80NSSC18K0298

Background:
In support of NASA's Earth Surface and Interior (ESI) focus area, the Terrestrial Reference Frame (TRF) serves as the foundation for virtually all airborne, space-based, and ground-based Earth observations. This frame is developed by combining observations from satellite laser ranging (SLR), very long baseline interferometry (VLBI), the Global Navigation Satellite System (GNSS), and Doppler Orbitography and Radiopositioning Integrated by Satellite (DORIS) stations. It is realized as an international standard through the International Terrestrial Reference Frame (ITRF). Accurate knowledge of the relative measurement reference points between co-located systems is essential to combine the different measurement techniques and take full advantage of their strengths. However, the ITRF is currently limited in accuracy due to systematic errors in tying together the contributions from different geodetic techniques. As standard ground-based surveys have reached their capabilities, a new approach is required to extend technique ties into space.

Major Goals:
The proposed project aims to develop a new space flight instrument and verify a measurement concept that enables the determination of systematic errors between VLBI, GNSS, and SLR independent measurement techniques by extending surveying techniques out to spaceflight assets. The proposed instrument, functioning as a GNSS L-to-X-band transponder, establishes frequency compatibility between VLBI and GNSS, facilitating a direct space-based geodetic tie between these two radio-based techniques in post-processing. Additionally, separate laser retro-reflectors flown concurrently with the instrument would provide additional connection to the SLR network. The measurement concept only requires one VLBI station to observe the space vehicle, allowing the space vehicle to be in low-Earth orbit. This opens up the possibility of using inexpensive CubeSats or other small satellites, enabling the implementation of a cost-effective constellation of spacecraft to provide better global coverage and further improve the accuracy of the geodetic site ties.

Specific Tasks:
1) Develop a modified version of an existing space flight GNSS receiver to support GNSS relaying functionality and procure commercial space flight UHF (low data rate) and S/X-band (high data rate) digital data transmitters.
2) Design and fabricate a fit-form-function instrument capable of being implemented within a CubeSat/small satellite.
3) Bench test breadboard concept of GNSS-to-VLBI transponder with GNSS synthetic signal generators and space vehicle GNSS receivers.
4) Bench test breadboard concept of GNSS-to-VLBI transponder with GNSS synthetic signal generators and space vehicle GNSS receivers.
5) On-site ground test of GNSS-to-VLBI transponder at Goddard Geophysical Astronomical Observatory.
6) Airborne flight test evaluation of GNSS-to-VLBI transponder at Goddard Geophysical Astronomical Observatory.

