Mariner Venus 67 guidance and control system
Subsystems of Mariner Venus 67 spacecraft guidance and control system
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Subsystems of Mariner Venus 67 spacecraft guidance and control system
Necessary conditions for optimal control systems with adjustable delay time obtained from first order variation of performance index
Control systems design for in-core thermionic reactor space power plants, using variable feedback analysis and analog simulation
Model reference adaptive control system redesign by Liapunov second method for linear systems
Apollo lunar module pressure-fed bipropellant reaction control system design requirements and system description
Design technology of attitude control systems for large launch vehicles
Computation of regions of constrained stability for nonlinear control systems
Translational forces on Mariner 5 stemming from attitude control system studied to determine trajectory for scientific and operational purposes
Translational forces on Mariner 5 stemming from attitude control system, determining trajectory for scientific and operational purposes
Performance index includes a model representing linear control-system design specifications. Based on a geometric criterion for approximation of the model by the actual system, the index can be interpreted directly in terms of the desired system response model without actually having the model's time response.
Analysis of Saturn launch vehicle navigation, guidance, and control system
Saturn S-4B orbital workshop attitude control system analysis
Terminal states and time specifications influence on optimum control systems, using Pontryagin principle for boundary value problems application
Development of spacecraft experiment pointing and attitude control system
Development of magnetic attitude control system for High Energy Astronomy Observatory satellite
Design and development of synchronous servo loop control system
Results and description of qualification tests of attitude control system and yo-yo despin system in flight configuration as installed on IMP-1 spacecraft
Absolute stability analysis of attitude control systems for large launch vehicles