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    There are a total of 515904 record(s) matching your query.
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    Flight Results of the NF-15B Intelligent Flight Control System (IFCS) Aircraft with Adaptation to a Longitudinally Destabilized Plant

    Author(s): Bosworth, John T.
    Abstract: Adaptive flight control systems have the potential to be resilient to extreme changes in airplane behavior. Extreme changes could be a result of a system failure or of damage to the airplane. The goal for the adaptive system ...
    NASA Center: Dryden Flight Research Center
    Publication Year: 2008
    Added to NTRS: 2008-09-11
    Document ID: 20080034509

    GRACE Gravity Data Constrain Ancient Ice Geometries and Continental Dynamics over Laurentia

    Author(s): Tamisiea, M. E.; Mitrovica, J. X.; Davis, J. L.
    Abstract: The free-air gravity trend over Canada, derived from the Gravity Recovery and Climate Experiment (GRACE) satellite mission, robustly isolates the gravity signal associated with glacial isostatic adjustment (GIA) from the ...
    NASA Center: Goddard Space Flight Center
    Publication Year: 2007
    Added to NTRS: 2008-09-11
    Document ID: 20080034472

    Chromated Material Obsolescence

    Author(s): Segars, Matt G.
    Abstract: This viewgraph presentation describes the obsolescence of chrome and cadmium papers. The supplier obsolescence of the Randolph TT-P-1757 zinc chromate primer and continental coatings zinc chromate paste is also presented.
    NASA Center: Marshall Space Flight Center
    Publication Year: 2008
    Added to NTRS: 2008-09-11
    Document ID: 20080034512

    Annoyance judgements of aircraft with and without acoustically treated nacelles

    Author(s): Borsky, P. N.; Leonard, S.
    Abstract: A series of subjective response laboratory tests were conducted to determine the effectiveness of reducing aircraft noise by treating the aircraft engine nacelles with acoustically absorbent material. A total of 108 subjects ...
    NASA Center: NASA (non Center Specific)
    Publication Year: 1973
    Added to NTRS: 2008-09-11
    Accession Number: 73N30941; Document ID: 19730022209; Report Number: NASA-CR-2261

    Practical Application of a Subscale Transport Aircraft for Flight Research in Control Upset and Failure Conditions

    Author(s): Cunningham, Kevin; Foster, John V.; Morelli, Eugene A.; Murch, Austin M.
    Abstract: Over the past decade, the goal of reducing the fatal accident rate of large transport aircraft has resulted in research aimed at the problem of aircraft loss-of-control. Starting in 1999, the NASA Aviation Safety Program ...
    NASA Center: Langley Research Center
    Publication Year: 2008
    Added to NTRS: 2008-09-11
    Document ID: 20080034480

    The X-43 Fin Actuation System Problem - Reliability in Shades of Gray

    Author(s): Peebles, Curtis
    Abstract: Following the loss of the first X-43 during launch, the mishap investigation board indicated the Fin Actuator System (FAS) needed to have a larger torque margin. To supply this added torque, a second actuator was added. The ...
    NASA Center: Dryden Flight Research Center
    Publication Year: 2006
    Added to NTRS: 2008-09-11
    Document ID: 20060047742

    The Role of Trust and Interaction in Global Positioning System Related Accidents

    Author(s): Johnson, Chris W.; Shea, Christine; Holloway, C. Michael
    Abstract: The Global Positioning System (GPS) uses a network of satellites to calculate the position of a receiver over time. This technology has revolutionized a wide range of safety-critical industries and leisure applications. ...
    NASA Center: Langley Research Center
    Publication Year: 2008
    Added to NTRS: 2008-09-11
    Document ID: 20080034491

    In-Flight Stability Analysis of the X-48B Aircraft

    Author(s): Regan, Christopher D.
    Abstract: This report presents the system description, methods, and sample results of the in-flight stability analysis for the X-48B, Blended Wing Body Low-Speed Vehicle. The X-48B vehicle is a dynamically scaled, remotely piloted ...
    NASA Center: Dryden Flight Research Center
    Publication Year: 2008
    Added to NTRS: 2008-09-11
    Document ID: 20080034515

    Verification of a Constraint Force Equation Methodology for Modeling Multi-Body Stage Separation

    Author(s): Tarabini, Paul V.; Roithmayr, Carlos; Toniolo, Matthew D.; Karlgaard, Christopher; Pamadi, Bandu N.
    Abstract: This paper discusses the verification of the Constraint Force Equation (CFE) methodology and its implementation in the Program to Optimize Simulated Trajectories II (POST2) for multibody separation problems using three ...
    NASA Center: Langley Research Center
    Publication Year: 2008
    Added to NTRS: 2008-09-11
    Document ID: 20080034488

    Multibody Modeling and Simulation for the Mars Phoenix Lander Entry, Descent and Landing

    Author(s): Queen, Eric M.; Prince, Jill L.; Desai, Prasun N.
    Abstract: A multi-body flight simulation for the Phoenix Mars Lander has been developed that includes high fidelity six degree-of-freedom rigid-body models for the parachute and lander system. The simulation provides attitude and rate ...
    NASA Center: Langley Research Center
    Publication Year: 2008
    Added to NTRS: 2008-09-11
    Document ID: 20080034477

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