Explore: Controllability

Discover books, insights, and more — all in one place.

Learn more about Controllability with top reads curated from trusted sources — all in one place.

Topic Search

Search for any topic

AI-Generated Overview About “controllability”:


Books Results

Source: The Open Library

The Open Library Search Results

Search results from The Open Library

1Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration

By

“Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” Metadata:

  • Title: ➤  Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Washington, DC

“Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” 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.

Online Borrowing:

    Online Marketplaces

    Find Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration at online marketplaces:


    2A theory for the roll-ratchet phenomenon in high performance aircraft

    By

    “A theory for the roll-ratchet phenomenon in high performance aircraft” Metadata:

    • Title: ➤  A theory for the roll-ratchet phenomenon in high performance aircraft
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: ➤  Springfield, Va - [Washington, DC

    “A theory for the roll-ratchet phenomenon in high performance aircraft” 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.

    Online Borrowing:

      Online Marketplaces

      Find A theory for the roll-ratchet phenomenon in high performance aircraft at online marketplaces:


      3Flight testing the X-36--the test pilot's perspective

      By

      “Flight testing the X-36--the test pilot's perspective” Metadata:

      • Title: ➤  Flight testing the X-36--the test pilot's perspective
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor]
      • Publish Date:
      • Publish Location: ➤  Edwards, Calif - [Springfield, Va

      “Flight testing the X-36--the test pilot's perspective” 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.

      Online Borrowing:

        Online Marketplaces

        Find Flight testing the X-36--the test pilot's perspective at online marketplaces:


        4Ground-to-flight handling qualities comparisons for a high performance airplane

        By

        “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.

        Online Borrowing:

          Online Marketplaces

          Find Ground-to-flight handling qualities comparisons for a high performance airplane at online marketplaces:


          5Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane

          By

          “Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane” Metadata:

          • Title: ➤  Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane
          • Author:
          • Language: English
          • Number of Pages: Median: 35
          • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office - Langley Research Center
          • Publish Date:
          • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va - Hampton, Va

          “Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1987
          • 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.

          Online Borrowing:

            Online Marketplaces

            Find Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane at online marketplaces:


            6"Wavefront analysis of adaptive telescope"

            By

            “"Wavefront analysis of adaptive telescope"” Metadata:

            • Title: ➤  "Wavefront analysis of adaptive telescope"
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - Universty of Alabama in Huntsville - National Technical Information Service, distributor - University of Alabama in Huntsville
            • Publish Date:
            • Publish Location: ➤  Springfield, Va - [Huntsville, Ala.] - [Washington, DC

            “"Wavefront analysis of adaptive telescope"” 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.

            Online Borrowing:

              Online Marketplaces

              Find "Wavefront analysis of adaptive telescope" at online marketplaces:


              7An investigation of nonlinear controller for propulsion controlled aircraft

              By

              “An investigation of nonlinear controller for propulsion controlled aircraft” Metadata:

              • Title: ➤  An investigation of nonlinear controller for propulsion controlled aircraft
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  [Washington, D.C - Ames, IA : Dept. of Aerospace Engineering and Engineering Mechanics, Iowa State University - Springfield, Va

              “An investigation of nonlinear controller for propulsion controlled aircraft” 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.

              Online Borrowing:

                Online Marketplaces

                Find An investigation of nonlinear controller for propulsion controlled aircraft at online marketplaces:


                8Handling qualities of unstable highly augmented aircraft

                By

                “Handling qualities of unstable highly augmented aircraft” Metadata:

                • Title: ➤  Handling qualities of unstable highly augmented aircraft
                • Author: ➤  
                • Language: English
                • Number of Pages: Median: 113
                • Publisher: AGARD
                • Publish Date:
                • Publish Location: ➤  Neuilly-sur-Seine - Neuilly sur Seine, France

                “Handling qualities of unstable highly augmented aircraft” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1991
                • 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.

