Virtual Telescope Alignment System

Metadata Updated: March 23, 2019

Next-generation space telescopes require two spacecraft to fly in a coordinated fashion in space forming a virtual telescope. Achieving and maintaining this precise formation alignment is achieved with guidance, navigation, and control (GN[HTML_REMOVED]C). The Virtual Telescope Alignment System (VTAS) is a prototype GN[HTML_REMOVED]C system to sense and maintain on-target formation alignment. This project is a multi-year effort focused on the development, integration, and testing of the VTAS using commercial CubeSat-class hardware and in-house developed software. This multi-year effort is to develop a prototype GN[HTML_REMOVED]C system (sensors, actuators, and algorithms), VTAS, and test it on the ground as a means for maturing the[HTML_REMOVED]TRL of this systems-level technology. Raising the[HTML_REMOVED]maturity of a prototype system reduces the risk for missions requiring dual spacecraft precise[HTML_REMOVED]inertial alignment. Heliophysics and Astrophysics missions such as a solar coronagraph, exo-planet finder, black hole x-ray and gamma-ray imager, solar flare x-ray and extreme ultraviolet imager, etc benefit from this advancement.Next-generation space telescopes require large separation distances between two elements of a science payload such as an occulting disk and a camera, or a lens and detector, making them too large to launch into space. A solution to this problem is to replace the structure of a traditional large monolithic space telescope with the science payload and GN[HTML_REMOVED]C distributed amongst the two spacecraft. For example, a solar coronagraph requires an occulting disk on one spacecraft and a camera on the other spacecraft with the two spacecraft separated by a large distance (hundreds of meters) with precise inertial alignment on the order of sub-arc-seconds. The two spacecraft use GN[HTML_REMOVED]C to fly in[HTML_REMOVED]coordination and align themselves to an inertial target of interest. Formation flying offers the ability to increase the separation distance, which leads to decreased errors from vignetting and diffracted light.[HTML_REMOVED]

Access & Use Information

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 March 23, 2019

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date March 23, 2019
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_17383
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
Datagov Dedupe Retained 20190322235447
Harvest Object Id e884a794-ccbf-4f1b-8ef0-a380e7c402f4
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2015-09-01
Homepage URL https://techport.nasa.gov/view/17383
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 6be99cadd2dd064bb52adabe2b566f22c3e8b6e4
Source Schema Version 1.1

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