Master Thesis - OUFTI-1
Master Thesis - OUFTI-1 Master Thesis - OUFTI-1
[26] P. HARIS. "PC/104-Plus Specication, Version 2.2 ". PC/104 Embedded Consortium, San Francisco, United States, 2007. [27] K. CAN. "Projet de Nanosatellite OUFTI-1: Développement du Logiciel Embarqué". Master thesis, University of Liège, Belgium, 2010. [28] N. CROSSET. "Implémentation du Relais D-STAR à Bord du Nanosatellite OUFTI- 1 ". Master thesis, GRAMME Institute, Belgium, 2010. [29] N. MARCHAL. "Design, Implémentation et Test de l'Architecture du Système de Télécommunication du CubeSat OUFTI-1 ". Master thesis, GRAMME Institute, Belgium, 2010. [30] A. KALMAN. "Midplane Stando Kit ". Pumpkin Inc., San Francisco, United States, 2008. [31] T. KOIZUMI et al. "Identication of the Center-of-Gravity and Inertia Terms of 3-Dimensional Body". Department of Engineering, Doshisha University, Japan, 2006. [32] "Dassault Systemes - Catia Website ". http://www.3ds.com/products/catia/welcome/. [33] N. FRANCOIS. "Integration Procedure for the Engineering Model of OUFTI-1 ". Technical Report, University of Liège, Belgium, 2010. [34] "Samtech Website". http://www.samcef.com/page.aspid=3&langue=EN [35] J.-Ph. NOEL. "Thermal Issues Settlement and Test Procedure Investigation of OUFTI-1 Nanosatellite". Master thesis, University of Liège, Belgium, 2010. [36] "Kokam Catalog". http://kokamamerica.com/kokam_catalog.pdf. [37] J. PEDERSEN. "Vega's CubeSats Design Specication ". Workshop on the Verication of the CubeSats for the Vega Maiden Flight, ESA-ESTEC, Noordwijk, The Netherlands, 2010. [38] M. ASHBY. "Materials Selection in Mechanical Design ". Butterworth-Heinemann, 1999. [39] J. LECOMTE-BECKERS. "Materials Selection". LTAS, University of Liège, Belgium, 2009. 127
[40] "Dejond - Aluminum Catalog ". http://www.dejond.com/EN/Downloads/metals/Dejond%20aluminium.pdf. [41] "Minco - Polyimide Thermofoil Heaters ". http://www.minco.com/uploadedFiles/Products/Thermofoil_Heaters/Kapton_Heaters/ hs202b-hk.pdf. [42] "Klixon 3BT and 4BT Series Catalog ". [43] "Red Book - Aerospace Thermal Control Materials ". http://www.sheldahl.com/Product/bulletins/Redbook.pdf, 2007. [44] R. AMY, G. AGLIETTI & G. RICHARDSON. "Accuracy of Simplied Printed Circuit Board Finite Element Models ". Microelectronics Reliability 50 (2010), 86-97. [45] R. AMY, G. AGLIETTI & G. RICHARDSON. "Sensitivity Analysis of Simpli- ed Printed Circuit Board Finite Element Models ". Microelectronics Reliability 49 (2009), 791-799. [46] D. WATTIAUX, O.VERLINDEN & Ch. DE FRUYTIER. "Modelling of the Dynamic Behaviour of Modular Equipments Designed by Thales Alenia Space ETCA". [47] R. AMY, G. AGLIETTI & G. RICHARDSON. "Simplied Modelling of Printed Circuit Boards for Spacecraft Applications ". Acta Astronautica 65 (2009), 192-201. [48] R. AMY, G. AGLIETTI & G. RICHARDSON. "Analysis of Simplied FE Models of PCBs Exposed to Random Vibrations". Proceedings of ISMA 2008: Durability Testing - Vibration Control, 979-986. [49] J. PITARRESI et al. "Dynamic Modeling and Measurement of Personal Computer Motherboards". Electronic Components and Technology Conference (2002), 597-603. [50] D. BAKER & Y. CHEN. "Modeling the Vibration Restraints of Wedge Lock Card Guides". ASME, Journal of Electronic Packaging 115 (1993), Issue 2, 189-194. [51] D.J. EWINS. Modal Testing: Theory, Practice and Application. Second Edition, Research Studies Press LTD, 2000. [52] N. MAIA & J. SILVA. Theoretical and Experimental Modal Analysis. Research Studies Press LTD, 1997. 128
- Page 77 and 78: Figure 4.4: Illustration of the exp
