Development of a hardware-in-the-loop attitude control simulator for EIRSAT-1, a magnetically actuated 2U CubeSat

Masoud Emam; Joseph Thompson; Daire Sherwin; Maeve Doyle; Rachel Dunwoody; Jessica Erkal; Joe Flanagan; Gianluca Fontanesi; Andrew Gloster; Joseph Mangan; David Murphy; Favour Okosun; Conor O'Toole; Rakhi Rajagopalan Nair; Jack Reilly; Lána Salmon; Sarah Walsh; Paul Cahill; Umair Javaid; Daithí de Faoite; Kenneth Stanton; Alexei Ulyanov; Ronan Wall; Sheila McBreen; Lorraine Hanlon; William O'Connor; David McKeown

Development of a hardware-in-the-loop attitude control simulator for EIRSAT-1, a magnetically actuated 2U CubeSat

Masoud Emam, Joseph Thompson, Daire Sherwin, Maeve Doyle, Rachel Dunwoody, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster, Joseph Mangan, David Murphy, Favour Okosun, Conor O'Toole, Rakhi Rajagopalan Nair, Jack Reilly, Lána Salmon, Sarah Walsh, Paul Cahill, Umair Javaid, Daithí de FaoiteKenneth Stanton, Alexei Ulyanov, Ronan Wall, Sheila McBreen, Lorraine Hanlon, William O'Connor, David McKeown

University College Dublin

Research output: Contribution to journal › Conference article › peer-review

Abstract

Attitude determination and control system (ADCS) is one of the essential subsystems of a satellite that requires thorough testing before launch. Hardware-In-the-Loop simulation is a well-known approach to test the ADCS subsystem. A novel structure for HIL simulation is addressed in this paper, with the main aim of introducing a cost effective and easy to implement simulator for CubeSats. To achieve this aim, a motorised gimbal testbed is presented as the alternative for to air bearing low friction testbeds which are widely used in CubeSat HIL simulators. HIL simulation results for EIRSAT-1, a 2U CubeSat being designed and built at University College Dublin, are presented in this paper.

Original language	English
Article number	IAC-19_C1_IP_16_x53626
Journal	Proceedings of the International Astronautical Congress, IAC
Volume	2019-October
Publication status	Published - 2019
Externally published	Yes
Event	70th International Astronautical Congress, IAC 2019 - Washington, United States Duration: 21 Oct 2019 → 25 Oct 2019

Keywords

ADCS
CubeSat
EIRSAT-1
HILS
PILS
Real-time simulation
Testbed

Cite this

Emam, M., Thompson, J., Sherwin, D., Doyle, M., Dunwoody, R., Erkal, J., Flanagan, J., Fontanesi, G., Gloster, A., Mangan, J., Murphy, D., Okosun, F., O'Toole, C., Nair, R. R., Reilly, J., Salmon, L., Walsh, S., Cahill, P., Javaid, U., ... McKeown, D. (2019). Development of a hardware-in-the-loop attitude control simulator for EIRSAT-1, a magnetically actuated 2U CubeSat. Proceedings of the International Astronautical Congress, IAC, 2019-October, Article IAC-19_C1_IP_16_x53626.

@article{9babb2e0e9d941a8865eec3576599b8c,

title = "Development of a hardware-in-the-loop attitude control simulator for EIRSAT-1, a magnetically actuated 2U CubeSat",

abstract = "Attitude determination and control system (ADCS) is one of the essential subsystems of a satellite that requires thorough testing before launch. Hardware-In-the-Loop simulation is a well-known approach to test the ADCS subsystem. A novel structure for HIL simulation is addressed in this paper, with the main aim of introducing a cost effective and easy to implement simulator for CubeSats. To achieve this aim, a motorised gimbal testbed is presented as the alternative for to air bearing low friction testbeds which are widely used in CubeSat HIL simulators. HIL simulation results for EIRSAT-1, a 2U CubeSat being designed and built at University College Dublin, are presented in this paper.",

keywords = "ADCS, CubeSat, EIRSAT-1, HILS, PILS, Real-time simulation, Testbed",

author = "Masoud Emam and Joseph Thompson and Daire Sherwin and Maeve Doyle and Rachel Dunwoody and Jessica Erkal and Joe Flanagan and Gianluca Fontanesi and Andrew Gloster and Joseph Mangan and David Murphy and Favour Okosun and Conor O'Toole and Nair, {Rakhi Rajagopalan} and Jack Reilly and L{\'a}na Salmon and Sarah Walsh and Paul Cahill and Umair Javaid and {de Faoite}, Daith{\'i} and Kenneth Stanton and Alexei Ulyanov and Ronan Wall and Sheila McBreen and Lorraine Hanlon and William O'Connor and David McKeown",