                Online Borrowing:

                  Online Marketplaces

                  Find Handling qualities of unstable highly augmented aircraft at online marketplaces:


                  9Dynamics of flexible spacecraft

                  By

                  “Dynamics of flexible spacecraft” Metadata:

                  • Title: ➤  Dynamics of flexible spacecraft
                  • Author:
                  • Number of Pages: Median: 178
                  • Publisher: National Aerospace Laboratory
                  • Publish Date:
                  • Publish Location: Amsterdam

                  “Dynamics of flexible spacecraft” 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 Marketplaces

                  Find Dynamics of flexible spacecraft at online marketplaces:


                  10Supersonic flying qualities experience using the SR-71

                  By

                  “Supersonic flying qualities experience using the SR-71” Metadata:

                  • Title: ➤  Supersonic flying qualities experience using the SR-71
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                  • Publish Date:
                  • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                  “Supersonic flying qualities experience using the SR-71” 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.

                  Online Borrowing:

                    Online Marketplaces

                    Find Supersonic flying qualities experience using the SR-71 at online marketplaces:


                    11Cooperative control theory and integrated flight and propulsion control

                    By

                    “Cooperative control theory and integrated flight and propulsion control” Metadata:

                    • Title: ➤  Cooperative control theory and integrated flight and propulsion control
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - Dept. of Aerospace Engineering, University of Maryland - National Aeronautics and Space Administration
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - [Washington, DC - College Park, Md

                    “Cooperative control theory and integrated flight and propulsion control” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1994
                    • 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.

                    Online Borrowing:

                      Online Marketplaces

                      Find Cooperative control theory and integrated flight and propulsion control at online marketplaces:


                      12Robust, decoupled, flight control design with rate saturated actuators

                      By

                      “Robust, decoupled, flight control design with rate saturated actuators” Metadata:

                      • Title: ➤  Robust, decoupled, flight control design with rate saturated actuators
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                      • Publish Date:
                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                      “Robust, decoupled, flight control design with rate saturated actuators” 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.

                      Online Borrowing:

                        Online Marketplaces

                        Find Robust, decoupled, flight control design with rate saturated actuators at online marketplaces:


                        13Numerical solution of large Lyapunov equations

                        By

                        “Numerical solution of large Lyapunov equations” Metadata:

                        • Title: ➤  Numerical solution of large Lyapunov equations
                        • Author:
                        • Language: English
                        • Publisher: ➤  Research Institute for Advanced Computer Science, NASA Ames Research Center
                        • Publish Date:
                        • Publish Location: [Moffett Field, Calif.]

                        “Numerical solution of large Lyapunov equations” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1989
                        • 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.

                        Online Borrowing:

                          Online Marketplaces

                          Find Numerical solution of large Lyapunov equations at online marketplaces:


                          14Pilot-induced oscillation research

                          “Pilot-induced oscillation research” Metadata:

                          • Title: ➤  Pilot-induced oscillation research
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - NASA Center for AeroSpace Information (CASI)
                          • Publish Date:
                          • Publish Location: Edwards, Calif - Hanover, MD

                          “Pilot-induced oscillation research” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 2001
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

                          Online Marketplaces

                          Find Pilot-induced oscillation research at online marketplaces:


                          15Flight-time identification of a UH-60A helicopter and slung load

                          By

                          “Flight-time identification of a UH-60A helicopter and slung load” Metadata:

                          • Title: ➤  Flight-time identification of a UH-60A helicopter and slung load
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                          • Publish Date:
                          • Publish Location: ➤  Springfield, Va - Moffett Field, Calif

                          “Flight-time identification of a UH-60A helicopter and slung load” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1998
                          • 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.

                          Online Borrowing:

                            Online Marketplaces

                            Find Flight-time identification of a UH-60A helicopter and slung load at online marketplaces:


                            16Techniques for designing rotorcraft control systems

                            By

                            “Techniques for designing rotorcraft control systems” Metadata:

                            • Title: ➤  Techniques for designing rotorcraft control systems
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                            • Publish Date:
                            • Publish Location: ➤  Springfield, Va - [Washington, DC

                            “Techniques for designing rotorcraft control systems” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1994
                            • 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.

