Network-based Navigation

Metadata Updated: February 28, 2019

With the expansion of communication assets into planetary networks, such as the Mars Network, there exists a great opportunity to integrate a new solar system-wide navigation system.Initial networks, such as Mars Reconnaissance Orbiter (MRO) operating as a communications relay for Mars ground-based assets, show that the capability exists for such a distributed networking system. Research into Delay-[HTML_REMOVED]Disruption-Tolerant Networking is developing a protocol for high-bandwidth reliable communication There is a range of navigation techniques in use for spacecraft in deep space. Traditional techniques involve optical navigation, in which the bearing and range (or multiple bearings) to a celestial object(s) are combined with known ephemeris information to calculate a position fix. The application of this method is constrained by the optical observation capabilities. There is also a requirement for ground support to analyze the optical images and compute the navigation fix. Research into Autonav moves this analysis onboard the spacecraft, at the cost of a large a priori knowledge requirement and increased mission planning to tell the spacecraft when and where to point in order to capture observations for a navigation fix. This capability is also limited by knowledge of the observed objects[HTML_REMOVED] ephemeris. Another method is to use radio waves to determine range and radial velocity. The range is calculated by measuring the time it takes a tone to travel to the spacecraft and return to the ground (two-way ranging) and radial velocity is measured by capturing the Doppler shift inherent in the received signal (of an initially known frequency). The angular position in the sky is captured by antenna tracking techniques which utilize specialized hardware and software to analyze the power of the received signal. This measured angular position can be improved by DDOR techniques, which utilize multiple antennas and observations of a known source to capture errors, to the order of nanoradians. This process is very sophisticated, requires a large amount of ground hardware and analytical support. Research into software-defined radios has developed the Electra instrument, which can perform in-orbit radiometric ranging and Doppler tracking. Currently this is only implemented on UHF radios, which limit the range and applicability of the solution. Additional methods utilize dead reckoning and measurements of the intrinsic state through highly accurate inertial navigation units.

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Public: This dataset is intended for public access and use. License: U.S. Government Work

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Dates

Metadata Created Date August 1, 2018
Metadata Updated Date February 28, 2019

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date February 28, 2019
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_10929
Maintainer
TECHPORT SUPPORT
Maintainer Email
Public Access Level public
Bureau Code 026:00
Metadata Context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
Metadata Catalog ID https://data.nasa.gov/data.json
Schema Version https://project-open-data.cio.gov/v1.1/schema
Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
Harvest Object Id 58a3a666-7b45-4fd5-b3c2-cedbdd8abf5f
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2012-09-01
Homepage URL https://techport.nasa.gov/view/10929
License http://www.usa.gov/publicdomain/label/1.0/
Data Last Modified 2018-07-19
Program Code 026:027
Source Datajson Identifier True
Source Hash 27fd4d6dbee96ad165854dea8279b3dc8af8a781
Source Schema Version 1.1

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