阅读说明：本技术 控制系统 (Control system ) 是由 V.基里齐斯 M.布里斯托 于 2019-06-20 设计创作，主要内容包括：本发明题为“控制系统”。本发明提供了一种能够操作以为飞行器提供经修改的主控制参数的控制系统(100),该控制系统(100)包括：主控制参数支路,该主控制参数支路被配置为输出该飞行器的主控制参数(103)中的需求；主控制参数补偿支路,该主控制参数补偿支路被配置为接收涡流角和/或风扇压力在相对于参考的主控制参数下的绝对水平和/或空间分布的检测到的变化(107),并将该检测到的变化(107)转换为该主控制参数(106)的变化；和处理器,该处理器适于：接收从该主控制参数支路输出的该主控制参数(103)中的需求和从该主控制参数补偿支路输出的该主控制参数(106)的变化；比较从该主控制参数支路输出的该主控制参数(103)中的该需求和从该主控制参数补偿支路输出的该主控制参数(106)的该变化；以及为该飞行器生成经修改的主控制参数(105)。(The invention provides a control system. The invention provides a control system (100) operable to provide an aircraft with modified master control parameters, the control system (100) comprising: a main control parameter branch configured to output a demand in a main control parameter (103) of the aircraft; a main control parameter compensation branch configured to receive a detected change (107) of the swirl angle and/or of the absolute horizontal and/or spatial distribution of the fan pressure at a main control parameter relative to a reference and to convert the detected change (107) into a change of the main control parameter (106); and a processor adapted to: receiving a demand in the main control parameter (103) output from the main control parameter branch and a change in the main control parameter (106) output from the main control parameter compensation branch; comparing the demand in the main control parameter (103) output from the main control parameter branch with the change in the main control parameter (106) output from the main control parameter compensation branch; and generating modified master control parameters for the aircraft (105).)