- Page 79 and 80: Figure 4.5: MAC between the two mod
- Page 81 and 82: • Global mass/stiness smearing me
- Page 83 and 84: 4.2.6 Modeling of the chassis A gen
- Page 85 and 86: Q = ω k = 1 ω b − ω a 2 ζ ⇒
- Page 87 and 88: Their study was based on the fact t
- Page 89 and 90: Figure 4.14: Example of spacecraft
- Page 91 and 92: Figure 4.15: Location of measuremen
- Page 93 and 94: Figure 4.18: MAC matrix using the s
- Page 95 and 96: 4.3.6 Application of the local mass
- Page 97 and 98: ρ P C 104 connector = 10.12 × 10
- Page 99 and 100: According to this particular shape,
- Page 101 and 102: This is due to the fact that this c
- Page 103 and 104: environment. Then, this model is ex
- Page 105 and 106: 5.2.4 Antenna support For the anten
- Page 107 and 108: Components Young's moduli (GP a) Po
- Page 109 and 110: Components Young's moduli (GP a) Po
- Page 111 and 112: 5.3 Static analysis As described in
- Page 113 and 114: Figure 5.9: Illustration of the com
- Page 115 and 116: Figure 5.11: Maximal Von Mises stre
- Page 117 and 118: Figure 5.12: First mode of OUFTI-1
- Page 119 and 120: Figure 5.15: Precise PSD of Vega [5
- Page 121 and 122: Chapter 6 Conclusions This master t
- Page 123 and 124: provided for each method used. We h
- Page 125 and 126: last versions of the Verication Con
- Page 127: [13] Ph. LEDENT. "Design and Implem
- Page 131 and 132: Appendix A Schemas of solar panels
- Page 133 and 134: Appendix B Schemas of electronic ca
- Page 135 and 136: Appendix C Fixations of the endless
- Page 137 and 138: Appendix D Datasheet of the battery
[26] P. HARIS. "PC/104-Plus Specication, Version 2.2 ". PC/104 Embedded Consortium,<br />
San Francisco, United States, 2007.<br />
[27] K. CAN. "Projet de Nanosatellite <strong>OUFTI</strong>-1: Développement du Logiciel Embarqué".<br />
<strong>Master</strong> thesis, University of Liège, Belgium, 2010.<br />
[28] N. CROSSET. "Implémentation du Relais D-STAR à Bord du Nanosatellite <strong>OUFTI</strong>-<br />
1 ". <strong>Master</strong> thesis, GRAMME Institute, Belgium, 2010.<br />
[29] N. MARCHAL. "Design, Implémentation et Test de l'Architecture du Système de<br />
Télécommunication du CubeSat <strong>OUFTI</strong>-1 ". <strong>Master</strong> thesis, GRAMME Institute, Belgium,<br />
2010.<br />
[30] A. KALMAN. "Midplane Stando Kit ". Pumpkin Inc., San Francisco, United<br />
States, 2008.<br />
[31] T. KOIZUMI et al. "Identication of the Center-of-Gravity and Inertia Terms of<br />
3-Dimensional Body". Department of Engineering, Doshisha University, Japan, 2006.<br />
[32] "Dassault Systemes - Catia Website ". http://www.3ds.com/products/catia/welcome/.<br />
[33] N. FRANCOIS. "Integration Procedure for the Engineering Model of <strong>OUFTI</strong>-1 ".<br />
Technical Report, University of Liège, Belgium, 2010.<br />
[34] "Samtech Website". http://www.samcef.com/page.aspid=3&langue=EN<br />
[35] J.-Ph. NOEL. "Thermal Issues Settlement and Test Procedure Investigation of<br />
<strong>OUFTI</strong>-1 Nanosatellite". <strong>Master</strong> thesis, University of Liège, Belgium, 2010.<br />
[36] "Kokam Catalog". http://kokamamerica.com/kokam_catalog.pdf.<br />
[37] J. PEDERSEN. "Vega's CubeSats Design Specication ". Workshop on the Verication<br />
of the CubeSats for the Vega Maiden Flight, ESA-ESTEC, Noordwijk, The Netherlands,<br />
2010.<br />
[38] M. ASHBY. "Materials Selection in Mechanical Design ". Butterworth-Heinemann,<br />
1999.<br />
[39] J. LECOMTE-BECKERS. "Materials Selection". LTAS, University of Liège, Belgium,<br />
2009.<br />
127