System Design for Attitude and Orbit Control System for DelFFI Formation Flying Mission
Date
2017
Authors
Journal Title
Journal ISSN
Volume Title
Publisher
Tartu Ülikool
Abstract
This thesis designs system architecture for DelFFi nanosatellite. The objective of the DelFFi
mission is to demonstrate autonomous formation flying between two identical CubeSats, named
Delta and Phi. The thesis updates existing requirements and develops a final set of requirements
for the DelFFi mission. Secondly, the thesis considers hardware problems with the Delfi-n3Xt
mission and analyzes formation flying mission hardware architectures. Furthermore, it proposes
new hardware architecture for DelFFi mission. Finally, the thesis analyzes software requirements
and develops new software architecture for DelFFi attitude and orbit control system.
Description
Keywords
AOCS; ADCS; Requirements; Hardware System Design; Software System Design, Süsteemi disain; Asendi määramis ja kontrollimis süsteem; nõuded; Tarkvara arhitektuur; Riistvara arhitektuur