University Of Massachusetts Lowell

BACKGROUND: IN SUPPORT OF NASA''S EARTH SURFACE AND INTERIOR (ESI) FOCUS AREA THE TERRESTRIAL REFERENCE FRAME (TRF) IS THE FOUNDATION FOR VIRTUALLY ALL AIRBORNE SPACE-BASED AND GROUND-BASED EARTH OBSERVATIONS. THIS FRAME IS DEVELOPED BY COMBINING THE OBSERVATIONS FROM SATELLITE LASER RANGING (SLR) VERY LONG BASELINE INTERFEROMETRY (VLBI) THE GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) AND DOPPLER ORBITOGRAPHY AND RADIOPOSITIONING INTEGRATED BY SATELLITE (DORIS) STATIONS AND IS REALIZED AS AN INTERNATIONAL STANDARD THROUGH THE INTERNATIONAL TERRESTRIAL REFERENCE FRAME (ITRF). COMBINING THE DIFFERENT MEASUREMENT TECHNIQUES IS ONLY POSSIBLE WITH ACCURATE KNOWLEDGE OF THE RELATIVE MEASUREMENT REFERENCE POINTS BETWEEN CO-LOCATED SYSTEMS AND DOING SO IS ESSENTIAL TO TAKE FULL ADVANTAGE OF THE STRENGTHS OF EACH TECHNIQUE. CURRENTLY THE ITRF IS LIMITED IN ACCURACY BY SYSTEMATIC ERRORS IN TYING TOGETHERTHE CONTRIBUTIONS FROM THE DIFFERENT GEODETIC TECHNIQUES. SINCE STANDARD GROUND-BASED SURVEYS PROVIDING TIES BETWEEN GEODETIC TECHNIQUES HAVE REACHED THE LIMIT OF THEIR CAPABILITIES A NEW APPROACH IS REQUIRED THAT EXTENDS TECHNIQUE TIES INTO SPACE. MAJOR GOALS: WE PROPOSE TO DEVELOP A NEW SPACE FLIGHT INSTRUMENT AND VERIFY A MEASUREMENT CONCEPT THAT ENABLES THE DETERMINATION OF SYSTEMATIC ERRORS BETWEEN THE VLBI GNSS AND SLR INDEPENDENT MEASUREMENT TECHNIQUES BY EXTENDING SURVEYING TECHNIQUES OUT TO SPACEFLIGHT ASSETS. THE PROPOSED INSTRUMENT FUNCTIONING AS A GNSS L-TO-X-BAND TRANSPONDER ESTABLISHES FREQUENCY COMPATIBILITY BETWEEN VLBI ANDGNSS THEREBY FACILITATING A DIRECT SPACE-BASED GEODETIC TIE BETWEEN THESE TWO RADIO-BASED TECHNIQUES IN POST- PROCESSING. SEPARATE LASER RETRO-REFLECTORS FLOWN CONCURRENTLY WITH GRITSS WOULD PROVIDE ADDITIONAL CONNECTION TO THE SLR NETWORK. BECAUSE THE MEASUREMENT CONCEPT BY WHICH THE VLBI/GNSS SYSTEMATIC ERRORS WILL BE DETERMINED ONLY REQUIRES ONE VLBI STATION TO OBSERVE THE SPACE VEHICLE THE SPACE VEHICLE MAY BE IN LOW-EARTH ORBIT. THIS IS ADVANTAGEOUS AS IT OPENS UP THE POSSIBILITY OF USING INEXPENSIVE CUBESATSOR OTHER SMALL SATELLITES MAKING IT POSSIBLE TO IMPLEMENT A COST-EFFECTIVE CONSTELLATION OF SPACECRAFT TO PROVIDE BETTER GLOBAL COVERAGE AND FURTHER IMPROVE THE ACCURACY OF THE GEODETIC SITE TIES. SPECIFIC TASKS: 1) DEVELOP MODIFIED VERSION OF AN EXISTING SPACE FLIGHT GNSS RECEIVER TO SUPPORT GNSS RELAYING FUNCTIONALITY PROCURE COMMERCIAL SPACE FLIGHT UHF (LOW DATA RATE) S AND X-BAND(HIGH DATA RATE) DIGITAL DATA TRANSMITTERS. 2) DESIGN AND FABRICATE A FIT-FORM-FUNCTION INSTRUMENT CAPABLE OF BEING IMPLEMENTED WITHIN A CUBESAT/SMALL SATELLITE. 3) BENCH TEST BREADBOARD CONCEPT OF GNSS-TO-VLBI TRANSPONDER WITH GNSS SYNTHETIC SIGNAL GENERATORS AND SPACE VEHICLE GNSS RECEIVERS. 4) BENCH TEST BREADBOARD CONCEPT OF GNSS-TO-VLBI TRANSPONDER WITH GNSS SYNTHETIC SIGNAL GENERATORS AND SPACE VEHICLE GNSS RECEIVERS. 5) ON SIGHT GROUND TEST OF GNSS-TO-VLBI TRANSPONDER AT GODDARD GEOPHYSICAL ASTRONOMICAL OBSERVATORY. 6) AIRBORNE FLIGHT TEST EVALUATION OF GNSS-TO-VLBI TRANSPONDER AT GODDARD GEOPHYSICAL ASTRONOMICAL OBSERVATORY.

43.001 - Science

Shared Services Center (NSSC) [NASA]

Lowell, Massachusetts 01854-3983 United States

Single Zip Code

NOT APPLICABLE

Amendment Since initial award the End Date has been extended from 02/14/20 to 09/30/26 and the total obligations have increased 2649% from $185,000 to $5,085,007.