ROSÆ, Inc.

7901 52nd Ave. W., #205

Arvada, CO  80002

January 1, 2007

 

 

 

 

 

 

 

 

 


MIRIAH: An idea whose time has come (Grisham, U.S. Patent No. 6,452,532)

 

The Challenge.

 

There is the common belief that since conventional EEE systems for imaging (SAR, ISAR, etc.), communications, navigation, etc., can be redesigned in hundreds (if not thousands) of different ways to accomplish the same functional purpose, then this will also apply to MIRIAH (a new Satellite Imaging invention). But MIRIAH is not a typical EEE system. Rather, it is a uniquely arranged set of Interferometers - a much different technology from the conventional EEE technology (SAR is far more sensitive to timing errors than are Interferometers). Moreover, Interferometers have such stringent requirements for their successful implementation, that these constraints demand great care in the choice of the architecture. In my opinion, this demands a "marriage" of the uniquely innovative Interferometric methods used by MIRIAH to the ROSÆ Satellite architecture - which is also uniquely innovative. This solution, to this most critical Mission Requirement (see *Note), is so unique, that the following brief technical review has become necessary. For otherwise the government – industrial community may continue their fruitless search for an "equivalent" to MIRIAH (to bypass the Patent), while none will ever be found.

*Note: Link here to the "Mission Requirement" - choose either the (1) short version or the more comprehensive (2) long version .

 

The Answer to the Challenge

 

Einstein proved light has a particle nature, comprised of distinct individual points or packets of substance possessing energy. Whereas, Huygens proved light has a wave form nature. Yet, while these two concepts of light appear to contradict one another, they do not according to Fourier. Fourier, a French mathematician, related these two forms of light into a unifying concept known as the "Fourier Pair", in which both forms exist, but are focused at two different planes. The first of these is known as the Fourier Plane (the wave nature plane, which has phase diversity), and the second is known as the imaging plane (the particle nature plane, which has spatial diversity). In nature, man has cognition in the Imaging Plane, while whales and porpoises have cognition in the Fourier Plane (as do submarine SONAR). Furthermore, since the electromagnetic spectrum is a continuum, which occurs at all frequencies, then these laws of Physics are true starting at the very lowest frequency (audio) - to Radio Frequency (RF) - to HF – to VHF – to UHF - to microwave - to light, etc.

 

The illumination coming to MIRIAH´s receiving apertures (or antennae), reflected to them from the Field of View (FOV), and subsequently deposited on a disc(s) or other random access high density medium, requires a plane (or area) in order to pass energy, which this illumination contains. Yet, it is clear that only the Fourier Plane is capable of accumulating all of the information for every imaged object in the FOV - not the Imaging Plane. For it is only the Fourier plane, which spreads the imagery data throughout its focused plane. This illumination energy comes to the receiving aperture in the form of an energy distribution, which aggregates throughout the plane during the time it takes to "fully fill" the aperture of the recording medium. Then, in considering these two planes, it is the Fourier Plane which has all of the information contained in the object. This is why I prefer to call it the Holographic Plane, rather than the Fourier Plane. Since the distribution of the total energy in the image is present throughout a very large solid angle, then the object (and so the FOV) must rotate and translate, in order to sample all of the illumination energy, which each resolved object within the FOV contains (or rotate in azimuth and elevation for complete solid angle sampling). Clearly, this will take considerable time, which is why this is not a real aperture (until it is later illuminated), but rather it is a 2-D matched filter at this point in time (a kind of “delayed” synthetic aperture). Later, when illuminated by a collimated laser, it is a real aperture, focusing a real image (as opposed to the SAR virtual image requiring complex and time consuming reconstruction).

 

However, for maximum efficiency, the "fill time" of this Matched Filter should be just enough to sample all of the information in the FOV onto the Holographic Plane, coherently (i.e., phase synched). Once completely "filled", it becomes a source, which replicates every object in the FOV (reproduced at some later time in all of its detail, at every angle). That is, this imaging format becomes a 2-D hologram – after the Holographic Plane is "fully filled". And, it is efficiently "filled" (and so not inefficiently "over filled" - thereby wasting energy), if the next cycle of "filling" is reached just as the previous cycle completes the "filling" process. (And besides, to provide time-sequenced imaging, successive discs should be registered to the same phase grid).

 

Then it follows that for efficiency, the satellite orbits must repeat, and they must be symmetric, which is why we use ROSÆ in a 5:1 resonant case as our preferred architecture and preferred orbit. And, as has been proven in other presentations, ROSÆ is the only possible distribution of satellites, which is symmetric, stable, orthogonal, and possesses the attributes of a "perfect" machine. These "perfect" attributes, require the 1st and 2nd Moments of this space "machine" to be collinear, constant, orthogonal, and balanced in all three dimensions about the "machine's" mass center (in this case earth’s gravity center). ROSÆ is the only such architecture possible for earth or for any other planet (since all planets have spherically concentric gravity fields). Hence, MIRIAH – ROSÆ has no peer concept capable of providing these three services of Imaging, Communications, and Navigation with anywhere close to its efficiency. This efficiency improvement is several orders of magnitude - about a billion to one (in theory) for the case of its improvement over SAR, which is today’s most efficient microwave imaging concept.

