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A distributed control system (DCS) is a computerized control system for a process or plant usually with many control loops, in which autonomous controllers are distributed throughout the system, but there is no central operator supervisory control. This is in contrast to systems that use centralized controllers; either discrete controllers ...
FOUNDATION HSE provides complete "DCS style" redundancy with redundant network switches, redundant devices, and redundant communication ports ensuring unsurpassed availability. Foundation HSE is also based on standard IP, enabling it to coexist with other devices and ensuring compatibility with standard tools.
An operator training simulator (OTS) is a computer-based training system that uses a dynamic simulation model of an industrial process, usually integrated with an emulator of the process plant's Distributed Control System (DCS). [1]
DeltaV, a distributed control system used in industrial process control; Other uses. Delta-v, a novel by Daniel Suarez; Delta-V (musical group), an Italian band ...
A distributed control system (DCS) is a digital process control system (PCS) for a process or plant, wherein controller functions and field connection modules are distributed throughout the system. As the number of control loops grows, DCS becomes more cost effective than discrete controllers.
OPC servers provide a method for different software packages (as long as it is an OPC client) to access data from a process control device, such as a programmable logic controller (PLC) or distributed control system (DCS). Traditionally, any time a package needed access to data from a device, a custom interface or driver had to be written.
Developed in 1985, SIMVOX was the first simulation software application for Fisher Controls PROVOX Distributed Control System. SIMVOX was a VMS-based simulation software package used for PROVOX system testing and training. It was adopted by Fisher Controls as the worldwide platform for PROVOX testing and training in 1986.
Delta-v (also known as "change in velocity"), symbolized as and pronounced /dɛltə viː/, as used in spacecraft flight dynamics, is a measure of the impulse per unit of spacecraft mass that is needed to perform a maneuver such as launching from or landing on a planet or moon, or an in-space orbital maneuver.