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Syed Tauqeer ul Islam Rizvi
Syed Tauqeer ul Islam Rizvi
College of Aeronautical Engineering, NUST, Pakistan
Verified email at cae.nust.edu.pk
Title
Cited by
Cited by
Year
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
532021
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
312015
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
282021
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
192021
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
182015
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
162020
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
152017
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
112021
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
62021
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
42022
Integrated CLOS and PN Guidance for Increased Effectiveness of Surface to Air Missiles.
BFT Zahra, SIA SHAH
INCAS Bulletin 9 (2), 2017
42017
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
32020
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
22023
A review of UAV platforms for autonomous applications: comprehensive analysis and future directions
MA Tahir, I Mir, TU Islam
IEEE Access, 2023
22023
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
12012
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
12012
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
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Articles 1–20