| 摘要 |
FIELD: aircraft engineering. ^ SUBSTANCE: display system (1) incorporates hardware (4) to automatically reconfigure system (1) if one of system displays (E1 to En) fails. Aforesaid reconfiguring hardware exploits priority rule for displaying image related with faulty display. Note that hardware (4) comprises multiple auxiliary appliances (B1 to Bn), each being connected with one of aforesaid displays ( E1 to En). ^ EFFECT: higher reliability. ^ 8 cl, 2 dwg |