 

Some Scientists are of the mistaken opinion that many EEE system designs can be found to compete with MIRIAH – ROSÆ. But all of these EEE designs are correlated and registered to the recording medium as a function of time. For example, the range dimension requires an extremely fine determination of time since the range gate is moving across the FOV at the speed of light, whereas, an Interferometer is self-registering. And, an Interferometer’s grid (interference pattern) moves across the face of the FOV at the much slower speed of satellites. This is why, per Heizenberg´s Uncertainty Principle of Physics, that the Interferometer has a theoretical advantage in coherence time, resolution (both spatial and spectral), and in energy density Gain. This advantage will be a function of the speed ratio of (1) light to (2) the speed at which the Interferometer´s interference pattern sweeps across the FOV. In theory, this Gain advantage is about a billion to one. For with Interferometry, image registration is sensitive to geometry, rather than time correlation (as needed for the image reconstruction of all of a SAR’s EEE systems). In fact, MIRIAH's image is a real image vs.SAR’s virtual images. Hence, SAR needs lengthy non real-time "image reconstruction", while MIRIAH can more quickly illuminate its hologram (coherently) and focus with conventional optics in real time.

 

Therefore, MIRIAH – ROSÆ uses triads of Interferometers, which correlate and maintain phase coherence primarily as a function of geometry rather than time. Furthermore, MIRIAH's images are in both 2-D and 3-D. This is practical with architectures which use Interferometers distributed in a 3-D symmetric geodesic set of equilateral triads about the earth. This is needed to set all phase zero lines through a satellite, to enable phase offset "unwrapping" to the phase origin faster and more efficiently. Once again, this defines MIRIAH – ROSÆ, since it has eight equilateral faces or planes - the minimum number of conformal planes for data continuity throughout each imaged surface. Plus, it has the other necessary attributes needed (orthogonal, linear, stable, radially symmetric, focuses a large depth of field linearly to a disc, etc.). Hence, any further exploration by Scientists to find an alternative to MIRIAH – ROSÆ is doomed to failure.

 

Another way in which government and industry microwave imaging Scientists have been misled, is in the belief that wide bandwidth SAR will deliver more imaging information, more efficiently, than can narrow bandwidth MIRIAH. (For this is the case in the communications discipline – and so they reason it should also be true in imaging). Although this assumption at first seems reasonable, this mistake defeated the LightSAR project a few years ago. The problem stems from the way a wide bandwidth SAR´s beam width shrinks as its bandwidth increases. This drastically shrinks its FOV to where so many users are left "out in the cold" (out of the supplied service area), that the resulting extremely high unit cost creates a huge economic deficit for the operational service. And, the signal propagation losses are so huge, its satellites must use very low altitude orbits, which require "store and forward" data methods, which completely cancels out the fast response time advantage of wide bandwidth. This is so severe, that the MIRIAH imaging system throughput time will deliver imagery much faster - even though its response time is much slower than for a SAR.

MIRIAH generates a 2-D Matched Filter with a positive Gain, which is impossible for an EEE system for  a SAR. Likewise, it would be impossible for an EEE system on a SAR to generate a 2nd Power – Aperture (2nd PA) in tandem with the 1st PA. Therefore, the tremendous boost this gives to MIRIAH´s performance (160 dB Gain - in theory) will never be possible for a SAR. This kind of performance is possible only for 2-D Interferometric architectures, known also as a "sparse phased arrays", but only if the array is much larger than the FOV. For uninterrupted coverage of the earth, this creates the requirement for a satellite architecture, which has about two to three times the diameter of the earth (as in ROSÆ). Such an altitude would be totally impractical for SAR’s EEE system. In summary, no EEE system for SAR or any other form of EE design can ever be designed to compete with MIRIAH’s efficiency (as an architecture – which will in time have many system designs)..

 

All of the above reasons are why there is no real competition for MIRIAH. Nor is there any competition for MIRIAH – ROSÆ when it comes to global imaging, navigation, communication services. The disparity is so great, that even the most "hard nosed" captain of industry will be forced to switch to this new architecture in order to survive in a competitive world marketplace.

Lest any one still doubt this disparity in efficiency, it is on the order of a trillion to one in favor of MIRIAH – ROSÆ (in theory). Even with the reality of needing to use "off the shelf" components, which will degrade this theoretical performance, we believe that the benefit/cost ratio will remain somewhere from 10,000 to 1 - to 100,000 to 1 - in favor of MIRIAH.

 

This is why we confidently "await the awakening" of the global market. For, it is not a question of " if ", rather it is only a question of " when ". And, given the nature of its critical mission requirement, then the "when" has all but arrived. (If you failed to read this Mission Requirement above, then here it is again - link here to the "Mission Requirement" - choose either the (1) short version or the more comprehensive (2) long version.).

 

 

William H. Grisham ("Bill"), Inventor, President

ROSÆ, Inc.