Item Details

Print View

Simulator Evaluation of the Effects of Reduced Spoiler and Thrust Authority on a Decoupled Longitudinal Control System During Landings in Wind Shear

G. Kimball Miller, Jr.
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:83188
Description
48 p. : ill. ; 28 cm.
Notes
  • "Langley Research Center."
  • "October 1981"--Cover.
  • Subject Category 08.
  • Inncludes bibliographical references.
Series Statement
NASA technical memorandum 83188
Technical Details
  • Access in Virgo Classic
  • Staff View

    LEADER 01516cam a2200373 a 4500
    001 u1491471
    003 SIRSI
    008 821020s1981 dcua b f00010 eng d
    035
      
      
    a| (Sirsi) o08882759
    035
      
      
    a| (OCoLC)08882759
    035
      
      
    a| (GPO)82028820
    035
      
      
    a| (OCoLC)8882759
    040
      
      
    a| GPO c| GPO
    049
      
      
    a| VA@D
    074
      
      
    a| 830-D (microfiche)
    086
    0
      
    a| NAS 1.15:83188
    100
    1
      
    a| Miller, G. Kimball.
    245
    1
    0
    a| Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear / c| G. Kimball Miller, Jr.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration, Scientific and Technical Information Branch ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1981.
    300
      
      
    a| 48 p. : b| ill. ; c| 28 cm.
    440
      
    0
    a| NASA technical memorandum v| 83188
    500
      
      
    a| "Langley Research Center."
    500
      
      
    a| "October 1981"--Cover.
    500
      
      
    a| Subject Category 08.
    504
      
      
    a| Inncludes bibliographical references.
    596
      
      
    a| 2
    650
      
    0
    a| Stability of airplanes, Longitudinal.
    650
      
    0
    a| Airplanes x| Control systems.
    650
      
    0
    a| Vertical wind shear.
    710
    1
      
    a| United States. b| National Aeronautics and Space Administration. b| Scientific and Technical Information Branch.
    710
    2
      
    a| Langley Research Center.
    999
      
      
    a| NAS 1.15:83188 w| SUDOC i| 1491471-1001 l| 3EAST m| ALDERMAN t| MICROFICHE
▾See more
▴See less

Availability

Google Preview

Google Books Preview
Library Location Map Availability Call Number
Alderman 3rd Floor East Reading Room N/A Available Non-Circ.