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   journal of aerospace science and technology   
سال:2024 - دوره:17 - شماره:2


  tick  active vibration control and improving flutter characteristics of uav wing by using piezoelectric material - صفحه:73-91

  tick  advancing flexible rope motion measurement in aerospace: vision-based innovations for enhanced accuracy and efficiency through edge segmentation - صفحه:1-15

  tick  aeroelastic instability analysis of a wing equipped with a conventional aerodynamic control surface - صفحه:137-144

  tick  analysing the effect of helicopter pilot cushion on body vibrations through numerical and analytical investigation - صفحه:16-25

  tick  experimental assessment of the airflow-induced vibration of a single cylinder with a cantilever beam - صفحه:92-109

  tick  experimental investigation of flow interference between four circular cylinders - صفحه:57-72

  tick  intelligent control of a tailsitter uav during transition flight: a feedback linearization approach - صفحه:38-46

  tick  investigation of effective parameters on graphite distribution in fgm structure of a356/al2o3/gr composite - صفحه:27-36

  tick  jaya-based optimal type-2 fuzzy sliding mode controller design for a cylindrical robotic arm - صفحه:146-161

  tick  precise dynamic modeling and super-twisting sliding mode control for an articulated aerial robot in capturing process - صفحه:47-56

  tick  prediction of earth orientation parameters using a hybrid attention-based cnn-gru model with a coordinate transformation approach - صفحه:125-136

  tick  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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