Integrated controller applied to aircraft and aircraft
The embodiment of the invention provides an integrated controller applied to an aircraft and the aircraft, and the integrated controller comprises a case, and a functional module, a backboard and an interface board which are arranged in the case; a plurality of module slots are formed in the inner w...
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| creator | ZHANG TAO CHANG XINYUE YANG CHUNLEI NIAN YONGSHANG WEI MIN JIANG KAI LI XUESI WANG JINING FAN JIAORONG SHI RUOCHONG CONG ENBO CHEN JUNJIE WAN GUIBIN WANG RUOFAN SU ZHONGWEI REN XINYU SUN RUNYU |
| description | The embodiment of the invention provides an integrated controller applied to an aircraft and the aircraft, and the integrated controller comprises a case, and a functional module, a backboard and an interface board which are arranged in the case; a plurality of module slots are formed in the inner wall of the case, and at least two functional modules are inserted into the module slots from the front end of the case in the direction of the center line of the case. The back plate is perpendicular to the center line of the case and connected to the rear end of the case. The interface board is perpendicular to the center line of the case, connected to the rear end of the case and located on the outer side of the back plate. And an interface in the interface board is exposed out of the rear endsurface of the case. The integrated controller applied to the aircraft and the aircraft provided by the embodiment of the invention have the advantages of integration and miniaturization.
本申请实施例提供一种应用于飞行器的综合控制器及飞行器，其中，综合控制器包 |
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本申请实施例提供一种应用于飞行器的综合控制器及飞行器，其中，综合控制器包</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS |
| title | Integrated controller applied to aircraft and aircraft |
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