[1] Huang, H., “Developing Next-Generation Aerospace Innovatiove Talents through Space Cooperation, ’APSCO 9th International Symposium on, November 2018.
[2] Sidi, M., Spacecraft Dynamics & Control, a Practical Engineering Approach, Cambridge University Press, 1997.
[3] Tudor, Z., Design and Implementation of Attitude Control for 3-Axis Magnetic Coil Stabilization of a Spacecraft, (M.SC. Thesis), Norwegian University of Science and Technology, Institutt for teknisk kybernetikk, 2011.
[4] Ofodile, I., Ch., Design and Comparison of Attitude Control Modes for ESTCube-2,(M.Sc. Thesis) University of Tartu, 2017.
[5] Miri Roknabadi, S.H., Mirshams M. and Nikkhah A.A., “Spacecraft Optimal Attitude Control By Means of Reaction Wheels,” Journal of Space Science And Technology (Jsst), Winter 2010.
[6] Li, J., Post, M., Wright, T., & Lee, R., "Design of Attitude Control Systems for CubesSat-Class Nanosatellite" Journal of Control Science and Engineering, 2013, https://doi.org/ 10.1155/ 2013/ 657182
[7] Daniel, M. Torczynski and Amini, R., Magnetorquer Based Attitude Control for a Nanosatellite Testplatform, Delft University of Technology, Delft, 2629 GZ, The Netherlands, 2010.
[8] Saghari, A., Mirshams, M., Jafarsalehi, A., “Comprehensive Code of Remote Sensing Satellite Conceptual Design”, Journal of Space Science and Technology (Jsst), Summer 2014.
[9] Fritz, M., Shoer, J., Singh, L., Henderson, T., McGee, J., Rose, R., & Ruf, C. (2015). Attitude determination and control system design for the CYGNSS microsatellite. 2015 IEEE Aerospace Conference, 2015, pp. 1–12.
[10] Junaid, M. The Development of a Hardware-in-the-Loop Platform for the Attitude Determination and Control Testing of a Small Satellite, (Thesis), December 2015.
[11] APSCO Small Student Satellite (SSS) Technical report, K.N.Toosi University of Technology, 2018
[12] Sajjad, N., Design and Implementation of Control Modes for Student Micro Satellite,(M. Sc. Thesis), Faculty of Aerospace Engineering, K. N. Toosi University of Technology, Summer 2019.
[13] Quadrino, M., Kathleen, Prof D. Miller and Prof K. Cahoy. "Testing the Attitude Determination and Control of a CubeSat with Hardware-in-the-Loop." Massachusetts institute of technology space systems laboratory, 2014.
[14] Mirshams, M. and et al., “Using Air-Bearing Based Platform and Cold Gas Thruster Actuator For Satellite Attitude Dynamics Simulation,” Modares Mechanical Engineering, Vol. 14, No. 12, 2015, pp. 1-12.
[15] Taei, H., Mirshams, M., Ghobadi, M., Vahid D., M., Haghi, H., "Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels," Journal of Space Science and Technology (JSST), Vol. 8, No. 4, 2016, pp. 35-44.
[16] Bohlouri, V., Haghighi, H., Kaviri, S., Taghinezhad, M., maani, E., Seyedzamani, S., "Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control," Journal of Space Science and Technology (JSST), Vol. 12, No. 2, 2019, pp. 55-70.
