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Construction and Implementation of Tracking System for the ISAAC Sounding Rocket Experiment
KTH, School of Engineering Sciences (SCI), Physics.
KTH, School of Engineering Sciences (SCI), Physics.
2013 (English)Independent thesis Basic level (degree of Bachelor), 10 credits / 15 HE creditsStudent thesis
Abstract [en]

 

The ISAAC rocket experiment is part of the

REXUS–15 payload. It has two free-falling units performing

infrared spectroscopy between them. One of the free-falling units

will actively track the other in the sky so as to enable continuous

measurements. In this thesis report, the design of this tracking

solution is described. The general concept of the tracking process

is outlined, upon which the conceptuals as well as the hardware,

software and firmware of each subsystem are explained. Tests of

respective subsystems are conducted and conclusions are drawn

pertaining to the accuracy and suitability of each subsystem for

the tracking system.

Index Terms

—Tracking system, Sounding Rocket Experiment,

VHDL, REXUS, I

2C, FPGA, CMOS Camera Sensor, Sun Sensing,

Hardware Design, Software Design

Place, publisher, year, edition, pages
2013. , 13 p.
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-129344OAI: oai:DiVA.org:kth-129344DiVA: diva2:651784
Examiners
Available from: 2013-09-27 Created: 2013-09-27 Last updated: 2013-09-27Bibliographically approved

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Emil Lundkvist, Markus Silberstein Hont kandidatex(961 kB)318 downloads
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CiteExportLink to record
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Citation style
  • apa
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Output format
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