发明名称 System and method for an integrated backup control system
摘要 Embodiments of the invention relate to a flight control system for controlling an aircraft in flight having a backup control system integrated into an active control stick. The actuated control stick may include a processing unit that includes independent and separate hardware and/or software dedicated to the primary control system and the backup control system. For the primary control system, the processing unit may receive a sensed primary control stick signal and communicate with a primary processor, which may be configured to generate a primary control signal. For the backup control system, the processing unit may receive a sensed backup control stick signal and generate a backup control signal. The processing unit may also generate tactile signal for use by the actuated control stick to adjust the feel of a pilot's control stick.
申请公布号 US8104720(B2) 申请公布日期 2012.01.31
申请号 US201113019226 申请日期 2011.02.01
申请人 HIRVONEN JUKKA MATTI;PALFREYMAN GARY;GULFSTREAM AEROSPACE CORPORATION 发明人 HIRVONEN JUKKA MATTI;PALFREYMAN GARY
分类号 B64C13/00;B64C13/42 主分类号 B64C13/00
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