A Hybrid Facility for the Simulation, Development, and Validation of ECS Microprocessor Based Controls 820867
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.
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. Download Citation
Author(s):
Brion N. Emde, Adam J. P. Lloyd
Affiliated:
Systems Research Group, Boeing Commercial Airplane Co.
Pages: 10
Event:
Intersociety Conference on Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Computer simulation
Virtual reality
Control systems
Simulation and modeling
Technical review
SAE MOBILUS
Subscribers can view annotate, and download all of SAE's content.
Learn More »