| 摘要 |
<p>The system has a set of LCD screens (FE1, FE2) that is independent to each other in a multi-tactile display unit (MTDU), and two tactile surfaces (TS1, TS2) are dedicated to corresponding LCD screens. Two electronic units (BE) are provided for acquisition of aeronautical presentation data with information output from the set of LCD screens. A set of independent electrical supplies (Ps1, PS2) is arranged, and a safety unit allows information output to failed LCD screen and/or tactile surface to be reconfigured on the screen of active display and tactile surface. The screens and tactile surface are provided based on different technologies.</p> |
