[1] Berner, R., “Control Moment Gyro Actuator for Small Satellite Application,” )M. Sc. Thesis), Department of Electrical and Electronic Engineering, University of Stellenbosch, 2005.
[2] Jacot, A.D. and Liska, D.J., “Control Moment Gyros in Attitude Control,” Journal of Spacecrafts and Rockets, Vol. 3., 1966, pp. 1313-1320.
[3] Margulies, G. and Aubrun, J.N., “Geometrical Theory of Single Gimbal Control Moment Gyro System,” Journal of the Astronautical Sciences, Vol. XXVI, No.2, 1978, pp.159-191.
[4] Bedrossian, N.S. and et. al., “Redundant Single Gimbal Control Moment Gyroscope Singularity Analysis,” Journal of Guidance, Vol. 13, No. 6, 1990.
[5] Bedrossian, N.S. and et. al., “Steering Law Design For Redundant Single Gimbal Control Moment Gyroscopes,” Journal of Guidance, Control, and Dynamics, Vol. 13, No.6, 1990, pp. 1083-1089.
[6] Vadali, S. R. and et. al., “Preferred Gimbal Angles for Single Gimbal Control Moment Gyroscopes,” Journal of Guidance, Control and Dynamics, Vol. 13, No. 6, 1990, pp. 1090-1095.
[7] Oh, H.S. and Vadali, S.R., “Feedback Control and Steering Laws forSpacecraft Using Single Gimbal Control Moment Gyros,” Journal of the Astronautical Sciences, Vol. 39, No. 2, 1991, pp. 183-203.
[8] Meffe, G. and Stocking, M., “Momentum Envelope Topology of Single Gimbal CMG Arrays for Space Vehicle Control,” Proceedings of AAS Guidance and Control Conference, Keystone, CO, 1987.
[9] Kurokawa, H. “Constrained Steering Law of Pyramid-Type Control Moment Gyros and Ground Tests,” Journal of Guidance, Control, and Dynamics, Vol. 20, No. 3, 1997, pp. 445-449.
[10] Wie, B. and et. al., “Singularity Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros,” Journal of Guidance, Control and Dynamics, Vol. 24, No. 5, 2001, pp. 865-871.
[11] Lappas, V. J. and et. al., “Attitude Control for Small Satellites Using Control Moment Gyros,” 52nd IAF, 2001.
[12] Tekinalp, O. and Yavuzoglu, E., “A New Steering Law for Redundant Control Moment Gyroscope Cluster,” Journal of Aerospace Science and Technology, Vol. 9, No. 7, 2005, pp. 626-634,.
[13] Kown, S. W. and et. al., “Fixed-Star Tracking Attitude Control of Spacecraft Using Single-Gimbal Control Moment Gyros,” American Journal of Engineering and Applied Sciences, 2010.
[14] Harland, D.M. and Lorenz, R.D., Space Systems Failures, Springer-Praxis, 2005.
[15] KrishnaKumar, K., “Adaptive Neuro-Control for Spacecraft Attitude Control,” Proceedings of the Third IEEE Conference, Aug. 1994.
[17] Makunis, W., “Adaptive Satellite Attitude Control in the Presense of Inertia And CMG Gimbal Friction Uncertainties,” Journal of the Astronautical Sciences, Vol. 56, No. 1, 2008, pp. 121–134.
[18] Aghalari, A., Faghihinia, A., “PD and Feedback Quaternion Control Strategy for Attitude Control of a Satellite Equipped with Four Single Gimbal Control Moment Gyro,” 10th Iranian Aerospace Society Conference, TarbiatModarres University, 1389, (In Persian).
[19] Aghalari, A., Kalhor, A., Dehghan, S. M. and Abedian, A., “Designing, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite,” Jorunal of Space Science and Technology (JSST), Vol. 2, No. 3, p.p.13-23, 1388, (In Persian).
[20] Aghalari, A., Study on Satellite Simulators, Designing and Fabrication of A Single Gimbal Control Moment Gyro for Simulator, Technical Report, Aerospace University Complex, 1389, (In Persian).
[21] Kalhor, A., Cheheltani, S. H., Designing and Integration of Electronics and Computer Parts of Satellite Simulator With Single Gimbal Control Moment Gyros, Technical Report, Aerospace University Complex, 1390, (In Persian).
[22] Aghalari, A., Kalhor, A., Dehghan, S. M., and Cheheltani, S. H., “Design, Manufacturing and Test of a Three-Degree-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros,” Jorunal of Space Science and Technology (JSST), Vol. 7, No. 3, 1393, pp. 51-67, (In Persian).
[23] Available, [on line]: http://www. Microstrain. com, Access Date, 2010.
[24] Nakamura, Y., Hanafusa, H., “Inverse Kinematic Solutions with Singularity Robustness for Robot Manipulator Control,” Journal of Dynamic Systems, Measurement, and Control, Vol. 108, Vol. 3, 1986, pp.163-171.
[25] Wie, B., Lu, J., “Feedback Control Logic for Spacecraft Eigenaxis Rotations Under Slow Rate And Control Constraints,” Guidance, Navigation, and Control Conference, Guidance, Navigation, and Control and Co-Located Conferences, Vol. 18, No. 6, 1995.