                            Online Borrowing:

                              Online Marketplaces

                              Find Techniques for designing rotorcraft control systems at online marketplaces:


                              17Impact of flying qualities on mission effectiveness for helicopter air combat (vol. 1)

                              By

                              “Impact of flying qualities on mission effectiveness for helicopter air combat (vol. 1)” Metadata:

                              • Title: ➤  Impact of flying qualities on mission effectiveness for helicopter air combat (vol. 1)
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center
                              • Publish Date:
                              • Publish Location: [Moffett Field, Calif.]

                              “Impact of flying qualities on mission effectiveness for helicopter air combat (vol. 1)” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1983
                              • 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.

                              Online Borrowing:

                                Online Marketplaces

                                Find Impact of flying qualities on mission effectiveness for helicopter air combat (vol. 1) at online marketplaces:


                                18Euler technology assessment for preliminary aircraft design

                                By

                                “Euler technology assessment for preliminary aircraft design” Metadata:

                                • Title: ➤  Euler technology assessment for preliminary aircraft design
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from the National Technical Information Service
                                • Publish Date:
                                • Publish Location: Springfield, VA - Hampton, Va

                                “Euler technology assessment for preliminary aircraft design” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1998
                                • 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.

                                Online Borrowing:

                                  Online Marketplaces

                                  Find Euler technology assessment for preliminary aircraft design at online marketplaces:


                                  19Generic airplane model concept and four specific models developed for use in piloted simulation studies

                                  By

                                  “Generic airplane model concept and four specific models developed for use in piloted simulation studies” Metadata:

                                  • Title: ➤  Generic airplane model concept and four specific models developed for use in piloted simulation studies
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                  • Publish Date:
                                  • Publish Location: [Springfield, Va - Hampton, Va

                                  “Generic airplane model concept and four specific models developed for use in piloted simulation studies” 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.

                                  Online Borrowing:

                                    Online Marketplaces

                                    Find Generic airplane model concept and four specific models developed for use in piloted simulation studies at online marketplaces:


                                    20PREDAVOR

                                    By

                                    “PREDAVOR” Metadata:

                                    • Title: PREDAVOR
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                    • Publish Date:
                                    • Publish Location: ➤  [Washington, DC - Springfield, Va

                                    “PREDAVOR” 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.

                                    Online Borrowing:

                                      Online Marketplaces

                                      Find PREDAVOR at online marketplaces:


                                      21A design procedure for the handling qualities optimization of the X-29A aircraft

                                      By

                                      “A design procedure for the handling qualities optimization of the X-29A aircraft” Metadata:

                                      • Title: ➤  A design procedure for the handling qualities optimization of the X-29A aircraft
                                      • Author:
                                      • Language: English
                                      • Number of Pages: Median: 18
                                      • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
                                      • Publish Date:
                                      • Publish Location: ➤  [Springfield, VA - [Washington, DC]

                                      “A design procedure for the handling qualities optimization of the X-29A aircraft” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

                                      • First Year Published: 1989
                                      • 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.

                                      Online Borrowing:

                                        Online Marketplaces

                                        Find A design procedure for the handling qualities optimization of the X-29A aircraft at online marketplaces:


                                        22Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5

                                        By

                                        “Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5” Metadata:

                                        • Title: ➤  Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
                                        • Publish Date:
                                        • Publish Location: ➤  Hampton, Va - NASA Center for AeroSpace Information [distributor] - Linthicum Heights, MD - Springfield, VA

                                        “Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5” 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.

                                        Online Borrowing:

                                          Online Marketplaces

                                          Find Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5 at online marketplaces:


                                          23Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling

                                          By

                                          “Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling” Metadata:

                                          • Title: ➤  Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
                                          • Publish Date:
                                          • Publish Location: ➤  Springfield, Va - [Washington, DC - Reston, VA

                                          “Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling” 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.

