Change search
ReferencesLink to record
Permanent link

Direct link
Optimization of a Laser Coarse Pointing Assembly for Low Earth Orbit Satellite Missions
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
2016 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

A laser communications terminal was developed by the Deutsches Zentrum für Luft- und Raumfahrt and is already being flown over the BIROS satellite, however it is desired to improvepointing performance with the utilization of a coarse pointing assembly. This study presents theseries of optimizations towards space applicability performed on an existing coarse pointingassembly for such a laser communications terminal. This module was initially built for airborneapplications and tested upon the tornado aircraft. The idea was to use this existing flight performanceproven system and with the help of commercial off the shelf components providebetter structural stability and tolerance to the Low Earth Orbit space environment. Criticalpoints were highlighted and the scope of the study was defined to provide reliable modal andthermal analysis results for its performance under the specified mission design parameters. Acircular low earth orbit of 450 km altitude with an inclination similar to that of the BIROS satellitewas chosen to simulate the space environmental effects for this analysis. A preliminary designreview highlighted the need to increase the link budget, which brought down the beamdivergence to 50 μrad from a previous 100 μrad. This made the entire system sensitive andmore susceptible to environmental factors requiring a more rigid and deformation tolerantstructure. In this study the effect of thermal loadings in worst-case scenarios were analysed.Aside from the optimization changes, the results of the analysis pointed out the need to utilizethermal control measures for optimum performance. Therefore, some passive thermal controlmeasures are also presented in this study, which are necessary to meet the requirements.

Place, publisher, year, edition, pages
2016. , 73 p.
National Category
Aerospace Engineering
URN: urn:nbn:se:ltu:diva-60946OAI: diva2:1052365
External cooperation
Deutsches Zentrum für Luft- und Raumfahrt (DLR); Julius Maximilian University of Würzburg
Educational program
Space Engineering, master's level (120 credits)
Available from: 2016-12-13 Created: 2016-12-06 Last updated: 2016-12-13Bibliographically approved

Open Access in DiVA

No full text

By organisation
Space Technology
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar

Total: 33 hits
ReferencesLink to record
Permanent link

Direct link