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journal of aerospace science and technology
  
سال:2024 - دوره:17 - شماره:2
  
 
active vibration control and improving flutter characteristics of uav wing by using piezoelectric material
- صفحه:73-91
  
 
advancing flexible rope motion measurement in aerospace: vision-based innovations for enhanced accuracy and efficiency through edge segmentation
- صفحه:1-15
  
 
aeroelastic instability analysis of a wing equipped with a conventional aerodynamic control surface
- صفحه:137-144
  
 
analysing the effect of helicopter pilot cushion on body vibrations through numerical and analytical investigation
- صفحه:16-25
  
 
experimental assessment of the airflow-induced vibration of a single cylinder with a cantilever beam
- صفحه:92-109
  
 
experimental investigation of flow interference between four circular cylinders
- صفحه:57-72
  
 
intelligent control of a tailsitter uav during transition flight: a feedback linearization approach
- صفحه:38-46
  
 
investigation of effective parameters on graphite distribution in fgm structure of a356/al2o3/gr composite
- صفحه:27-36
  
 
jaya-based optimal type-2 fuzzy sliding mode controller design for a cylindrical robotic arm
- صفحه:146-161
  
 
precise dynamic modeling and super-twisting sliding mode control for an articulated aerial robot in capturing process
- صفحه:47-56
  
 
prediction of earth orientation parameters using a hybrid attention-based cnn-gru model with a coordinate transformation approach
- صفحه:125-136
  
 
the new hybrid meta-model by using doe and rsm for liquid propellant engine's feed system optimization
- صفحه:110-124
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