Progress Report (Oct 30, 1997)

5305-EX-RR-1998 Post Grant Documents

GEOPHONE COMPANY, L.L.C.

2003-10-21ELS_63483

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Geo!Phome
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GEOPHONE COMPANY, LLL.C.

180 Admiral Cochrane Dr.
Suite 310

Annapolis, MD 21401 USA
Phone: 410—571—9090
FAX: 410—571—0022

E—mail: mkig@geophone.com




               Date: October 30‘" 1997




                FCC, Experimental Licensing Branch, Suite 230, 2000 M ST., MS 1300E1,
               Washington, D.C. 20554


               Gentlemen:
                           Please find enclosed a copy of the progress report on the usage of the Experimental License
               issued to the GeoPhone Company LLC.           This report covers and summarizes the testing that was
               conducted from August 1996 through September 1997 which covers two reporting periods. A copy of
               this report is also being submitted to the FCC Satellite Engineering Branch, Room 512, 2000 M St., MS
               08000B1, Washington D.C. 20554, Attention : Mr. Karl Kensinger.
               Any questions pertaining to the following information should be directed to the undersigned.



                                                                                  Operations Manager |

                                                                                  Theodore L. Battle



                CC:   Steve Sweeney


                                 PROGRESS REPORT SATELLITE TESTING


1.0 Scope
This report contains information on the progress of satellite link testing of two GeoPhone Developmental
Earth Stations located at GeoPhone headquarters at 180 Admiral Cochrane Drive in Annapolis MD
during the period of August 1996 through April 1997. It also contains information on the testing of the
pre— production prototypes.
Since April 1997 the developmental electronic equipment has been replaced by newly developed pre—
production prototype equipment while retaining the same antenna structure and feed. Testing was done
over the SBS— 6 Satellite Business Systems Satellite located at 74 Degrees West Longitude. These
Very Small Aperture Terminals (VSATS) are capable of transmitting a frequency hopped spread
spectrum signal in the 14.0 to 14.5 GHz band and receiving in the 11.7 —12.2 GHz band . The
developmental equipment operated within a bandwidth of approximately 170 kHz and the pre— production
equipment operates within a bandwidth of 1 MHz although a complete 43 MHz transponder was leased
for the testing.


Antenna Coordinates: The VSAT antenna coordinates are 38.92 degrees North Latitude and 76.55
degrees West Longitude.


Antenna Pointing: The VSAT antenna will be pointed at an elevation of 45.22 degrees above the
horizon plane and at an azimuth angle of 175.84 degrees from the Geographic North.


Test Configuration: The test configurations will allow IF test loops and a complete RF test loop including
the satellite to be configured. The testing will be done in a sequence to maximize the use of satellite test
time to obtain data.
Maximum output power: The maximum available output power from the outdoor unit for the experimental
terminal is 5 watts and the maximum available output power from the outdoor unit for the pre production
unit is 2 watts in the 14 to 14.5 GHz band.
Approval: Approval was provided for the operation of these earth stations under a class XD MO
Experimental License issued to GeoPhone Company LLC under the call sign WAZ2XB1 under file
number 5305—EX—PL—96. A copy of the license is attached at the end of this report.


Applicable Documents:
1. Commercial documents including by not limited to commercial standards, specifications and drawing,
as well as all applicable FCC documents.
2. Industry Documents were Hughes Uplink Requirements Document.




2.0 Purpose
Tests performed on these terminals will provide the initial technology evaluation in the GeoPhone
Corporation‘s VSAT Network product development effort.


The key technologies to be evaluated during this test program will consist of low—rate vocoders, new
signal processing algorithms, a new spread spectrum modem and a unique RF hardware architecture.


The purpdse of the test series was to establish that the CAMA Waveform could be used to provide two
way duplex voice links over an operational KU band satellite and to determine how robust the connection
was both during the call establishment and the conversation phase.


The evaluation of GeoPhone‘s Proprietary Spread Spectrum Modems using the CAMA waveform and
low rate vocoder over a satellite link under varying operational conditions while measuring the subjective
quality of the voice transmissions and BER performance is one of the goals of this test series. The link
design analysis will also be validated during these tests.


3.0 Satellite Accesses
All Satellite accesses were coordinated through Hughes Communication Network Operations (HCNO)
and were completely in compliance with Hughes access procedures and requirements for the SBS—6
satellite. Several transponders were used for the testing with transmission always on the Vertical
Polarization and reception on the Horizontal Polarization.


The FCC type approved 1.2 meter Channel Master antennas were pointed and optimized to maximize
the receive and transmitted signals and to minimize cross polarization interference.


The following table indicates typical access times and the transponders used during the satellite test
program.




