Lurie BJ, Schier JA. Satellite attitude stabilization using fluid rings. Acta Mechanica. 2009;208(1-2):117-131. [
Link] [
DOI:10.1007/s00707-008-0132-5]
Tayebi J, Soleymani A. A comparative study of CMG and FMC actuators for nano satellite attitude control system-pyramidal configuration. 7th International Conference on Recent Advances in Space Technologies (RAST), 16-19 June, 2015, Istanbul, Turkey. Piscataway: IEEE; 2015. [
Link] [
DOI:10.1109/RAST.2015.7208370]
Kurokawa H. Survey of theory and steering laws of single-gimbal control moment gyros. Journal of Guidance, Control, and Dynamics. 2007;30(5):1331-1340. [
Link] [
DOI:10.2514/1.27316]
Jones LL, Zeledon RA, Peck MA. Generalized framework for linearly constrained control moment gyro steering. Journal of Guidance, Control, and Dynamics. 2012;35(4):1094-1103. [
Link] [
DOI:10.2514/1.56207]
Margulies G, Aubrun JN. Geometric theory of single-gimbal control moment gyro system. Journal of the Astronautical Sciences. 1978;26(2):159-191. [
Link]
Meng T, Matunaga S. Failure-tolerant control for small agile satellites using single-gimbal control moment gyros and magnetic torquers. Acta Mechanica Sinica. 2012;28(2):551-558. [
Link] [
DOI:10.1007/s10409-012-0044-4]
Tang L, Xu Sh. Geometric analysis of singularity for single- gimbal control moment gyro systems. Chinese Journal of Aeronautics.2005;18(4):295-303. [
Link] [
DOI:10.1016/S1000-9361(11)60248-3]
Jin L, Xu Sh. An improved constrained steering law for SGCMGs with DPC. Acta Mechanica Sinica.2009;25(5):713-720. [
Link] [
DOI:10.1007/s10409-009-0269-z]
Zhang JR, Rachid A, Zhang Y. Attitude control for part actuator failure of agile small satellite. Acta Mechanica Sinica. 2008;24(4):463-468. [
Link] [
DOI:10.1007/s10409-008-0153-2]
Jin L, Xu Sh. An improved constrained steering law for SGCMGs with DPC. Acta Mechanica Sinica. 2009;25(5):713-720. [
Link] [
DOI:10.1007/s10409-009-0269-z]
Jin L, Xu Sh. Fault tolerant attitude control for small satellites using single gimbal control moment gyros and magnetic torquers. Journal of Aerospace Engineering. 2014;28(3):401-407. [
Link]
Noumi A, Takahashi M, Kanzawa T, Haruki M. Fault-tolerant attitude control systems using multi-objective optimization for a spacecraft equipped with control moment gyros. AIAA Guidance, Navigation, and Control Conference, 5-9 January, 2015, Kissimmee, Florida. Reston: AIAA; 2015. [
Link] [
DOI:10.2514/6.2015-1088]
Akau RL, Behr VL, Whitaker R. Thermal design of the fast-on-orbit recording of transient events (FORTE) satellite. 8th Annual AIAA/USU, Conference on Small Satellites, 29 August-1 September, 1994, Utah, USA; 1994. [
Link]
Sozbir N, Bulut M, Oktem MF, Kahriman A, Chaix A. Design of thermal control subsystem for TUSAT telecommunication satellite. International Journal of Electrical, Computer, Energetic, Electronic and Communication Engineering. 2008;2(7):1384-1387. [
Link]
Cheng W, Liu N, Li Z, Zhong Q, Wang A, Zhang Z, et al. Application study of a correction method for a spacecraft thermal model with a Monte-Carlo hybrid algorithm. Chinese Science Bulletin. 2011;56(13):1407-1412. [
Link] [
DOI:10.1007/s11434-010-4053-z]
Gerhart Ch. University nanosat system thermal design, analysis, and testing. SPIE Defense & Security Symposium, 18-20 April, 2006, Orlando (Kissimmee), Florida, United States. Bellingham: SPIE; 2006. [
Link] [
DOI:10.1117/12.667770]
Chandrasekaran V, Subramanian ER. Transient thermal analysis of a nanosatellite in low earth orbit. Proceedings of 8th International Conference on Engineering Computational Technology, 4-7 September, 2012, Stirlingshire, UK. Stirlingshire: Civil-Comp Press; 2012. [
Link]
Nosratollahi M, Soleymani A, Sadati H. Design of satellite's combined attitude and thermal control system equipped with FMC actuators. Modares Mechanical Engineering. 2018;18(1):122-130. [Persian] [
Link]
Waswa PMB, Elliot M, Hoffman JA. Spacecraft Design-for-Demise implementation strategy & decision-making methodology for low earth orbit missions. Advances in Space Research. 2013;51(9):1627-1637. [
Link] [
DOI:10.1016/j.asr.2012.11.020]
Kreinovich V, Nguyen HT, Starks SA, Yam Y. Decision making based on satellite images: Optimal fuzzy clustering approach. Proceedings of the 37th IEEE Conference on Decision and Control, 18 December, 1998, Florida, USA. Piscataway: IEEE; 1998. [
Link] [
DOI:10.1109/CDC.1998.761970]
Wie B. Space vehicle dynamics and control. 2nd Edition. Reston: AIAA; 1998. pp. 305-320. [
Link]
Nobari NA, Misra AK. Attitude dynamics and control of satellites with fluid ring actuators. Journal of Guidance Control and Dynamics. 2012;35(6):1855-1864. [
Link] [
DOI:10.2514/1.54599]
Nobari NA, Misra AK. A hybrid attitude controller consisting of electromagnetic torque rods and an active fluid ring. Acta Astronautica. 2014;94(1):470-479. [
Link] [
DOI:10.1016/j.actaastro.2012.12.012]
Thunnissen DP, Tsuyuki GT. Margin determination in the design and development of a thermal control system. 34th International Conference on Environmental Systems (ICES), 19-22 July, 2004, Colorado Springs, Colorado, United States; 2004. [
Link] [
DOI:10.4271/2004-01-2416]
Bolduc C, Adourian C. Rapid thermal analysis of rigid three-dimensional bodies with the use of modelica physical modelling language. Proceedings of the 7th International Modelica Conference, 20-22 September, 2009, Como, Italy. Linköping: Linköping University Electronic Press; 2009. [
Link] [
DOI:10.3384/ecp09430036]
