Mardani, M. & Mobed, M. (2007). FINDING OPTIMAL SATELLITE LAUNCH TRAJECTORIES USING THE LINEAR TANGENT GUIDANCE LAW. Sharif Journal of Mechanical Engineering, 23(No . 38), 75-80.
MLA
Mardani, M., & Mobed, M. "FINDING OPTIMAL SATELLITE LAUNCH TRAJECTORIES USING THE LINEAR TANGENT GUIDANCE LAW", Sharif Journal of Mechanical Engineering, 23, No . 38, 2007, 75-80.
HARVARD
Mardani M., Mobed M. (2007). 'FINDING OPTIMAL SATELLITE LAUNCH TRAJECTORIES USING THE LINEAR TANGENT GUIDANCE LAW', Sharif Journal of Mechanical Engineering, 23(No . 38), pp. 75-80.
CHICAGO
M. Mardani & M. Mobed, "FINDING OPTIMAL SATELLITE LAUNCH TRAJECTORIES USING THE LINEAR TANGENT GUIDANCE LAW," Sharif Journal of Mechanical Engineering, 23 No . 38 (2007): 75-80,
VANCOUVER
Mardani M., Mobed M. FINDING OPTIMAL SATELLITE LAUNCH TRAJECTORIES USING THE LINEAR TANGENT GUIDANCE LAW. Sharif Journal of Mechanical Engineering. 2007;23(No . 38):75-80 (In Persian).
