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A Hybrid Facility for the Simulation, Development, and Validation of ECS Microprocessor Based Controls
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English
Abstract
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.
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Citation
Emde, 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.Also In
References
- Lloyd A. J. P. et al “Environmental Control System Transient Analysis” July 1977
- “Air Transport Avionics Equipment Interfaces” February 1982