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Source: The Open Library

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1X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data

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“X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data” Metadata:

  • Title: ➤  X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
  • Author:
  • Language: English
  • Number of Pages: Median: 35
  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center - National Aeronautics and Space Administration - National Technical Information Service, distributor]
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C] - Washington, D.C - [Springfield, Va - [Washington, D.C.]

“X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1996
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Access

Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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    2Ground-to-flight handling qualities comparisons for a high performance airplane

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    “Ground-to-flight handling qualities comparisons for a high performance airplane” Metadata:

    • Title: ➤  Ground-to-flight handling qualities comparisons for a high performance airplane
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics
    • Publish Date:
    • Publish Location: ➤  Springfield, Va - Washington, D.C

    “Ground-to-flight handling qualities comparisons for a high performance airplane” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1995
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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      3Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)

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      “Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)” Metadata:

      • Title: ➤  Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)
      • Author:
      • Language: English
      • Number of Pages: Median: 32
      • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

      “Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1990
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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        4F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness

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        “F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness” Metadata:

        • Title: ➤  F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: Hampton, Va - [Springfield, Va

        “F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1995
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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          5Performance validation of the ANSER control laws for the F-18 HARV

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          “Performance validation of the ANSER control laws for the F-18 HARV” Metadata:

          • Title: ➤  Performance validation of the ANSER control laws for the F-18 HARV
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
          • Publish Date:
          • Publish Location: Hampton, Va - [Springfield, Va

          “Performance validation of the ANSER control laws for the F-18 HARV” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1995
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Access

          Downloads Are Not Available:

          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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            6Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers

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            “Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers” Metadata:

            • Title: ➤  Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

            “Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1996
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

            Downloads Are Not Available:

            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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              7Fuzzy logic decoupled lateral control for general aviation airplanes

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              “Fuzzy logic decoupled lateral control for general aviation airplanes” Metadata:

              • Title: ➤  Fuzzy logic decoupled lateral control for general aviation airplanes
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: Hampton, Va - [Springfield, Va

              “Fuzzy logic decoupled lateral control for general aviation airplanes” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1997
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                8Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport

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                “Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport” Metadata:

                • Title: ➤  Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
                • Publish Date:
                • Publish Location: ➤  Springfield, VA - Hampton, Va - Hanover, MD

                “Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 2000
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

                Downloads Are Not Available:

                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                  9Investigation of interactions between limb-manipulator dynamics and effective vehicle roll control characteristics

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                  “Investigation of interactions between limb-manipulator dynamics and effective vehicle roll control characteristics” Metadata:

                  • Title: ➤  Investigation of interactions between limb-manipulator dynamics and effective vehicle roll control characteristics
                  • Author:
                  • Number of Pages: Median: 57
                  • Publisher: Ames Research Center
                  • Publish Date:
                  • Publish Location: Edwards, Calif

                  “Investigation of interactions between limb-manipulator dynamics and effective vehicle roll control characteristics” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1986
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

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                  10Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method

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                  “Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method” Metadata:

                  • Title: ➤  Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - West Virginia University
                  • Publish Date:
                  • Publish Location: ➤  Morgantown, WV - [Washington, DC - Springfield, Va

                  “Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1995
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Access

                  Downloads Are Not Available:

                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                    11Relative control effectiveness technique with application to airplane control coordination

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                    “Relative control effectiveness technique with application to airplane control coordination” Metadata:

                    • Title: ➤  Relative control effectiveness technique with application to airplane control coordination
                    • Author:
                    • Language: English
                    • Publisher: ➤  For sale by the National Technical Information Service,] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                    • Publish Date:
                    • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                    “Relative control effectiveness technique with application to airplane control coordination” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1985
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

                    Online Access

                    Downloads Are Not Available:

                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                      12Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight

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                      “Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight” Metadata:

                      • Title: ➤  Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering
                      • Publish Date:
                      • Publish Location: ➤  Boca Raton, FL - Springfield, Va - [Washington, DC

                      “Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1996
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

                      Online Access

                      Downloads Are Not Available:

                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                        13Reynolds number effects on the performance of lateral control devices

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                        “Reynolds number effects on the performance of lateral control devices” Metadata:

                        • Title: ➤  Reynolds number effects on the performance of lateral control devices
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                        • Publish Date:
                        • Publish Location: Hampton, Va - Springfield, VA

                        “Reynolds number effects on the performance of lateral control devices” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 2000
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Access

                        Downloads Are Not Available:

                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                          14Two blowing concepts for roll and lateral control of aircraft

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                          “Two blowing concepts for roll and lateral control of aircraft” Metadata:

                          • Title: ➤  Two blowing concepts for roll and lateral control of aircraft
                          • Author:
                          • Number of Pages: Median: 102
                          • Publisher: ➤  Dept. of Aeronautics and Astronautics, Stanford University
                          • Publish Date:
                          • Publish Location: Stanford, Calif

                          “Two blowing concepts for roll and lateral control of aircraft” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1986
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          15V/STOL dynamics, control, and flying qualities

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                          “V/STOL dynamics, control, and flying qualities” Metadata:

                          • Title: ➤  V/STOL dynamics, control, and flying qualities
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - Available from NASA Center for AeroSpace Information
                          • Publish Date:
                          • Publish Location: ➤  Hanover, MD - Moffett Field, Calif

                          “V/STOL dynamics, control, and flying qualities” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 2000
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

                          Online Access

                          Downloads Are Not Available:

                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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