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"DTIC ADA520301: Neural-Network-Based Modeling Of Rotorcraft Vibration For Real-Time Applications" and the language of the book is English.


“DTIC ADA520301: Neural-Network-Based Modeling Of Rotorcraft Vibration For Real-Time Applications” Metadata:

  • Title: ➤  DTIC ADA520301: Neural-Network-Based Modeling Of Rotorcraft Vibration For Real-Time Applications
  • Author: ➤  
  • Language: English

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  • Internet Archive ID: DTIC_ADA520301

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"DTIC ADA520301: Neural-Network-Based Modeling Of Rotorcraft Vibration For Real-Time Applications" Description:

The Internet Archive:

The overall objective of this ongoing effort is to provide the capability to model and simulate rotorcraft aeromechanics behaviors in real-time. This would be accomplished by the addition of an aeromechanics element to an existing high-fidelity, real-time helicopter flight simulation. As a first step, the peak vertical vibration at the pilot floor location was considered in this neural-network-based study. The flight conditions considered were level flights, rolls, pushovers, pull-ups, autorotations, and landing flares. The NASA/Army UH-60A Airloads Program flight test database was the source of raw data. The present neural network training databases were created in a physically consistent manner. Two modeling approaches, with different physical assumptions, were considered. The first approach involved a maneuver load factor that was derived using the roll-angle and the pitch-rate. The second approach involved the three pilot control stick positions. The resulting, trained back-propagation neural networks were small, implying rapid execution. The present neural-network-based approach involving the peak pilot vibration was utilized in a quasi-static manner to simulate an extreme, time-varying pull-up maneuver. For the above pull-up maneuver, the maneuver load factor approach was better for real-time simulation, i.e., produced greater fidelity, as compared to the control stick positions approach. Thus, neural networks show promise for use in high-fidelity, real-time modeling of rotorcraft vibration.

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  • Source: Internet Archive
  • Internet Archive Link: Archive.org page
  • All Files are Available: Yes
  • Number of Files: 16
  • Number of Available Files: 16
  • Added Date: 2018-07-26 11:29:23
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