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  1. 1
    Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft

    Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft by Murphy, Patrick C.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  2. 2
    Efficient eigenvalue assignment by state and output feedback with applications for large space structures

    Efficient eigenvalue assignment by state and output feedback with applications for large space structures by Vannell, Eric C. (Eric Carl)

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  3. 3
    Three-axis stabilization of spacecraft using parameter-independent nonlinear quaternion feedback

    Three-axis stabilization of spacecraft using parameter-independent nonlinear quaternion feedback by Joshi, S. M. (Suresh M.)

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  4. 4
    Control structure interaction/optimized design

    Control structure interaction/optimized design by McLaren, Mark

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  5. 5
    Flight guidance system validation using SPIN

    Flight guidance system validation using SPIN by Naydich, Dimitri

    Hampton, Va. : Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1998
    Format: Government Document Book


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  6. 6
    NASA future mission needs and benefits of controls : structural interaction technology

    NASA future mission needs and benefits of controls : structural interaction technology by Grantham, William L.

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, VA] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service, distributor], 1991
    Format: Government Document Book


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  7. 7
    Exploratory studies in generalized predictive control for active aeroelastic control of tiltrotor aircraft

    Exploratory studies in generalized predictive control for active aeroelastic control of tiltrotor aircraft by Kvaternik, Raymond G.

    Hampton, Va. : Hanover, MD :; Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for Aerospace Information (CASI), 2000
    Format: Government Document Book


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  8. 8
    Microgravity isolation system design : a case study

    Microgravity isolation system design : a case study

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  9. 9
    An expert system for restructurable control

    An expert system for restructurable control by Litt, Jonathan

    [Washington, DC] : [St. Louis, Mo.] : NASA ; US Army Aviation Systems Command, Aviation R&T Activity, 1988
    Format: Government Document Book


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  10. 10
    Near minimum-time maneuvers of the Advanced Space Structures Technology Research Experiment (ASTREX) test article : theory and experiments

    Near minimum-time maneuvers of the Advanced Space Structures Technology Research Experiment (ASTREX) test article : theory and experiments by Vadali, Srinivas

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  11. 11
    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 : final technical report, grant #NAG 2-789

    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 : final technical report, grant #NAG 2-789 by Roskam, Jan, 1930-

    Lawrence, Kan. : [Washington, DC] : [Springfield, Va.] : University of Kansas, Center for Research, Inc. ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  12. 12
    Development of ADOCS controllers and control laws

    Development of ADOCS controllers and control laws by Landis, Kenneth H.

    Moffett Field, Calif. : St. Louis, Mo. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; ; U.S. Army Aviation Systems Command ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


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  13. 13
    System identification methods for aircraft flight control development and validation

    System identification methods for aircraft flight control development and validation by Tischler, Mark B. (Mark Brian), 1957-

    Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, Aeroflightdynamics Directorate ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  14. 14
    Independent Orbiter assessment : analysis of the electrical power distribution and control subsystem

    Independent Orbiter assessment : analysis of the electrical power distribution and control subsystem by Schmeckpeper, K. F.

    Houston, Tex. : [Marshall Space Flight Center, Ala.] :; Houston, Tex. : [Marshall Space Flight Center, Ala. :] : McDonnell Douglas Astronautics Company, Houston Division ; [National Aeronautics and Space Administration, George C. Marshall Space Flight Center], 1987
    Format: Government Document Book


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  15. 15
    Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft

    Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft by Garg, Sanjay

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  16. 16
    Approximations for quantitative feedback theory designs

    Approximations for quantitative feedback theory designs by Henderson, D. K.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  17. 17
    Reduction of helicopter blade-vortex interaction noise by active rotor control technology

    Reduction of helicopter blade-vortex interaction noise by active rotor control technology

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  18. 18
    Modeling and validation of a Navy A6-Intruder actively controlled landing gear system

    Modeling and validation of a Navy A6-Intruder actively controlled landing gear system by Horta, Lucas G.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


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  19. 19
    Application of variable-gain output feedback for high-alpha control

    Application of variable-gain output feedback for high-alpha control by Ostroff, Aaron J.

    Hampton, Va. :; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1990
    Format: Government Document Book


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  20. 20
    Sensitivity, optimal scaling, and minimum roundoff errors in flexible structure models : progress report

    Sensitivity, optimal scaling, and minimum roundoff errors in flexible structure models : progress report by Skelton, Robert E.

    West Lafayette, Ind. : [Washington, DC] : [Springfield, Va.] : Purdue University, School of Aeronautics and Astronautics ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


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