Show simple item record

dc.contributor.authorMarlow, Weston A.
dc.contributor.authorCarlton, Ashley K.
dc.contributor.authorYoon, Hyosang
dc.contributor.authorClark, James R.
dc.contributor.authorHaughwout, Christian Alexander
dc.contributor.authorCahoy, Kerri
dc.contributor.authorMales, Jared R.
dc.contributor.authorClose, Laird M.
dc.contributor.authorMorzinski, Katie M.
dc.date.accessioned2019-08-02T19:01:32Z
dc.date.available2019-08-02T19:01:32Z
dc.date.issued2017-03
dc.date.submitted2016-11
dc.identifier.issn0022-4650
dc.identifier.issn1533-6794
dc.identifier.urihttps://hdl.handle.net/1721.1/121963
dc.description.abstractIn this study, the feasibility and utility of using a maneuverable nanosatellite laser guide star from a geostationary equatorial orbit have been assessed to enable ground-based, adaptive optics imaging of geosynchronous satellites with next-generation extremely large telescopes. The concept for a satellite guide star was first discussed in the literature by Greenaway and Clark in the early 1990s ("PHAROS: An Agile Satellite-Borne Laser Guidestar," Proceedings of SPIE, Vol. 2120, 1994, pp. 206-210), and expanded upon by Albert in 2012 ("Satellite-Mounted Light Sources as Photometric Calibration Standards for Ground-Based Telescopes," Astronomical Journal, Vol. 143, No. 1, 2012, p. 8). With a satellite-based laser as an adaptive optics guide star, the source laser does not need to scatter, and is well above atmospheric turbulence. When viewed from the ground through a turbulent atmosphere, the angular size of the satellite guide star is much smaller than a backscattered source. Advances in small-satellite technology and capability allowed the revisiting of the concept on a 6UCubeSat, measuring 10 × 20 × 30 cm. It is shown that a system that uses a satellite-based laser transmitter can be relatively low power (∼1 W transmit power) and operated intermittently. Although the preliminary analysis indicates that a single satellite guide star cannot be used for observing multiple astronomical targets, it will only require a little propellant to relocate within the geosynchronous belt. Results of a design study on the feasibility of a small-satellite guide star have been presented, and the potential benefits to astronomical imaging and to the larger space situational awareness community have been highlighted.en_US
dc.description.sponsorshipUnited States. Air Force Office of Scientific Research (Contract FA8721-05-C-0002)en_US
dc.description.sponsorshipAir Force Office of Scientific Research (Contract FA8702-15-D-0001)en_US
dc.language.isoen
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)en_US
dc.relation.isversionofhttp://dx.doi.org/10.2514/1.a33680en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourceProf. Cahoy via Barbara Williamsen_US
dc.titleLaser-Guide-Star Satellite for Ground-Based Adaptive Optics Imaging of Geosynchronous Satellitesen_US
dc.typeArticleen_US
dc.identifier.citationMarlow, Weston A. et al. "Laser-Guide-Star Satellite for Ground-Based Adaptive Optics Imaging of Geosynchronous Satellites." Journal of Spacecraft and Rockets 53, 4 (March 2017): A33680 © 2016 Massachusetts Institute of Technologyen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.contributor.departmentLincoln Laboratoryen_US
dc.relation.journalJournal of Spacecraft and Rocketsen_US
dc.eprint.versionOriginal manuscripten_US
dc.type.urihttp://purl.org/eprint/type/JournalArticleen_US
eprint.statushttp://purl.org/eprint/status/NonPeerRevieweden_US
dc.date.updated2019-08-02T17:57:35Z
dspace.date.submission2019-08-02T17:57:37Z
mit.journal.volume54en_US
mit.journal.issue3en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record