                                 SATELLITE ACCESS EVENTS




                DATE                     Start/End (Hrs)                  Sat Txpdr        Equip tested
                09/05/96                 13:45 — 14:00                    17               exp. terminal
                09/11/96                 11:00 — 11:15                    17               exp. terminal
                09/24/96                 16:45 — 17:00                    17               exp. terminal
                09/24/96                 17:25 — 17:40                    17               exp. terminal
                10/02/96                 18:15 — 18:45                    17               exp. terminal
                10/02/96                 18:25 — 18:55                    17               exp. terminal
                10/02/96                 09:55 — 10:10                    17               exp. terminal
                 10/03/96                11:05 — 11:35                    17               exp. terminal
                10/10/96                 09:00 — 09:15                    15               exp. terminal
                 10/10/96                17:15 — 17:45                    15               exp. terminal
                 10/18/96                16:20 — 16:35                    15               exp. terminal

                 10/21/96                08:15 — 08:30                    15               exp. terminal
                 10/28/96                18:10 — 18:25                    15               exp. terminal
                 10/29/96                08:30 — 08:45                    15               exp. terminal
                 10/29/96                09:00 — 09:15                    15               exp. terminal
                 12/09/96                10:45 — 11:15                    15               exp. terminal
                 12/10/96                09:30 — 09:45                    15               exp. terminal
                 12/11/96                16:45 — 17:00                    15               exp. terminal


12/12/97   10:05 — 10:20   15   exp. terminal
2/12/97    15:00 — 16:00   15   exp. terminal
3/08/97    11:00 — 11:15   15   exp. terminal
3/10/97    10:40 — 10:55   15   exp. terminal
3126/97    20:05 — 20:20   15   pre prod.
4/15/97    15:05 — 15:20   15   pre prod.
4/15/97    15:40 — 15:55   15   pre prod.
4/16/97    12:05 — 12:20   15   exp. /pre prod
5/01/97    09:35 — 09:50   15   exp. /pre prod
5/02/97    13:15 — 13:30   15   pre prod.
5102/97    16:30 — 16:45   15   pre prod.
51/02/97   09:25 — 09:45   15   pre prod.
5105/97    12:40 — 13:10   15   pre prod.
5105/97    17:15 — 17:45   15   pre prod.
5/20/97    07:45 — 08:15   15   pre prod.
5/20/97    19:15 — 19:30   15   pre prod.
5/22/97    10:15 — 10:25   15   pre prod.
5/22/97    12:00 — 12:30   15   pre prod.
5/22/97    16:15 — 16:45   15   pre prod.
5/27/97    09:15 — 09:45   15   pre prod.
5/27/97    18:30 — 19:00   15   pre prod.
5/28/97    15:30 — 16:00   15   pre prod.
5/30/97    14:45 — 15:15   15   pre prod.
6/03/97    17:15 — 17:45   15   pre prod.
6/10/97    13:20 — 13:50   15   pre prod.
6/11/97    08:25 — 08:55   15   pre prod.
6/17/97    15:35 — 16:05   15   pre prod.
6/19/97    10:00 — 10:30   15   pre prod.
7/15/97    09:30 — 09:45   15   pre prod.
7/15/97    10:15 — 10:45   15   pre prod.
7/31/97    14:05 — 14:20   15   pre prod.
8101/97    10:55 — 11:25   15   pre prod.
8/26/97    13:00 — 13:30   15   pre prod.
9/19/97    16:30 — 15:45   15   pre prod.
9/03/97    10:35 — 10:50   15   pre prod.
10/16/97   10:30 —11:00    15   pre prod.


4.0 Test Results
        Reviewing the testing program over the twelve months spanned, it can be seen that very
effective use was made of satellite access time. The performance of these tests in a laboratory
environment, enabled GeoPhone to improve the design of the next generation of its products by
incorporating design features that were uncovered during this experimental testing series. During this
experimental testing series, testing was done with two different terminal designs.
        The two experimental terminals were constructed using available commercial off the shelf
hardware and technology. Indoor Unit (IDU) ware comprised of rack mounted equipment in a four foot
rack cabinet. The Pre Production Terminals were integrated in a computer tower case using custom
software and hardware engineered specifically for this system.


4.1 Test results on the Experimental ( Demonstration) units
        The testing on the experimental units spanned the time period from August 1996 through March
1997 and were used to verify the design concept and the link performance parameters for the
experimental units. This testing enabled the improvement of some hardware and software features in
the experimental units and provided performance benchmarks to drive the design of the pre production
units. The satellite accesses were used to establish the reliability and robustness of this single channel
design. The key technologies evaluated during this experimental terminal program was to evaluate low
rate vocoders, new signal processing algorithms, a new spread spectrum modem and a unique hardware
architecture.   It should be noted the CAMA (Convolution Ambiguity Multiple Access) waveform
technique for this test was using MFSK (Multiple Frequency Shift Keying) modulation. The experimental
terminals were used to demonstrate CAMA operation over existing commercial satellites.
         These units provided one voice channel utilizing a generic SHARC DSP processor, codec, and
VSAT hardware. The SHARC DSP processor was programmed to validate the CAMA waveform. The
same SHARC DSP processor was used in the Pre Production Terminal to minimize the design changes
and risk.
        The tests performed during the experimental terminal program were designed to test that the
CAMA waveform could be used to provide a two way duplex voice link over an operational KU band
satellite and how robust the connection was during the call establishment and the conversation phase.
These tests were made over varying operational conditions while measuring the subjective quality of the
voice transmissions and BER bit error rate.
        We were able to determine how this new CAMA technique would operate in a commercial
satellite environment, with its rain fading, proximity of other carriers, Doppler frequency variations,
satellite frequency offsets, cross polarization interference effects.
        GeoPhone discovered that the frequency acquisition range of the CAMA modem was not broad
enough to acquire the return signal from the satellite with the frequency offset and design modifications
had to be made to the pre production terminals to compensate for this effect.


