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Title: AIRCRAFT Download
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  • matlab
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  • [PDF]
  • File Size:
  • 1.48mb
  • Update:
  • 2016-04-18
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  • Uploaded by:
  • xqwendy
 Description: The establishment of a four-rotor aircraft hovering attitude dynamics model and simulation analysis, under the premise of open-loop control analyzes the impact of structural and elastic damping augmentation method for aircraft platform attitude qualitative and presents an open loop realization of stable hover control strategy.
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Four-rotor aircraft attitude stability analysis and modeling.pdf
    

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