                                          Online Borrowing:

                                            Online Marketplaces

                                            Find Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling at online marketplaces:


                                            24Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling

                                            By

                                            “Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling” Metadata:

                                            • Title: ➤  Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
                                            • Publish Date:
                                            • Publish Location: ➤  Springfield, Va - [Washington, DC - Reston, VA

                                            “Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling” 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.

                                            Online Borrowing:

                                              Online Marketplaces

                                              Find Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling at online marketplaces:


                                              25An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities

                                              By

                                              “An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities” Metadata:

                                              • Title: ➤  An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                                              • Publish Date:
                                              • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                              “An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities” 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.

                                              Online Borrowing:

                                                Online Marketplaces

                                                Find An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities at online marketplaces:


                                                26Pilot evaluation comments during selected maneuvers from flight tests of the HARV NASA-1A control law

                                                By

                                                “Pilot evaluation comments during selected maneuvers from flight tests of the HARV NASA-1A control law” Metadata:

                                                • Title: ➤  Pilot evaluation comments during selected maneuvers from flight tests of the HARV NASA-1A control law
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                                • Publish Date:
                                                • Publish Location: [Springfield, Va - Hampton, Va

                                                “Pilot evaluation comments during selected maneuvers from flight tests of the HARV NASA-1A control law” 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.

                                                Online Borrowing:

                                                  Online Marketplaces

                                                  Find Pilot evaluation comments during selected maneuvers from flight tests of the HARV NASA-1A control law at online marketplaces:


                                                  27Elements of active vibration control for rotating machinery

                                                  By

                                                  “Elements of active vibration control for rotating machinery” Metadata:

                                                  • Title: ➤  Elements of active vibration control for rotating machinery
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  For sale by the National Technical Information Service - NASA
                                                  • Publish Date:
                                                  • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                                  “Elements of active vibration control for rotating machinery” 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.

                                                  Online Borrowing:

                                                    Online Marketplaces

                                                    Find Elements of active vibration control for rotating machinery at online marketplaces:


                                                    28Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air

                                                    By

                                                    “Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air” Metadata:

                                                    • Title: ➤  Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air
                                                    • 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

                                                    “Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1999
                                                    • 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.

                                                    Online Borrowing:

                                                      Online Marketplaces

                                                      Find Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air at online marketplaces:


                                                      29Failures in advanced flight control systems of future transport aircraft

                                                      By

                                                      “Failures in advanced flight control systems of future transport aircraft” Metadata:

                                                      • Title: ➤  Failures in advanced flight control systems of future transport aircraft
                                                      • Author:
                                                      • Number of Pages: Median: 184
                                                      • Publisher: National Aerospace Laboratory
                                                      • Publish Date:
                                                      • Publish Location: Amsterdam

                                                      “Failures in advanced flight control systems of future transport aircraft” Subjects and Themes:

                                                      Edition Identifiers:

                                                      Access and General Info:

                                                      • First Year Published: 1984
                                                      • Is Full Text Available: No
                                                      • Is The Book Public: No
                                                      • Access Status: No_ebook

                                                      Online Marketplaces

                                                      Find Failures in advanced flight control systems of future transport aircraft at online marketplaces:


                                                      30Pilot-induced oscillation research

                                                      “Pilot-induced oscillation research” Metadata:

                                                      • Title: ➤  Pilot-induced oscillation research
                                                      • Language: English
                                                      • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - NASA Center for AeroSpace Information (CASI)
                                                      • Publish Date:
                                                      • Publish Location: Edwards, Calif - Hanover, MD

                                                      “Pilot-induced oscillation research” Subjects and Themes:

                                                      Edition Identifiers:

                                                      Access and General Info:

                                                      • First Year Published: 2001
                                                      • 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.

                                                      Online Borrowing:

                                                        Online Marketplaces

                                                        Find Pilot-induced oscillation research at online marketplaces: