Starting/generating system and method for aircraft turbine engine

A starting/generating system for an aircraft turbine engine, the starting/generating system comprising at least one brushless drive motor/generator (1), at least one control module (6) and at least one power module (7), the power module (7) being configured to supply/receive electric power from the brushless drive motor/generator (1), the control module (6) being connected to the brushless drive motor/generator (1) by a control cable (L1) in order to control its operation, in which system the power module (7) is configured to be mounted in the housing (3) of the non-pressurised zone (NP) so asto be located adjacent to the brushless drive motor/generator (1) and the control module (6) is configured to be mounted in a pressurised zone (P) of the aircraft, the control module (2) being connected to the power module (7) by a two-way communication cable (L3) in order to control its operation. 用于飞机涡轮发动机的启动/发电系统，其包括至少一个无刷驱动马达/发电机(1)、至少一个控制模块(6)和至少一个电源模块(7)，电源模块(7)被配置为向无刷驱动马达/发电机(1)供应电力或从无刷驱动马达/发电机(1)接收电力，控制模块(6)通过控制电