| Trajectory optimization of hypersonic vehicle using gauss pseudospectral method R Tawfiqur, H Zhou, YZ Sheng, YM Younis, KN Zhang Applied Mechanics and Materials 110, 5232-5239, 2012 | 16 | 2012 |
| Bézier approximation based inverse dynamic guidance for entry glide trajectory T Rahman, Z Hao, C Wanchun 2013 9th Asian Control Conference (ASCC), 1-6, 2013 | 15 | 2013 |
| Pseudospectral Model Predictive Control for Exo-atmospheric Guidance T Rahman, H Zhou, L Yang, W Chen International Journal of Aeronautical and Space Sciences 16 (1), 2015 | 14 | 2015 |
| Small launch vehicle trajectory profile optimization using hybrid algorithm FM Villanueva, H Linshu, AF Rafique, T Rahman Proceedings of 2013 10th International Bhurban Conference on Applied …, 2013 | 12 | 2013 |
| Impact angle and impact velocity constrained terminal guidance for stationary target H Zhou, T Rahman, W Chen Aircraft Engineering and Aerospace Technology: An International Journal 87 …, 2015 | 10 | 2015 |
| Applications of AUSM+ scheme on subsonic, supersonic and hypersonic flows fields MY Younis, MA Sohail, T Rahman, Z Muhammad, SR Bakaul World Academy Of Science, Engineering and Technology, 2011 | 9 | 2011 |
| Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight Z Hao, T Rahman, C Wanchun thescientificworldjournal, 2014 | 7 | 2014 |
| Onboard pseudospectral guidance for re-entry vehicle H Zhou, T Rahman, D Wang, W Chen Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2014 | 4 | 2014 |
| Rapid Entry Trajectories Generation with Multi-Constraints for CAV Z Hao, L Jiafeng, C Wanchun, T Rahman 3rd IEEE International Conference on Computer Science and Automation Engineering, 2013 | 2 | 2013 |
| Waypoints Following Guidance for Surface-to-Surface Missiles H Zhou, EM Khalil, T Rahman, W Chen International Journal of Aeronautical & Space Sciences, 1-13, 2018 | 1 | 2018 |
| Trajectory optimization study of a lifting body re-entry vehicle for medium to intermediate range applications STI Rizvi, H Linshu, T ur Rehman, AF Rafique AIP Conference Proceedings 1493 (1), 782-789, 2012 | 1 | 2012 |
| Optimal Trajectory Study of a Small Size Waverider and Wing-Body Reentry Vehicle at Suborbital Entry Speed of Approximately 4 km/s with Dynamic Pressure and Heat Rate Constraint S Tauqeer Ul Islam Rizvi, H Linshu, T Rahman AUT Journal of Modeling and Simulation 44 (2), 29-36, 2012 | 1 | 2012 |
| Higher order low dissipative scheme Limiters Comparison for Hypersonic Blunt Cone MA Sohail, MY Younis, T Rahman, Z Muhammad, ZN Tun The Proceedings of 2010 Asia-Pacific International Symposium on Aerospace …, 2010 | | 2010 |
| Inviscid and Viscous Computation on Aerodynamic Characteristics of A Conventional Projectile MA Sohail, T Rahman, MY Younis, ZN Tun, Z Muhammad, Z Maqbool The Proceedings of 2010 Asia-Pacific International Symposium on Aerospace …, 2010 | | 2010 |
| High Resolution, High Order, Low Dissipative Numerical scheme for hypersonic Flows MY Younis, T Rahman, MA Sohail, Z Muhammad, ZN Tun The Proceedings of 2010 Asia-Pacific International Symposium on Aerospace …, 2010 | | 2010 |
| Applications of Higher Order Low Dissipative Scheme on Hypersonic Configurations MA Sohail, MY Younis, T Rahman, Z Muhammad | | |
| Computation of drag over Launch vehicle Fairing Configurations by using viscous modeling ZN Tun, T Rahman, Z Maqbool, M Afzal, Z Muhammad | | |
Amer Farhan RafiqueAerospace Engineering Department, King Abdulaziz University, Jeddah, Saudi Arabia在 kau.edu.sa 的电子邮件经过验证
Amer Farhan RafiqueAerospace Engineering Department, King Abdulaziz University, Jeddah, Saudi Arabia在 kau.edu.sa 的电子邮件经过验证
Liang YangUniversity of California San Diego在 ucsd.edu 的电子邮件经过验证