| 摘要 |
The present invention relates to an active inceptor system for controlling an aircraft with at least one mechanically movable inceptor, at least one control of at least one control element or actuator for actuating the inceptor, and at least one detection means for detecting at least one state variable of the inceptor, wherein the active inceptor comprises at least one controller for actuating at least one control element or actuator and at least one feel generating means, wherein the feel generating means combines inner and/or outer state variables and a control setpoint variable can be determined with the aid of one or more physical-mathematical models. |
