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address these issues Advanced Avionics System advanced integrated flight altimeter Ames Research Center ATC simulation autopilot autopilot-mode controller California CC-CPU cockpits incorporating advanced conducted that demonstrates configuration crew-station research Crew-Station Systems-Integration Research criteria for rotorcraft DAAS data input David Thompson demonstrates the main Demonstration Advanced Avionics design criteria developed to support DEVELOPMENT AND VALIDATION display device drive the simulation electronics executive controls experiments that contribute fixed-wing aircraft flight planning flown Gary Leong Gordon Hardy hardware helicopter integrated flight-management systems intercom interface KOPS lation magnetic brakes main features management systems missed approach Moffett Field monitoring multitask NASA navigation aids neutral point Palo Alto parameters pedestal Performing Organization radio tuning heads reconfigurable RNAV rotorcraft cockpits incorporating scenario segment simu simulation cab simulation math model simulation software Sterling Software support experiments switches systems in aircraft Systems-Integration Research Simulation Ted Lichtenstein tion understanding of design validation experiment various issues associated Whetstone benchmark