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Journal Of Aerospace Science And Technology
  
سال:2020 - دوره:13 - شماره:1
  
 
Calculation Of Nonlinear Normal Modes Using Epfm Method
- صفحه:57-65
  
 
Designing A Fault-Tolerant Control System For The Boeing 747
- صفحه:1-9
  
 
Experimental Comparison Of Thrust Performance Of Two Low And Medium-Speed Motors By Wind Tunnels And Obtaining The Flight Time Of A Specific Drone
- صفحه:11-17
  
 
Experimental Investigation Of The Geometric Properties Of Different Rotor Blades For Controlling The Wingtip Vortex
- صفحه:89-98
  
 
Growth And Collapse Of A Cavitation Bubble Inside A Rigid Cylinder: Effect Of Membrane Tension
- صفحه:67-76
  
 
Modeling Of 9 Degrees Of Parafoil Freedom Through Transverse Displacement Of Cargo Weight
- صفحه:27-38
  
 
Neural Network Backstepping Control Of A Reentry Vehicle In The Presence Of Uncertainties
- صفحه:77-81
  
 
Numerical Investigation Of Aerodynamic Effects Of Geometry And Sensor Distance On A Spherical Projectile
- صفحه:39-47
  
 
Numerical Study Of Changes In Length-To- Diameter Ratio Of A Cylindrical Diffuser, Used In A Vacuum Test Stand
- صفحه:18-25
  
 
Optimal Flight Trajectory Planning Using Improved Evolutionary Method For Ucav Navigation In 3d Constrained Environments
- صفحه:83-89
  
 
Optimal Guidance Of A Reentry Vehicle Based On Online Trajectory Optimization
- صفحه:99-110
  
 
Simulation And Examination Of Flow Characteristics Of The Butterfly Valve
- صفحه:49-56
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