         The optimal signal levels for operating the various components in the system and the sensitivity
of this type of modulation to the non linear effects of saturation of components in the system were
determined which helped us to finalize the system design for the pre production terminals.
        We also found that we needed a large amount of isolation between the uplinks and the downlink
RF equipment to prevent interference, because of the sensitivity of the detection process. This directly
affected the design of the pre production terminals in that great care was used in its design to improve
the isolation.
         We discovered that day/night temperature variations could result in the accumulation of water in
the RF waveguide in a humid environment which could damage the equipment. We have made design
modifications to minimize this effect.
         The lessons learned during the testing of the experimental terminals enabled GeoPhone to make
design changes that reduced the equipment cost per channel from $50,000 to $3,000.
         During this testing we were able to test and evaluate the following satellite and terminal
characteristics and determine solutions for implementing them in the pre production prototypes.
                 o       Compensation of the Doppler shifted frequency of the satellite
                 o       Satellite flux density measurement (SFD)
                 o       Effect of the satellite transponder saturation characteristics on performance
                 o       Compensation of rate of drift and instability of the satellite frequency translation
                 o       Evaluation of power stability of link budget including fading characteristics
                 o        Effect of spatial satellite movement on link performance with a fixed antenna
                 o        Effect of interference signals in satellite environment
                 o       Telephone call setup, connection, and tear down over the satellite.
         GeoPhone reviewed the concept of utilizing a network pilot terminal for network frequency and
power control and based on test results obtained it was decided to implement a solution by using an
innovative software approach. This approach allowed us to have a lower cost terminal. This approach is
also consistent with GeoPhone hubless, full—mesh network concept which world allowed for the
implementation of a lower cost network sooner.
         The following design enhancements were added to the for the pre production units as a result of
the experimental terminal testing program and engineering development.
         1) Cost reduction.

         2) Frequency Aquistion/Tracking.

         3) Power control/ Throttling

         4) 500 MHz agility

         5) Design for C—band and Extended C—band operation

         6) Time multiplexed channels

         7) Flexible hardware design allowing enhancements to be added via software upgrade.

         8) Frequency Hopping for time multiplexed channels.


        9) Automatic switching of data, facsimile and voice.




4.2 Test results on the Pre Production Prototypes
        Eight pre production KU Band satellite terminals were constructed for test and evaluation. These
units use improved software and hardware designs which allowed the complete indoor unit (IDU) to be
constructed in a computer tower case and was designed to accommodate four time multiplexed voice,
data or facsimile channels simultaneously. The outdoor equipment (ODU) was specifically designed
with characteristics to provide improved performance and operational features. From March 1997 until
the present, testing was done over 1.2 Meter Ku band antennas over the SBS6 Satellite using these pre
production units.
    We have simulated the loading and the capacity of network using Matlab software. However, we
    are planning to test congestion scenarios over the satellite once our 8 terminal network is
    established.


4.3 Significant test events


        12/09/96 Testing of new crystal filters for shared subband operation.
        04/16/97    First sucessful telephone call using new modems and existing ODU
        05/02/97    First successful 10 minute call achieved with all new pre production units
        06/11/97    First successful telephone call between two terminals.
        06/18/97    Measurement of total delay including satellite link
        10/16/97 Testing of four voice channels between two terminals ( non time multiplexed)


5.0 Future Testing Plans
        GeoPhone is in the process of installing a eight terminal network by November 1997 that will
enable us to fully test the effects of network performance characteristics such as channel loading tests,
capacity tests as well as network power and frequency control algorithms. The antennas used for this
series of testing will be the FCC and Intelsat approved Prodelin 1.8 Meter Ku Band antennas as well as
the existing 1.2 Meter Channel Master antennas. The 1.8 Meter Antennas will be located in Annapolis,at
905 Commerce Drive, well within the 161 km FCC limit.
        The risk of operating a network at customer sites which will be located in developing countries
will be greatly reduced as a result of GeoPhone having tested and evaluated an operational eight
terminal satellite network in Annapolis.
        Once we have completed this series of testing, we will be able to start to ship networks to our
customers in developing countries for implementation.



Document Created: 2003-10-21 13:04:57
Document Modified: 2003-10-21 13:04:57

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