Item Details

Flight-Determined Subsonic Longitudinal Stability and Control Derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) With Thrust Vectoring [microform]

Kenneth W. Iliff, Kon-Sheng Charles Wang
Format
Book; Government Document; Microform
Published
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
Language
English
Variant Title
Flight determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:206539
Description
1 v.
Notes
Shipping list no.: 99-0723-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.
Series Statement
[NASA technical paper] ; NASA/TP-97-206539
NASA technical paper 206539
Technical Details
  • Access in Virgo Classic

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    a| Flight determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
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    a| Edwards, Calif. : b| National Aeronautics and Space Administration, Dryden Flight Research Center ; a| [Springfield, Va. : b| National Technical Information Service, distributor, c| 1997]
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    a| Longitudinal stability. 2| nasat
    650
      
    7
    a| Thrust vector control. 2| nasat
    650
      
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    a| Research vehicles. 2| nasat
    650
      
    7
    a| Maximum likelihood estimates. 2| nasat
    650
      
    7
    a| Parameter identification. 2| nasat
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    7
    a| Angle of attack. 2| nasat
    650
      
    7
    a| Unsteady aerodynamics. 2| nasat
    650
      
    7
    a| Aircraft control. 2| nasat
    650
      
    7
    a| Flight tests. 2| nasat
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    a| Wang, Kon-Sheng Charles.
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