AstroVision
Australia Ltd
Suite 9
2 Short
Street
Double Bay
NSW 2028
Australia
url:
http://www.astrovisionaustralia.com
Shubber Ali:
Managing Director
Frank Williams: Chief Engineer
David Wright: Government
Relations
Mitchell Burnside Clapp: Chief Technologist
Jim Styles:
Sales/Marketing Consultant, WeatherMaxx
Incorporated in 2003,
AstroVision Australia is a public unlisted company based in Sydney. Over the
last year it has been familiarising Federal and State Government departments
and research organisations on the potential uses of high speed imaging from
cameras, infrared sensors, multispectral instruments and lightning detectors in
Geostationary orbit.
Australia and other countries in this region are
currently critically dependent for weather observations on one 11-years-old,
partially disabled US geostationary imaging satellite with obsolete
instrumentation, operated on lease from the American National Oceanic and
Atmospheric Administration (NOAA). Called GOES-9 (GOES stands for Geostationary
Operational Environmental Satellite), it has only a limited remaining life.
Sudden failure of GOES-9 would place our region in a precarious position,
affecting a wide range of industries and economies.
A Geostationary
satellite, which orbits at the same speed as the Earth's rotation, would
provide continuous coverage 24 hours a day, seven days a week from a fixed
location high above the Earth, allowing cloud weather patterns and cyclones to
be monitored continuously. Movements of ships, ocean temperatures, emissions of
volcanic ash, growth of pastures and locations of lightning strikes causing
bushfires are among many terrestrial and oceanographic observations that would
be greatly enhanced through the satellite.
Advanced instrumentation,
derived from equipment developed primarily for NASA interplanetary missions,
will provide much more frequent observations than is possible with present day
equipment. Australia has been chosen as the headquarters for AstroVision
because of an obvious gap in modern geostationary satellite coverage for the
Asia-Pacific.
The AstroVision 24 hour satellite coverage will be
distinct from, and complementary to, that offered by rapidly-orbiting Low Earth
Orbit (LEO) imaging satellites. LEOs give coverage for, at best, 15 minutes at
a time once a day before disappearing over the horizon. The business model
allows the total annual cost to be shared between a number of different
government departments, research bodies, private clients and users across the
Asia-Pacific region.
Technology
AstroVision's system
architecture consists of:
The AstroVision system is based on mature
space heritage hardware and technology, one of the keys to the low cost, high
reliability of the system. The sensors are derivatives of those developed and
flown initially for interplanetary missions and planetary observation by NASA,
which place a high premium on sensors being lightweight, with high reliability
and low power requirements. This makes for smaller payloads, with smaller
satellites to carry them, and results in significantly lower costs than
traditional satellite projects.
The AstroVision satellites are less
than half the size and mass of typical geostationary satellites. The satellites
are 3-axis stabilized, using star trackers, similar to those in deep space and
planetary missions, to meet the stringent pointing requirements of the
satellite's sensors. This is necessary to avoid smearing of the images being
sent back to earth.
The positioning of the satellite in geostationary
orbit will be at or near 130° East Longitude and will provide 24 hour
continuous coverage of the region from India to mid Pacific (west of Hawaii).
The planned launch date for the satellite is in 2007 and the nominal life of
the satellite is at least 9 years. The contract for the satellite bus has
already been put to tender, and Ball Aerospace (Colorado, USA) was selected by
AVII as the favoured entity for satellite construction and sensor integration.
Ball has an established history in satellite construction with particular
experience with imagery systems.
Three US patents (with numerous others
in process) have been granted and issued to protect the system designed by
AstroVision.
Cameras and Sensors
There will be seven
separate sensors on board the first satellite: one wide field, two narrow
field, one low light, one multi-spectral, one lightning mapper, and one thermal
infrared. This combination of sensors will enable the provision of real-time
imagery of not only the full Earth disk, but also higher resolution imagery of
any significant events happening across the Asia-Pacific region, and a range of
secondary applications created by the fusion of these data streams in different
combinations.
The Wide Field Camera (WFC), capable of showing the
Earth's full disk at 2.75 kilometre resolution, is actually composed of three
cameras, each one providing one of the three standard red, green and blue
colours that make up the typical true-colour digital image. The WFC is aligned
with the spacecraft's nadir-pointing axis, directed toward the Earth's centre.
The WFC will be fixed to the satellite body and will be pointed by pointing the
satellite itself. The field of view of the WFC is sufficiently large to view
the entire Earth disk including most of the Earth's atmosphere, while
accommodating motions of the satellite bus. The WFC provides context for the
Narrow Field Cameras for significant events.
There are two separate and
independent Narrow Field Cameras (NFCs) capable of providing 250 metre
resolution over a field of view of approximately 1,000 x 1,000 km for an
instantaneous image of one million square kilometres every second. As with the
WFC, each of these is made up of the three individual red, green and blue
cameras. The two NFC sensors/camera sets are independently mounted on steerable
platforms on the satellite bus, allowing use of the two cameras to provide
high-resolution imagery of two independent significant events on the Earth's
surface or atmosphere at the same time. These will provide local weather in all
metropolitan markets in the region updated at least every minute.
