The advanced electronic display system (ADEDS) task included a significant level of simulation effort to develop basic functional and operational requirements that could be translated to equipment hardware/software design specifications. Simulation was also used to evaluate selected ADEDS guidance options and display formats to obtain performance comparison data to be used for later comparison with flight test results. The final major simulation effort involved substitution of the actual airborne equipment into the simulator for integration prior to airplane installation. Detailed test data supporting this report, given in Boeing document D6-41832TN, provide results of the navigation and display subsystems acceptance tests, a summary of airborne equipment problems encountered during simulation integration tests, and pilot performance data from simulator evaluation. (Author)
SST Technology Follow - on Program - Phase II. ADEDS Simulation Test Report
1974
162 pages
Report
Keine Angabe
Englisch
Aircraft , Avionics , Navigation & Guidance System Components , Supersonic transports , Television display systems , Simulation , Specifications , Inertial navigation , Flight testing , Integrated systems , Aviation safety , Noise reduction , Computer programs , Navigation computers , Automatic , Errors , Flight control systems , Flight simulators , Flight instruments , Symbols , Checkout procedures , Acceptance tests , Tracking , Data transmission systems , Systems engineering , Pilot studies , Test methods , Advanced electronic display system , Computer hardware , Crosstrack error , Vertical error , SST technology follow on program