发明名称 AIRCRAFT UTILITY SYSTEMS CONTROL AND INTEGRATION
摘要 <p>An integrated aircraft control system in which the avionics functions of flight control are united with the utility functions of aircraft tending in an overall integration system utilizing a pilot cockpit display for producing control signals to a modular avionics unit which also receives inputs from the aircraft system sensors and the integrated avionics system to produce output signals for use by the aircraft controlled devices.</p>
申请公布号 WO1998013667(A1) 申请公布日期 1998.04.02
申请号 US1997016127 申请日期 1997.09.18
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