Cubeth ADCS design, implementation and validation tests

Stefano Rossi, Anton Ivanov, Guillaume Faure, Beat Geissman, Jerome Amiguet, Raphael Valceschini, Marcel Starein, Raphael Zufferey, Gaëtan Burri

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Citation (Scopus)

Abstract

CubETH is a one unit CubeSat developed in collaboration between EPFL (Lausanne) and ETH Zurich. The main objective of CubETH is to demonstrate the use of commercial GNSS receivers in space and test Precision Orbit Determination algorithms. One of the key driving requirements is to provide nadir pointing with a 20 degrees of precision and rotation rate less than 2 degree/second, in order to track GNSS constellation satellites. In this paper the solutions for the ADCS and the designed operatives modes are described. The ADCS shall provide for the Payload a nadir pointing with relaxed requirements, and in order to do that the team paid particular attention to the validation of the chosen hardware and software solutions. According the experience of SwissCube, its five years of data collected and lessons learned, we have started a vigorous process of design, implementation and validation for ADCS with several test setups and characterizations for sensors and actuators. We present the ADCS focusing mainly in the implementation, in the errors encountered and the process of validation in our test setups. A ball bearing with a Helmotz Cage has been used to validate the functionality of implemented algorithms (B-dot, TRIAD and an Extended Kalman Filter), results will be presented. Sensors calibrations and characterizations are addressed giving particular emphasis on their thermal drifts that can affect the determination process. Tests in Thermal Chambers show some interesting behaviours of the selected COTS sensors. A vigorous test campaign has been done on the first batch of Sun Sensors revealing not negligible effects that should be taken into account during final implementation. Even the actuators (magnetorquers) have been heavily tested to characterize their dipoles; tests revealed a really good match between the theoretical models and the hardware. Several test setups have been designed in order to characterize separately COTS components, and actuators for ADCS but more remarkable is the effort that has been spent for the validation of the whole ADCS system: one of the most challenging subsystem for CubeSat is the ADCS due to the several test setup and validations necessary to prove its functionality.

Original languageEnglish
Title of host publication66th International Astronautical Congress 2015, IAC 2015
Subtitle of host publicationSpace - The Gateway for Mankind's Future
PublisherInternational Astronautical Federation, IAF
Pages10665-10678
Number of pages14
ISBN (Electronic)9781510818934
Publication statusPublished - 2015
Externally publishedYes
Event66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015 - Jerusalem, Israel
Duration: 12 Oct 201516 Oct 2015

Publication series

NameProceedings of the International Astronautical Congress, IAC
Volume13
ISSN (Print)0074-1795

Conference

Conference66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015
Country/TerritoryIsrael
CityJerusalem
Period12/10/1516/10/15

Fingerprint

Dive into the research topics of 'Cubeth ADCS design, implementation and validation tests'. Together they form a unique fingerprint.

Cite this