Five tasks were completed toward the design of an advanced Subsystem Status Monitor that will reduce crew workload during the monitoring of helicopter subsystems: (1) Analysis of parameters currently monitored in the UH-60A, CH-47C, OH-58C, and AH-1G Army helicopters, and recommendation of information requirements for these helicopters, (2) Development of prioritization, logic, and display formats for the presentation of subsystem information on multi-function electronic displays for the above-mentioned helicopters, (3) Preliminary design of system architectures incorporating state-of-the-art, near-term and long-term technologies into an advanced Subsystem Status Monitor, (4) Evaluation of preliminary designs to determine predicted impacts on flight safety, workload, reliability and maintainability, survivability and vulnerability, aircraft space and volume, aircraft weight, and life cycle costs, (5) Design of keyboard and associated display formats for the following peripheral functions: checklist presentation, performance calculation, and load monitoring. (Author)
Advanced Subsystems Status Monitor
1980
261 pages
Report
Keine Angabe
Englisch
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