| 摘要 |
Modular electronic flight control system has a number of actuator modules (10,11) and a number of Actuator Control-Electronics (ACEs) (20,21). Each individual actuator module is assigned with a particular ACE. The ACE directly receives pilot guidelines and the actuator module is controlled accordingly. The ACEs have a selection logic, which decides, whether to use the directly received pilot guidelines or the reference values of the primary flight control processor (30,31) for controlling the actuator module. |
