Information Journal Paper
APA:
CopyMARDANI, M., & MOUBED, M.. (2007). FINDING OPTIMAL SATELLITE LAUNCH TRAJECTORIES USING THE LINEAR TANGENT GUIDANCE LAW. INDUSTRIAL ENGINEERING & MANAGEMENT SHARIF (SHARIF: ENGINEERING), 23(38), 75-80. SID. https://sid.ir/paper/107755/en
Vancouver:
CopyMARDANI M., MOUBED M.. FINDING OPTIMAL SATELLITE LAUNCH TRAJECTORIES USING THE LINEAR TANGENT GUIDANCE LAW. INDUSTRIAL ENGINEERING & MANAGEMENT SHARIF (SHARIF: ENGINEERING)[Internet]. 2007;23(38):75-80. Available from: https://sid.ir/paper/107755/en
IEEE:
CopyM. MARDANI, and M. MOUBED, “FINDING OPTIMAL SATELLITE LAUNCH TRAJECTORIES USING THE LINEAR TANGENT GUIDANCE LAW,” INDUSTRIAL ENGINEERING & MANAGEMENT SHARIF (SHARIF: ENGINEERING), vol. 23, no. 38, pp. 75–80, 2007, [Online]. Available: https://sid.ir/paper/107755/en