Development and flight testing of a fluidic control system
Three axis fluidic automatic flight control system developed and flight tested
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Three axis fluidic automatic flight control system developed and flight tested
Low sensitivity sampled-data control systems design
Optimality and strong stability of control system
Stabilization and control system sensitivity to power-off failure rate studied by simulated missions using block power switching
Decision making mathematical model for control system operation modes, generating human operators heuristics evolution
Optimal control systems with pure time delay, discussing design parameters
Frequency control system positions mirrors at either end of the laser cavity so the mirror separation is independent of thermal and acoustical fluctuations. A small portion of the laser output is split and directed upon a photodetector /photodiode/.
Design of pitch orientational flight control system
Manned spacecraft control system requirements for abort problems
Photographic control system requirements for Project Apollo manned launches, considering extreme heat, vibration and sound pressure environment
Fluidic secondary injection thrust vector control systems for solid propellant and hydrogen-oxygen rocket engines
Mars lander thermal control system design parameters including environment, power duty cycle and lander size and weight
Flight test experience with adaptive control systems
Requirements, design, and performance of control system from Brayton power system
TV camera output signal control system for digital spacecraft communication
Computerized thermal model simulating environment control system, crew and vehicle structure in performance prediction for Apollo lunar module
Three axis large angle attitude control system global analysis, determining system stability, responsiveness and sensitivity to disturbances
Mounting apparatus for temperature control system