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  • Final report for space shuttle propulsion estimation development verification [microform] : volume II / by Robert M. Rogers.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Final report for space shuttle propulsion estimation development verification [microform] : volume I / by Robert M. Rogers.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Groundspeed filtering for CTAS [microform] / G.L. Slater.

    • Text
    • Cincinnati, Ohio : Dept. of Aerospace Engineering and Engineering Mechanics, University of Cincinnati ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A real-time algorithm for integrating differential satellite and inertial navigation information during helicopter approach [microform] / by Ty Hoang.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994

  • Development of response models for the Earth Radiation Budget Experiment (ERBE) sensors. Part IV, Preliminary nonscanner models and count conversion algorithms [microform] / Nesim Halyo and Sang H. Choi.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Controlling flexible manipulators [microform] : an experimental investigation / by Gordon Greene Hastings.

    • Text
    • [Atlanta, GA] : Georgia Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Range filtering for sequential GPS receivers with external sensor augmentation [microform] / Russell Paielli.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • A simulation study of turbofan engine deterioration estimation using Kalman filtering techniques [microform] / Heather H. Lambert.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
    • 1991

  • Kalman filtering, smoothing and recursive robot arm forward and inverse dynamics [microform] / G. Rodriguez.

    • Text
    • Pasadena, Calif. : National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • The design of multirate degital control systems [microform] / Martin Conrad Berg.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Control design for robust stability in linear regulators [microform] : application to aerospace flight control : final report / by Ramra K. Yedavalli.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Performance analysis of a GPS interferometric attitude determination system for a gravity gradient stabilized spacecraft [microform] / by John C. Stoll.

    • Text
    • Cambridge, Mass. : Charles Stark Draper Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A vehicle health monitoring system for the space shuttle reaction control system during reentry [microform] / by Anthony David Rosello.

    • Text
    • Cambridge, Mass. : Charles Stark Draper Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Flight test results from real-time relative global positioning system flight experiment on STS-69 [microform] / Young W. Park ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Comparison of five system identification algorithms for rotorcraft higher harmonic control [microform] / Stephen A. Jacklin.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Kalman filtering with inequality constraints for turbofan engine health estimation [microform] / Dan Simon, Donald L. Simon.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55855

  • Discrete filtering techniques applied to sequential GPS range measurements [microform] / by Frank van Graas.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58418

  • On-line range prediction system (II) [microform] / principal investiagor, Nhan Levan.

    • Text
    • [Los Angeles, Calif. : UCLA School of Engineering and Applied Science ; Moffett Field, Calif. : NASA-Ames Dryden ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62215

  • Computer simulation of a pilot in V/STOL aircraft control loops. Appendix III, The adaptive control model of a pilot in V/STOL aircraft control loops [microform] / principal investigators: William G. Vogt, Marlin H. Mickle.

    • Text
    • Cleveland, OH : NASA Lewis Research Center, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69060

  • Estimating short-period dynamics using an extended Kalman filter [microform] / Jeffrey E. Bauer, Dominick Andrisani.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69237

  • A preliminary evaluation of an F100 engine parameter estimation process using flight data [microform] / Trindel A. Maine, Glenn B. Gilyard, and Heather H. Lambert.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70364

  • Discovery of the Kalman filter as a practical tool for aerospace and industry [microform] / Leonard A. McGee and Stanley F. Schmidt.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104644

  • On identifiability of bias-type actuator-sensor faults in multiple-model-based fault detection and identification / Suresh M. Joshi.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30917

  • Model based estimation of image depth and displacement / by Kevin T. Damour.

    • Text
    • Troy, New York : Rensselaer Polytechnic Institute, Electrical, Computer, and Systems Engineering Department, May 1992.
    • 1992-5

  • Background error covariance estimation using information from a single model trajectory with application to ocean data assimilation into the GEOS-5 coupled model / Christian L. Keppenne [and three others]

    • Text
    • Greenbelt, Maryland : National Aeronautics and Space Administration, Goddard Space Flight Center, September 2014.
    • 2014-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo59994

  • Model based estimation of image depth and displacement / by Kevin T. Damour.

    • Text
    • Troy, New York : Rensselaer Polytechnic Institute, Electrical, Computer, and Systems Engineering Department, May 1992.
    • 1992-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51994

  • Design and implementation of a parallel multivariate ensemble Kalman filter for the Poseidon ocean general circulation model / Christian L. Keppenne, Michele M. Rienecker.

    • Text
    • Greenbelt, Maryland : National Aeronautics and Space Administration, Goddard Space Flight Center, September 2001.
    • 2001-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo60456

  • A short tutorial on inertial navigation system and global positioning system integration / Kyle M. Smalling, Kenneth W. Eure.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2015.
    • 2015-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64041

  • Sensor selection for aircraft engine performance estimation and gas path fault diagnostics / Donald L. Simon, Aidan W. Rinehart.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2016.
    • 2016-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65884

  • Model-based engine control architecture with an extended Kalman filter / Jeffrey T. Csank and Joseph W. Connolly.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67578

  • Enhanced engine performance during emergency operation using a model-based engine control architecture / Jeffrey T. Csank and Joseph W. Connolly.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2016.
    • 2016-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68605

  • Application of an optimal tuner selection approach for on-board self-tuning engine models / Donald L. Simon, Jeffrey B. Armstrong, Sanjay Garg.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo29111

  • An integrated approach for aircraft engine performance estimation and fault diagnostics / Donald L. Simon, Jeffrey B. Armstrong.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37879

  • Exploration of an adaptive routine for battery modeling / Kenneth W. Eure, Edward F. Hogge.

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, March 2022.
    • 2022-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo176256

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