to a host of industries, including Oil and Gas Exploration & Production (E&P), Engineering and Construction and environmental studies

QuickBird Satellite Sensor Characteristics

Launch Date
October 18, 2001
Launch Vehicle
Boeing Delta II
Launch Location
Vandenberg Air Force Base, California, USA
Orbit Altitude
450 Km
Orbit Inclination
97.2°, sun-synchronous
Speed
7.1 Km/sec (25,560 Km/hour)
Equator Crossing Time
10:30 AM (descending node)
Orbit Time
93.5 minutes
Revisit Time
1-3.5 days, depending on latitude (30° off-nadir)
Swath Width
16.5 Km x 16.5 Km at nadir
Metric Accuracy
23 meter horizontal (CE90%)
Digitization
11 bits
Resolution
Pan: 61 cm (nadir) to 72 cm (25° off-nadir)
MS: 2.44 m (nadir) to 2.88 m (25° off-nadir)
Image Bands
Pan: 450-900 nm
Blue: 450-520 nm
Green: 520-600 nm
Red: 630-690 nm
Near IR: 760-900 nm


Jumat, 03 September 2010

PETA CITRA UNTUK PERENCANAAN TATA RUANG WILAYAH


Peta Citra Juga di pakai untuk perencanaan Tata Ruang Wilayah baik perkotaan, perdesaan, ibu kota provinsi/kabupaten dan kecamatan dan bisa juga digunakan untuk pembukaan lahan baru untuk transmigrasi.

PETA CITRA UNTUK INFRASTRUKTUR


Peta Citra juga bisa di gunakan untuk keperluan infrastruktur semisal pembangunan Jalan Tol, Jalan Layang, Jalan Kereta Api, Bandara, Jembatan, DAM atau Bendungan Irigasi atau infrastruktur yang lainnya yang terkain dengan perencanaan Kota

PETA CITRA UNTUK LAHAN PERTANIAN DAN PERKEBUNAN

Peta Citra juga bisa dimanfaatkan untuk inventarisasi perkebunan, pertanian dan kehutanan sehingga pola tanaman yang serasi atau bisa juga di manfaatakan untuk menditeksi area lahan seperti terlihat dalam gambar.

Sabtu, 21 Agustus 2010

MANFAAT PETA CITRA SATELIT QUICKBIRD UNTUK TRANSPORTASI

 
Peta Citra Quickbird juga bisa dimanfaatkan untuk penataan transportasi jalan dan jembatan penyeberangan di Wilayah Perkotaan, seperti tampak terlihat dalam gambar tersebut.(lokasi Bangkok, Thailand, Sumber Citra Quickbird Worldview-2)

Kamis, 05 Agustus 2010

MANFAAT PETA CITRA QUICKBIRD UNTUK PERTAMBANGAN

Citra Quickbird untuk menditeksi Pertambangan atau Sumber Daya Mineral yang ada, seperti terlihat pada gambar tersebut (lokasi Tambang Batu Bara Bukit Asam, Tanjung Enim, Sumber Citra Quickbird)