note = "Publisher Copyright: Copyright {\textcopyright} 2019 by the International Astronautical Federation (IAF). All rights reserved.; 70th International Astronautical Congress, IAC 2019 ; Conference date: 21-10-2019 Through 25-10-2019",

year = "2019",

language = "English",

volume = "2019-October",

journal = "Proceedings of the International Astronautical Congress, IAC",

issn = "0074-1795",

}

Emam, M, Thompson, J, Sherwin, D, Doyle, M, Dunwoody, R, Erkal, J, Flanagan, J, Fontanesi, G, Gloster, A, Mangan, J, Murphy, D, Okosun, F, O'Toole, C, Nair, RR, Reilly, J, Salmon, L, Walsh, S, Cahill, P, Javaid, U, de Faoite, D, Stanton, K, Ulyanov, A, Wall, R, McBreen, S, Hanlon, L, O'Connor, W & McKeown, D 2019, 'Development of a hardware-in-the-loop attitude control simulator for EIRSAT-1, a magnetically actuated 2U CubeSat', Proceedings of the International Astronautical Congress, IAC, vol. 2019-October, IAC-19_C1_IP_16_x53626.

TY - JOUR

T1 - Development of a hardware-in-the-loop attitude control simulator for EIRSAT-1, a magnetically actuated 2U CubeSat

AU - Emam, Masoud

AU - Thompson, Joseph

AU - Sherwin, Daire

AU - Doyle, Maeve

AU - Dunwoody, Rachel

AU - Erkal, Jessica

AU - Flanagan, Joe

AU - Fontanesi, Gianluca

AU - Gloster, Andrew

AU - Mangan, Joseph

AU - Murphy, David

AU - Okosun, Favour

AU - O'Toole, Conor

AU - Nair, Rakhi Rajagopalan

AU - Reilly, Jack

AU - Salmon, Lána

AU - Walsh, Sarah

AU - Cahill, Paul

AU - Javaid, Umair

AU - de Faoite, Daithí

AU - Stanton, Kenneth

AU - Ulyanov, Alexei

AU - Wall, Ronan

AU - McBreen, Sheila

AU - Hanlon, Lorraine

AU - O'Connor, William

AU - McKeown, David

PY - 2019

Y1 - 2019

N2 - Attitude determination and control system (ADCS) is one of the essential subsystems of a satellite that requires thorough testing before launch. Hardware-In-the-Loop simulation is a well-known approach to test the ADCS subsystem. A novel structure for HIL simulation is addressed in this paper, with the main aim of introducing a cost effective and easy to implement simulator for CubeSats. To achieve this aim, a motorised gimbal testbed is presented as the alternative for to air bearing low friction testbeds which are widely used in CubeSat HIL simulators. HIL simulation results for EIRSAT-1, a 2U CubeSat being designed and built at University College Dublin, are presented in this paper.

AB - Attitude determination and control system (ADCS) is one of the essential subsystems of a satellite that requires thorough testing before launch. Hardware-In-the-Loop simulation is a well-known approach to test the ADCS subsystem. A novel structure for HIL simulation is addressed in this paper, with the main aim of introducing a cost effective and easy to implement simulator for CubeSats. To achieve this aim, a motorised gimbal testbed is presented as the alternative for to air bearing low friction testbeds which are widely used in CubeSat HIL simulators. HIL simulation results for EIRSAT-1, a 2U CubeSat being designed and built at University College Dublin, are presented in this paper.

KW - ADCS

KW - CubeSat

KW - EIRSAT-1

KW - HILS

KW - PILS

KW - Real-time simulation

KW - Testbed

UR - http://www.scopus.com/inward/record.url?scp=85079128908&partnerID=8YFLogxK

M3 - Conference article

AN - SCOPUS:85079128908

SN - 0074-1795

VL - 2019-October

JO - Proceedings of the International Astronautical Congress, IAC

JF - Proceedings of the International Astronautical Congress, IAC

M1 - IAC-19_C1_IP_16_x53626

T2 - 70th International Astronautical Congress, IAC 2019

Y2 - 21 October 2019 through 25 October 2019

ER -

Development of a hardware-in-the-loop attitude control simulator for EIRSAT-1, a magnetically actuated 2U CubeSat

Abstract

Keywords

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