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Source: The Open Library

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1The propulsive-only flight control problem

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“The propulsive-only flight control problem” Metadata:

  • Title: ➤  The propulsive-only flight control problem
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C - Springfield, Va

“The propulsive-only flight control problem” 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

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    2Pilot-in-the-loop analysis of propulsive-only flight control systems

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    “Pilot-in-the-loop analysis of propulsive-only flight control systems” Metadata:

    • Title: ➤  Pilot-in-the-loop analysis of propulsive-only flight control systems
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Washington, DC - Springfield, Va

    “Pilot-in-the-loop analysis of propulsive-only flight control systems” 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:

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      3A comparison of time-optimal interception trajectories for the F-8 and F-15

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      “A comparison of time-optimal interception trajectories for the F-8 and F-15” Metadata:

      • Title: ➤  A comparison of time-optimal interception trajectories for the F-8 and F-15
      • Author:
      • Language: English
      • Publisher: ➤  Georgia Institute of Technology, School of Aerospace Engineering
      • Publish Date:
      • Publish Location: Atlanta, GA

      “A comparison of time-optimal interception trajectories for the F-8 and F-15” 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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        4The control system for the X-33 linear aerospike engine

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        “The control system for the X-33 linear aerospike engine” Metadata:

        • Title: ➤  The control system for the X-33 linear aerospike engine
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: ➤  [Washington, DC - Springfield, Va

        “The control system for the X-33 linear aerospike engine” 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:

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          5Design, analysis, and control of large transport aircraft utilizing selective engine thrust as a backup system for the primary flight control

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          “Design, analysis, and control of large transport aircraft utilizing selective engine thrust as a backup system for the primary flight control” Metadata:

          • Title: ➤  Design, analysis, and control of large transport aircraft utilizing selective engine thrust as a backup system for the primary flight control
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Facility
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - [Edwards, Calif.]

          “Design, analysis, and control of large transport aircraft utilizing selective engine thrust as a backup system for the primary flight control” 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

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          Downloads Are Not Available:

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            6Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls

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            “Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls” Metadata:

            • Title: ➤  Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - University of Kansas, Center for Research, Inc. - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  Springfield, Va - [Washington, DC - Lawrence, Kan

            “Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls” 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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              7Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft

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              “Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft” Metadata:

              • Title: ➤  Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  [Springfield, Va - [Washington, DC]

              “Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft” 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

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                8Numerical analysis of a variable camber rotor blade as a lift cotrol device

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                “Numerical analysis of a variable camber rotor blade as a lift cotrol device” Metadata:

                • Title: ➤  Numerical analysis of a variable camber rotor blade as a lift cotrol device
                • Author:
                • Language: English
                • Publisher: ➤  Flight Research Laboratory, University of Kansas Center for Research, Inc. - National Aeronautics and Space Administration, Ames Research Center
                • Publish Date:
                • Publish Location: ➤  [Moffett Field, Calif - Lawrence, Kans

                “Numerical analysis of a variable camber rotor blade as a lift cotrol device” 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

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                  9A vehicle health monitoring system for the space shuttle reaction control system during reentry

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                  “A vehicle health monitoring system for the space shuttle reaction control system during reentry” Metadata:

                  • Title: ➤  A vehicle health monitoring system for the space shuttle reaction control system during reentry
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration - Charles Stark Draper Laboratory - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  Cambridge, Mass - [Washington, DC - Springfield, Va

                  “A vehicle health monitoring system for the space shuttle reaction control system during reentry” 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:

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                    10Guidance and control strategies for aerospace vehicles

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                    “Guidance and control strategies for aerospace vehicles” Metadata:

                    • Title: ➤  Guidance and control strategies for aerospace vehicles
                    • Author:
                    • Language: English
                    • Publisher: ➤  Old Dominion University Research Foundation
                    • Publish Date:
                    • Publish Location: Norfolk, Va

                    “Guidance and control strategies for aerospace vehicles” 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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                      Wiki

                      Source: Wikipedia

                      Wikipedia Results

                      Search Results from Wikipedia

                      Thrust vectoring

                      Thrust vectoring, also known as thrust vector control (TVC), is the ability of an aircraft, rocket or other vehicle to manipulate the direction of the

                      Thrust

                      Thrust is a reaction force described quantitatively by Newton's third law. When a system expels or accelerates mass in one direction, the accelerated mass

                      Thrust reversal

                      Thrust reversal, also called reverse thrust, is an operating mode for jet engines equipped with a thrust reverser when thrust is directed forwards for

                      Thrust lever

                      Thrust levers or throttle levers are found in the cockpit of aircraft, and are used by the pilot, copilot, flight engineer, or autopilot to control the

                      Reaction control system

                      wheels can be used for attitude control, rather than RCS. Use of diverted engine thrust to provide stable attitude control of a short-or-vertical takeoff

                      Autopilot

                      a system, besides classic flight controls, many autopilots incorporate thrust control capabilities that can control throttles to optimize the airspeed

                      Convair F-106 Delta Dart

                      two-position afterburner exhaust nozzle was also used for idle thrust control, held open to decrease thrust by 40%, resulting in slower taxiing and less brake wear

                      Propelling nozzle

                      minimum area before or at the Military or maximum dry thrust setting. Two examples of this control are the General Electric J-79 and the Klimov RD-33 in

                      Cathay Pacific Flight 780

                      compensate for the low thrust of No. 2 engine. Following these actions, the crew declared a "pan-pan" with Hong Kong air traffic control, requesting the shortest

                      Critical engine

                      magnitude of the remaining thrust yawing moments with increasing angle of attack, only in the direction left or right. The minimum control speed during takeoff