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  • Author > Mukhopadhyay, A. K. [x]

  • Sort results by: NASA Center | Date Added to NTRS | Publication Year
    There are a total of 16 record(s) matching your query.
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    Performance verification and system parameter identification of spacecraft tape recorder control servo

    Author(s): Mukhopadhyay, A. K.
    Abstract: Design adequacy of the lead-lag compensator of the frequency loop, accuracy checking of the analytical expression for the electrical motor transfer function, and performance evaluation of the speed control servo of the ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1979
    Added to NTRS: 2004-11-03
    Accession Number: 79A41736; Document ID: 19790057723

    Monte Carlo modeling of the Martian atmosphere from Viking mission design point of view

    Author(s): Mukhopadhyay, A. K.
    Abstract: Martian atmosphere modeling for obtaining Viking lander spacecraft design margins by Monte Carlo method
    NASA Center: NASA (non Center Specific)
    Publication Year: 1970
    Added to NTRS: 2004-11-03
    Accession Number: 70A30564; Document ID: 19700054448

    Study of the effect of static/dynamic Coulomb friction variation at the tape-head interface of a spacecraft tape recorder by non-linear time response simulation

    Author(s): Mukhopadhyay, A. K.
    Abstract: A description is presented of six simulation cases investigating the effect of the variation of static-dynamic Coulomb friction on servo system stability/performance. The upper and lower levels of dynamic Coulomb friction ...
    NASA Center: NASA (non Center Specific)
    Publication Year: 1978
    Added to NTRS: 2004-11-03
    Accession Number: 78A51253; Document ID: 19780067344

    Subsystem weight trade-off studies for the design optimization of an out-of-orbit Mars soft lander

    Author(s): Mukhopadhyay, A. K.
    Abstract: Subsystem weight trade-offs for design optimization of out-of-orbit Mars soft lander, using atmosphere and surface environmental Monte Carlo model
    NASA Center: NASA (non Center Specific)
    Publication Year: 1970
    Added to NTRS: 2004-11-03
    Accession Number: 70A26215; Document ID: 19700050099

    Transfer function verification and block diagram simplification of a very high-order distributed pole closed-loop servo by means of non-linear time-response simulation

    Author(s): Mukhopadhyay, A. K.
    Abstract: Linear frequency domain methods are inadequate in analyzing the 1975 Viking Orbiter (VO75) digital tape recorder servo due to dominant nonlinear effects such as servo signal limiting, unidirectional servo control, and ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1975
    Added to NTRS: 2004-11-03
    Accession Number: 76A42089; Document ID: 19760059123

    Economic and engineering implications of the Project Independence 1985 geothermal energy output goal and the associated sensitivity analysis

    Author(s): Mukhopadhyay, A. K.
    Abstract: No Abstract Available
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1976
    Added to NTRS: 2004-11-03
    Accession Number: 77A12745; Document ID: 19770029893

    Effect of trajectory, guidance, and environmental parameters and uncertainties on the design optimization of the out-of-orbit Viking soft lander

    Author(s): Mukhopadhyay, A. K.
    Abstract: Trajectory, guidance and environmental parameters and uncertainties effect on design optimization of out-of-orbit Viking soft lander
    NASA Center: NASA (non Center Specific)
    Publication Year: 1970
    Added to NTRS: 2004-11-03
    Accession Number: 70A18134; Document ID: 19700042018; Report Number: AIAA PAPER 70-99

    Discrete event simulation and the resultant data storage system response in the operational mission environment of Jupiter-Saturn /Voyager/ spacecraft

    Author(s): Mukhopadhyay, A. K.
    Abstract: The Data Storage Subsystem Simulator (DSSSIM) simulating (by ground software) occurrence of discrete events in the Voyager mission is described. Functional requirements for Data Storage Subsystems (DSS) simulation are ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1978
    Added to NTRS: 2004-11-03
    Accession Number: 80A49834; Document ID: 19800065664

    Time response simulation of the guidance and control system of an automatically steered wire-following vehicle

    Author(s): Mukhopadhyay, A. K.; Dobrotin, B. M.
    Abstract: Time-response simulation studies carried out in support of the development and validation of the guidance/steering subsystem of a wire-following-vehicle (WFV) are described. A lateral guidance system is outlined, field ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1979
    Added to NTRS: 2004-11-03
    Accession Number: 80A47557; Document ID: 19800063387

    Automated flight path design for planetary flyby missions using advanced interactive graphics hardware/software

    Author(s): Mukhopadhyay, A. K.
    Abstract: Computer graphic interactive flight path design program for planetary flyby missions
    NASA Center: NASA (non Center Specific)
    Publication Year: 1971
    Added to NTRS: 2004-11-03
    Accession Number: 71A43050; Document ID: 19710062353; Report Number: AAS PAPER 71-380

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