The
Low Light Camera (LLC) will also have the same field of view as the NFCs, is
independently pointable, and take up to 1 frame a second. Used to observe light
sources and events on the night side, the low light capabilities of this sensor
will provide pictures of bright night-side events and under the right
conditions and pictures of cloud cover at night using only moonlight for
illumination.
The Multi-Spectral Camera (MSC) is made up of a Low Light
Camera giving enough light-gathering capability to observe 10 separate
frequencies of light at up to one frame a second and with the same field of
view and resolution as the NFC. The MSC is independently steerable and allows
observation in near-infrared and near-ultraviolet frequencies as well as the
more common visually observable red, green and blue. Chlorophyll and volcanic
ash are examples of ongoing processes that the MSC will be able to
sense.
The Lightning Mapper Sensor (LMS) will be able to measure total
lightning over much of the footprint of the satellite with a spatial resolution
of 8 km per pixel and a temporal resolution (refresh) of two milliseconds. This
will observe total lightning as well as turbulence within clouds and storms
that will initially be used for severe storm tracking, fire prediction, and
airline safety.
The Thermal Infrared (TIR) sensor will be able to
measure temperatures to within one degree celsius with a spatial resolution as
good as 4.5 km using half-stepping techniques and temporal resolution of
approximately 2 seconds. The TIR observes the vertical evolution of clouds and
storms, a means to monitor clouds at night, and surface temperatures of land
and water where there are few or no clouds. The TIR can supply live temperature
mapping relevant to energy demand and energy forecasting.
The
combination of these seven sensors gives real time imagery of not only the full
Earth disk but also high-resolution imagery of any significant events happening
on the Earth within the footprint of the satellite. It also provides a range of
secondary applications created by the fusion of the data streams in different
combinations.
The differences between the technologies available today
versus the AstroVision technology can be summarized as follows:
| Current Technology | AstroVision Technology |
| Hour(s) delay in delivery | Live, < 10 second delay |
| Red & infrared with false colour | True colour |
| 1-8 km resolution | 250 metre resolution |
| Averaging one image every hour | 1 image per second |
| Sporadic special event coverage | All special events covered live |
| Severely limited volcanic ash & aerosol tracking | Live volcanic ash & aerosol tracking |
| Poor rapid convective event coverage | Ideal rapid convective event coverage |
| Temperature, pressure, wind data reported hourly at best | Temperature every minute from 700,000 readings, pressure every second, wind speeds every minute |
Operations
When an event
occurs on or near the surface of the Earth, the event effects will arrive at
the suite of sensors one-eighth of a second later - at the speed of light. The
event will be recorded by the relevant sensor and transmitted from the
satellite to an Earth station located in Australia, either one owned and
operated by AstroVision, through one of AstroVision's partners/subcontractors
or a customer's site licensed to receive the encrypted AstroVision data stream.
On average, the entire process will take less than one second.
AstroVision's ground station will monitor the satellite in orbit and command
the satellite to ensure proper orbit maintenance and the appropriate
communications links are maintained. AstroVision plans to also transmit
commands to the sensor on board the satellite providing the longitude and
latitude of areas to be imaged in sequence. This latter function involves
receiving, prioritising and uplinking the image requests received from
AstroVision's direct customers and regional distributors.
Data
Handling
Upon arrival at the Earth station, the data will be
processed in real-time through our planned supercomputing facility. This
Australia-based facility is anticipated to be one of the fastest supercomputers
on the planet. Simultaneously passed to our storage network and downstream to
our customers for distribution to fixed and mobile subscribers or direct to a
remote client location. In addition, value-added services will be provided to
specific customer data sets per contract, and the resulting products will be
distributed in the most efficient method for use of the data (e.g. an alert
service for bush fire detection providing exact GPS coordinates of a new fire
event).
The technology developed by Horizon known as "Horizon TV" may
also have the potential to provide an important delivery platform for some data
and applications.
Data Storage
AstroVision intends to
select and partner with an Australian university in a mutually beneficial
arrangement. Data will be transferred to the university, which will maintain
the permanent archive. The university will become a global centre of excellence
for advanced meteorological and imagery processing and research, generate
entirely new fields of research and grants for that research, and will draw the
best and brightest information technology and space science students worldwide
to its programs.
In addition to reducing/eliminating storage costs
associated with the archive, AstroVision will benefit in two primary ways.
Firstly, by agreement with the university, any new algorithms developed that
have commercial potential will inure to the commercial benefit of AstroVision,
with shared royalties paid back to the university. Secondly AstroVision expects
a constant source of future engineering talent to draw upon from the graduates
of the university's programmes driven by our data, algorithm development and
research. AstroVision has initiated discussions with leading Australian
universities to develop the selection criteria we will use for locating the
archive.