Wagner, Paul und Hampf, Daniel und Sproll, Fabian und Hasenohr, Thomas und Humbert, Leif und Rodmann, Jens und Riede, Wolfgang (2016) Detection and laser ranging of orbital objects using optical methods. In: Proceedings of SPIE - The International Society for Optical Engineering. SPIE Optical Engineering and Applications, 2016-08-28 - 2016-09-01, San Diego, CA, USA. doi: 10.1117/12.2236919.
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Offizielle URL: http://proceedings.spiedigitallibrary.org/proceeding.aspx?articleid=2554542
Kurzfassung
Laser ranging to satellites (SLR) in earth orbit is an established technology used for geodesy, fundamental science and precise orbit determination. A combined active and passive optical measurement system using a single telescope mount is presented which performs precise ranging measurements of retro reflector equipped objects in low earth orbit (LEO). The German Aerospace Center (DLR) runs an observatory in Stuttgart where a system has been assembled completely from commercial off-the-shelf (COTS) components. The visible light directed to the tracking camera is used to perform angular measurements of objects under investigation. This is done astrometrically by comparing the apparent target position with cataloged star positions. First successful satellite laser ranging was demonstrated recently using an optical fiber directing laser pulses onto the astronomical mount. The transmitter operates at a wavelength of 1064 nm with a repetition rate of 3 kHz and pulse energy of 25 μJ. A motorized tip/tilt mount allows beam steering of the collimated beam with μrad accuracy. The returning photons reflected from the object in space are captured with the tracking telescope. A special low aberration beam splitter unit was designed to separate the infrared from visible light. This allows passive optical closed loop tracking and operation of a single photon detector for time of flight measurements at a single telescope simultaneously. The presented innovative design yields to a compact and cost effective but very precise ranging system which allows orbit determination. © (2016) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
elib-URL des Eintrags: | https://elib.dlr.de/107404/ | ||||||||||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||
Titel: | Detection and laser ranging of orbital objects using optical methods | ||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | 19 September 2016 | ||||||||||||||||||||||||||||||||
Erschienen in: | Proceedings of SPIE - The International Society for Optical Engineering | ||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||
DOI: | 10.1117/12.2236919 | ||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||
Stichwörter: | satellite laser ranging, optical telescope, low earth orbit, laser transmitter, fiber, single photon detector, space situational awareness, space debris | ||||||||||||||||||||||||||||||||
Veranstaltungstitel: | SPIE Optical Engineering and Applications | ||||||||||||||||||||||||||||||||
Veranstaltungsort: | San Diego, CA, USA | ||||||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||
Veranstaltungsbeginn: | 28 August 2016 | ||||||||||||||||||||||||||||||||
Veranstaltungsende: | 1 September 2016 | ||||||||||||||||||||||||||||||||
Veranstalter : | SPIE | ||||||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||||||||||||||||||
HGF - Programmthema: | Technik für Raumfahrtsysteme | ||||||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | R SY - Technik für Raumfahrtsysteme | ||||||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Space Debris / Laserbasiertes SSA (alt) | ||||||||||||||||||||||||||||||||
Standort: | Stuttgart | ||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Technische Physik | ||||||||||||||||||||||||||||||||
Hinterlegt von: | Wagner, Dr. Paul | ||||||||||||||||||||||||||||||||
Hinterlegt am: | 10 Nov 2016 11:53 | ||||||||||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:12 |
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