Satellite Formation Flying - NPOESS - Remote Sensing Application - Completely Remote Sensing, GPS, and GPS Tutorial
Satellite Formation Flying - NPOESS

During the preceding Sections we talked about individual satellites, each in its own orbit and making measurements usually independent of other co-operational satellites. But the notion of multi-sensor and multi-platform satellites has already been introduced. Thus, when more than one Landsat or SPOT or IRS, etc., satellite is in orbit and functioning at any given time, the possibility of multitemporal data gathering is activated. Weather satellites are a prime example of having different satellites all looking at the Earth during a given period of time. Data from them can be correlated and integrated to provide information on weather during any specified day. Another variation of such integration occurs when data from simultaneous observations or successive observations or from different platforms are combined by some mode of registration, usually done through computer processing.

In the past 10 years or so, and especially in recent years, the concept of satellite formation flying has crept into the thinking of those seeking different approaches to new programs. Some have described their awareness of birds, such as geese, flying in structured flocks (or bombers in the Second World War) as the inspiration for this concept. Formation flying can be defined as "groupings of duplicate or similar satellites, having sensors in common or are complementary (related), that talk to each other and share data processing (onboard and/or by means of utilizing comparable ground stations and facilities), payloads, and mission functions." The multiple satellites are, in one or more ways, said to be synchronized. Two sites that briefly overview satellite formation flying are found at these SpaceFlight Now and EO-1 web pages.

The Terra/Aqua pair and other EOS satellites are part of an integrated series of satellites that are, in effect, prime examples of formation flying or synchronization of satellites dedicated to gathering data/information on climate topics. Terra is in formation with Landsat-7, EO-1, and SAC-C. Aqua, which follows Terra orbital pathways about 3 hours later, has now been joined by CALIPSO, CloudSat, and Aura, and later by PARASOL. This chart summarizes the formation scheme for these satellites:

EOS-related diagram showing formation array of participating satellites.

This next image shows the value of flying the Terra-Aqua pair in close formation in which each satellite covers the same area on the same day but separated by several hours when passing over a scene. At 9:55 AM Terra imaged the Central Africa coastal part of western Nigeria. At that time, a large number of small fires deliberately set by local farmers (the "slash and burn" custom) to clear the land for a new crop planting are clearly evident. When Aqua passed this scene 3 hours later, the number of fires had increased significantly.

Terra and Aqua images of western Nigeria showing an increase in set fires from approximately 10 AM to 1 PM.

Another EOS satellite pair - CloudSat and Calipso - were launched together on April 28, 2006. Their orbital positions are adjusted so that they are close-spaced in formation. Here are the two:

The S and Calipso satellites; artist's rendition of the pair.

Both examine cloud structure and properties in 3-D. CloudSat uses radar to determine layer stratification; Calipso uses lidar to sense particulate distribution.

The first vertical CloudSat radar images were released in June, 2006. Here are two examples:

Three-dimensional image of cloud particles in a cloud bank off the Alaskan coast.
Cloud profile off the coast of Norway.

One of the early payoffs from CloudSat's capability was to obtain a vertical cloud pattern slice through the first Tropical Storm, Alberto, as it approached the west coast of Florida on June 12, 2006:

Cross-section through Tropial Storm Alberto.

A classic example of formation flying is given by the Global Positioning System (GPS), which we considered earlier on Page 11-6. There we learned that the U.S. is operating a program called NAVSTAR which facilitates location of any point on Earth to a high degree of accuracy (read that page for principles; you are probably familiar with some of its many applications, such as getting directions while driving your expensive car, locating yourself while hunting, or sending your position when shipwrecked at sea). A NAVSTAR satellite looks like this:

A NAVSTAR GPS satellite.

At present there are 27 operational NAVSTAR satellites (24 in the basic array; three others as "spares" or "reserves" to be emplaced as individuals fail). They all support the same sensor system, essentially a radio transponder which communicates with receivers distributed worldwide and linked to parent ground stations. Their orbits are carefully specified and maintained to have mutual regularity in spacing. Thus:

Orbital Configuration of the NAVSTAR fleet.

When plotted on a flattened global projection, the regularity of the orbital paths becomes apparent:

NAVSTAR configurations projected on a Global Map.

This type of formation flying is known as the "Constellation" configuration. The satellites are spaced at considerable distance from one another but maintain communication with one another as well as with ground stations, through relays. Another configuration of similar satellites is called "Cluster", in which a small group of satellites are located relatively close to each other as they follow orbits that permit them to remain the same distances apart. Here is a suggested arrangement of a group that would comprise the TechMap 21 system:

TechMap21 satellite group.

Still another formational configuration can be termed the "Trailing" mode. It is illustrated by the present pairing of Landsat 5 and EO-1 which follows the first satellite in the same orbit, so that EO-1 crosses the same "real estate" at a slightly later time (about 1 minute). This diagram illustrates the two satellites in their common orbit and includes some of the operational parameters.:

Operational configuration of the Landsat 7/EO-1 pairing..

An obvious advantage to this is that the trailing satellite not only sees slightly different temporal conditions, but can be equipped with one or more different sensors that provided additional sensing capabilities. In other words, if new sensors with improvements or operating in different parts of the spectrum are developed after the earlier satellite is placed in orbit, it would be next to impossible to add these to that satellite but the second satellite would be so close to the first in time and space, so that the effect is almost as if the sensor(s) has been emplaced on the first one.

One added benefit in grouping satellites in a co-ordinated program is that, under appropriate circumstances, each can be built and launched at lower costs. And, if one of a group fails after orbiting, the cost of replacing it would normally be less that replacing or Shuttle-servicing a large satellite operating as a stand-alone.

Among candidates for formation flying are very small and lightweight satellites called nanosatellites (under 10 kilograms [22 pounds]), or larger cousins called microsatellites (under 100 kilograms). An example of the first is the experimental communications satellite called SNAP-1 (shades of the first Sputnik!) developed by the University of Surrey, and shown here:

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Another example of formation flying of small objects will be the Magnetospheric Constellation, consisting of 100 microsatellites whose orbits are set to provide simultaneous coverage on a global scale.

Application categories especially suited to formation flying include astronomy, communications, meteorological, and environmental. In astronomy, multiple satellites at specific spacings open up the opportunity to use them as components in an array that permits the principles of interferometry to increase effective resolution. JPL is planning an astronomical project called SIM-Lite that will use multiple spacecraft to study stars by interferometry. A launch date has not yet been set

A major effort is underway to combine and coordinate programs to gather environmental and meteorological data now acquired independently by several agencies. Thus, NASA, NOAA, and the Dept. of Defense are joining forces to set up NPOESS (National Polar Orbiting Environmental Satellite System), scheduled to be fully operational around 2008. Three satellites, each with up to 10 sensors (most but not all duplicated on each satellite), will be placed in orbits that cross the Equator at times four hours apart. This is the current planned configuration:

NPOESS Orbital Configuration

The new spacecraft will be modeled after the present day POES program run by NOAA. More about this ambitious scheme can be learned by visiting these online sites: Air Force participation and NOAA, which describes some of the candidate sensors. Tasks considered for this grouping include improved 3 to 5 day forecasts, storm tracking, and crop management. Prior to launch, the proof of concept will be tested by the OSSE (Observing System Simulation Experiment).

To close, this last page highlights a trend illustrated by the EOS series of using pairs to multiples of satellites that fly in regular patterns, spacings, or time separtions, such that, coordinated together, the result is a symbiotic increase in information.

Source: http://rst.gsfc.nasa.gov/