Temperature control of the Mariner Venus 67 spacecraft
Temperature control design, instrumentation, and performance characteristics of Mariner 5 spacecraft
Dumas, L. N.↗
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Results for “Control design”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A method for obtaining desired sensitivity characteristics with optimal controls.
Feedback optimal control design minimizing parameter variations effects on system performance
Deyst, J. J., Jr.↗
Determination of a realistic error bound for a class of imperfect nonlinear controllers.
Error bound determined for class of nonlinear controllers designed by second method of Liapunov
Taylor, T. M.↗
Application of quadratic optimization to helicopter flight control.
Quadratic optimization applied to helicopter flight control design, assuming constant feedback gains and command step input with zero steady state error
Gray, D. L.↗
Quasi-optimum design of an aircraft landing control system.
Quasi-optimum control law for aircraft landing control system design based on Friedland technique, evaluating effectiveness by computer simulation
Ling, C. K.↗
Development and Implementation - DSIF Development
Antenna system instrumentation, phase modulator designs, control systems for transmitter and motor generator, and related DSIF developments
Source record↗
Application of imperfect, reduced-state relay control to model-reference systems
Imperfect, reduced-state relay control application to model-refference controller design
Taylor, T. M.↗
Relay control of systems with parameter uncertainties and disturbances
Relay control design for model-tracking system with parameter uncertainties and disturbances using semidefinite Liapunov function
Lindorff, D. P.↗
Design of the passive thermal control system of the SERT II satellite
Passive thermal control system design of SERT II nonspinning satellite based on 534-node analytical model calibrated against test data
Smolak, G. R.↗
Design of the passive thermal control system of the SERT II satellite
Mercury bombardment ion thrustor life test in space environment onboard space electric rocket test /SERT/ satellite, describing passive satellite thermal control system design
Smolak, G. R.↗
Determination of bounds on performance measure and min-max controllers in time-lag systems
Time lag system performance index bounds determination and optimal feedback controller design based on min-max criteria
Kahne, S. J.↗
Adaptive control of multivariable systems
Stable adaptive control design for linear time- invariant system with same number of inputs as outputs, considering disturbance effect
Lindorff, D. P.↗
Review of SERT II power conditioning
Power conditioning system for Hg ion thrustor on SERT 2 spacecraft, considering performance, design, control circuits and arcing
Bagwell, J. W.↗
Calibration-interval adjustment indicator - A concept
Circuit, when used with decision table, permits relatively unskilled personnel to maintain effective quality control. Design determines required changes in calibration intervals. Interval readings are recorded to nearest integer, making high precision unnecessary. Specific required performance-history information is discussed.
Hedene, P. S.↗
Space storable propellant module thermal control technology. Volume 1 - OF2/B2H6 propulsion module Summary report
Space storable oxygen fluoride/boron hydride tank module thermal control design for Jupiter mission
De Land, R. E.↗
Space storable propellant module thermal control technology. Volume 2 - F2/N2H4 propulsion module Summary report
Space storable fluorine/hydrazine tank module thermal control design for Jupiter mission
De Land, R. E.↗
High stability FM TV transmitter with sampled automatic frequency control
S band frequency modulated television transmitter with sampled automatic frequency control designed to drive traveling-wave-tube amplifier
Honnell, M. A.↗
Use of thermal analyses of systems to evolve development projects in spacecraft thermal control concepts
System and component models for spacecraft thermal control design, considering materials, environmental degradation, measurement errors, manufacturing and quality assurance
Turner, M. A.↗