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
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.
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.
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.
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