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A Hybrid Facility for the Simulation, Development, and Validation of ECS Microprocessor Based Controls
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1982 by SAE International in United States
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This paper presents an overview of digital microprocessor-based Environmental Control System (ECS) controller development and validation at Boeing. The application of a hybrid computer simulation laboratory to the development of real-time simulation capability for ECS is described. The approach used to develop microprocessor-based ECS controllers is illustrated by describing the steps which led to the implementation of a fully automatic cabin pressure control system. The approach to validating ECS digital controllers is also discussed.
CitationEmde, B. and Lloyd, A., "A Hybrid Facility for the Simulation, Development, and Validation of ECS Microprocessor Based Controls," SAE Technical Paper 820867, 1982, https://doi.org/10.4271/820867.
- Lloyd A. J. P. et al “Environmental Control System Transient Analysis” July 1977
- “Air Transport Avionics Equipment Interfaces” February 1982