Novel implementation of multi-robot space exploration utilizing coordinated multi-robot exploration and frequency modified whale optimization algorithm F Gul, I Mir, W Rahiman, TU Islam IEEE Access 9, 22774-22787, 2021 | 53 | 2021 |
Optimal trajectory analysis of hypersonic boost-glide waverider with heat load constraint H Linshu, X Dajun Aircraft Engineering and Aerospace Technology: An International Journal 87 …, 2015 | 31 | 2015 |
A stability perspective of bioinspired unmanned aerial vehicles performing optimal dynamic soaring I Mir, SA Eisa, H Taha, A Maqsood, S Akhtar, TU Islam Bioinspiration & Biomimetics 16 (6), 066010, 2021 | 28 | 2021 |
A stability perspective of bio-inspired UAVs performing dynamic soaring optimally I Mir, SA Eisa, H Taha, A Maqsood, S Akhtar, TU Islam Bioinspir. Biomim, 2021 | 19 | 2021 |
Optimal trajectory and heat load analysis of different shape lifting reentry vehicles for medium range application L He, D Xu Defence Technology 11 (4), 350-361, 2015 | 18 | 2015 |
Design and fabrication of solar thermal energy storage system using potash alum as a pcm MS Malik, N Iftikhar, A Wadood, MO Khan, MU Asghar, S Khan, ... Energies 13 (23), 6169, 2020 | 16 | 2020 |
Trajectory optimisation for a rocket-assisted hypersonic boost-glide vehicle STI Rizvi, H Linshu, X Dajun, SIA Shah The Aeronautical Journal 121 (1238), 469-487, 2017 | 15 | 2017 |
A semi-analytical approach for flutter analysis of a high-aspect-ratio wing RF Latif, MKA Khan, A Javed, SIA Shah, STI Rizvi The Aeronautical Journal 125 (1284), 410-429, 2021 | 11 | 2021 |
Comprehensive design of an oleo-pneumatic nose landing gear strut MA Ahmad, SIA Shah, TA Shams, A Javed, STI Rizvi Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2021 | 6 | 2021 |
Selection methodology of composite material for retractable main landing gear strut of a lightweight aircraft MA Ahmad, H Rafiq, SIA Shah, SA Khan, STI Rizvi, TA Shams Applied Sciences 12 (11), 5689, 2022 | 4 | 2022 |
Integrated CLOS and PN Guidance for Increased Effectiveness of Surface to Air Missiles. BFT Zahra, SIA SHAH INCAS Bulletin 9 (2), 2017 | 4 | 2017 |
Selection methodology of an electric actuator for nose landing gear of a light weight aircraft TA Shams, SIA Shah, MA Ahmad, K Mehmood, W Ahmad, STI Rizvi Applied Sciences 10 (23), 8730, 2020 | 3 | 2020 |
Control Algorithms, Kalman Estimation and Near Actual Simulation for UAVs: State of Art Perspective MA Tahir, I Mir, TU Islam Drones 7 (6), 339, 2023 | 2 | 2023 |
A review of UAV platforms for autonomous applications: comprehensive analysis and future directions MA Tahir, I Mir, TU Islam IEEE Access, 2023 | 2 | 2023 |
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 |
Experimental Investigation of Wing Rock on a Low Aspect Ratio Flying Wing Micro Aerial Vehicle using Pyramidal Balance TA Shams, S Irtiza Ali Shah, M Ayaz Ahmad, A Shahzad, ... AIAA SCITECH 2023 Forum, 0814, 2023 | | 2023 |
Semi-Analytical Flutter Analysis of a Light UAV Wing RF Latif, STI Rizvi, A Javed, SIA Shah 2020 17th International Bhurban Conference on Applied Sciences and …, 2020 | | 2020 |
Numerical Performance Study of Small Size Lifting-Body Reentry Vehicle STI Rizvi, LS He, DJ Xu Applied Mechanics and Materials 390, 161-165, 2013 | | 2013 |
Design of a Traverse Gear System for an Environmental Wind Tunnel S Rizvi University of Manchester, 1997 | | 1997 |