| 摘要 |
A control system and method of the anti-skid computers of an aircraft are provided. The control system comprises two IMA computers, comprising each one an Avionics Computer Control Device, an Avionics Computer Monitoring Device and at least one dual data acquisition means and at least one dual processing means. Each Avionics Computer Control Device and each Avionics Computer Monitoring Device are connected to the anti-skid computers of both sides. |
