[1] Kaplan, M.H., Modern spacecraft dynamics & control, 1st Ed., John Wiley & Sons, New York, 1976.
[2] Markley, F.L., Fundamentals of Spacecraft Attitude Determination and control, 1st Ed., Springer, New York, 2014.
[3] Brown, C.D., Elements of Space Design, 1st Ed., American Institute of Aeronautics and Astronautics, Virginia, 2002.
[4] Yang, Y., “Spacecraft attitude and reaction wheel desaturation combined,” Journal of Control Method, Vol.11, 2016, pp. 54-59.
[5] Borissov, S., Wu, Y. andMortari, D., “East–West GEO satellite station-keeping with degraded thruster Response,” Journal of Aerospace, Vol. 2, 2015, pp. 581-601.
[6] Kosari, A., Kaviri, S.,Moshiri, B. and Fakoor, M., “Design of optimal thruster configuration for attitude control of geostationary satellite,” Journal of Modares Mechanical Engineering, Vol.13, 2014, pp.67-77.
[7] Cassady, R.J., Meckel, N.J., Hoskins, W.A. and McGuire, M.L., “Pulsed Plasma Thruster Systems for Spacecraft Attitude Control,” ocobr 2014.
[8] Sabgatullahi, F., vertical flight aircraft, patent number 48464, country's documents and real estate registration organization, general department of industrial property, patent registration, Tehran, Iran, 2009 (In Persian).
[9] Chung, S.J., “Propellant free control of tethered formation flight,” Journal of guidance control and dynamics, Vol.31, 2008, pp. 390-400.
[10] Pourtakdoust, S. H. andJalali, M. A., “Thrust-Limited optimal Three-Dimensional spacecraft trajectories,” Journal of American Institute of Aeronautics and Astronautics, Vol. 14, 2000, pp.81-89.
[11] Martinsfilho, L. S. and Santana, A,. “Optimal On-Off Attitude Control for the Brazilian Multimission Platform Satellite,” Journal of Mathematical Problems in Engineering, Vol.17, 2009, pp.55-68.
[12] Sidi, M.J., Spacecraft dynamics & control a practical engineering approach, 1st Ed., Press Syndicate of the University of Cambridge, New York, 1997.
)