Software in the loop test set-up of a tethered nano-satellite

Carina Pereira; Varun Kashyap; Naman Saxena; Smit Kamal; Revathi Ravula; Raunaq Rakesh

doi:10.1109/AERO.2016.7500603

Software in the loop test set-up of a tethered nano-satellite

Carina Pereira, Varun Kashyap, Naman Saxena, Smit Kamal, Revathi Ravula, Raunaq Rakesh

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

2 Citations (Scopus)

Abstract

This paper describes the software in loop test bed developed in order to test the control system of a tethered nano-satellite simulated under de-orbiting conditions. The entire ADCS architecture of the satellite along with the descriptions of the individual models constituting the Software in-the loop test bed, such as descent modeling algorithm, the sun model, the eclipse model, disturbance torques model, quaternion estimation algorithm and control system designs have been presented. The entire software in loop test bed along with the results have been analyzed and described in the paper.

Original language	English
Title of host publication	2016 IEEE Aerospace Conference, AERO 2016
Publisher	IEEE Computer Society
Volume	2016-June
ISBN (Electronic)	9781467376761
DOIs	https://doi.org/10.1109/AERO.2016.7500603
Publication status	Published - 27-06-2016
Externally published	Yes
Event	2016 IEEE Aerospace Conference, AERO 2016 - Big Sky, United States Duration: 05-03-2016 → 12-03-2016

Publication series

Name	IEEE Aerospace Conference Proceedings
Volume	2016-June
ISSN (Print)	1095-323X

Conference

Conference	2016 IEEE Aerospace Conference, AERO 2016
Country/Territory	United States
City	Big Sky
Period	05-03-16 → 12-03-16

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science

Access to Document

10.1109/AERO.2016.7500603

Cite this

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title = "Software in the loop test set-up of a tethered nano-satellite",

abstract = "This paper describes the software in loop test bed developed in order to test the control system of a tethered nano-satellite simulated under de-orbiting conditions. The entire ADCS architecture of the satellite along with the descriptions of the individual models constituting the Software in-the loop test bed, such as descent modeling algorithm, the sun model, the eclipse model, disturbance torques model, quaternion estimation algorithm and control system designs have been presented. The entire software in loop test bed along with the results have been analyzed and described in the paper.",

author = "Carina Pereira and Varun Kashyap and Naman Saxena and Smit Kamal and Revathi Ravula and Raunaq Rakesh",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 2016 IEEE Aerospace Conference, AERO 2016 ; Conference date: 05-03-2016 Through 12-03-2016",

year = "2016",

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day = "27",

doi = "10.1109/AERO.2016.7500603",

language = "English",

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Pereira, C, Kashyap, V, Saxena, N, Kamal, S, Ravula, R & Rakesh, R 2016, Software in the loop test set-up of a tethered nano-satellite. in 2016 IEEE Aerospace Conference, AERO 2016. vol. 2016-June, 7500603, IEEE Aerospace Conference Proceedings, vol. 2016-June, IEEE Computer Society, 2016 IEEE Aerospace Conference, AERO 2016, Big Sky, United States, 05-03-16. https://doi.org/10.1109/AERO.2016.7500603

TY - GEN

T1 - Software in the loop test set-up of a tethered nano-satellite

AU - Pereira, Carina

AU - Kashyap, Varun

AU - Saxena, Naman

AU - Kamal, Smit

AU - Ravula, Revathi

AU - Rakesh, Raunaq

PY - 2016/6/27

Y1 - 2016/6/27

N2 - This paper describes the software in loop test bed developed in order to test the control system of a tethered nano-satellite simulated under de-orbiting conditions. The entire ADCS architecture of the satellite along with the descriptions of the individual models constituting the Software in-the loop test bed, such as descent modeling algorithm, the sun model, the eclipse model, disturbance torques model, quaternion estimation algorithm and control system designs have been presented. The entire software in loop test bed along with the results have been analyzed and described in the paper.

AB - This paper describes the software in loop test bed developed in order to test the control system of a tethered nano-satellite simulated under de-orbiting conditions. The entire ADCS architecture of the satellite along with the descriptions of the individual models constituting the Software in-the loop test bed, such as descent modeling algorithm, the sun model, the eclipse model, disturbance torques model, quaternion estimation algorithm and control system designs have been presented. The entire software in loop test bed along with the results have been analyzed and described in the paper.

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M3 - Conference contribution

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T3 - IEEE Aerospace Conference Proceedings

BT - 2016 IEEE Aerospace Conference, AERO 2016

PB - IEEE Computer Society

T2 - 2016 IEEE Aerospace Conference, AERO 2016

Y2 - 5 March 2016 through 12 March 2016

ER -

Software in the loop test set-up of a tethered nano-satellite

Abstract

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Conference

All Science Journal Classification (ASJC) codes

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