Patent ID: 11874114
Assignee: MDGROUP GERMANY GMBH
Field: Control (Instruments)
Classification: CPC G  B | IPC B  G

Claim 8:
9. A control system for an aircraft comprising a computing unit that matches an intended flight position of the aircraft against an item of geographical elevation information that corresponds to the intended flight position, wherein the item of geographical elevation information is taken from a set of items of elevation information that corresponds to a geographical area including a flight route between a present position of the aircraft and a target position of the aircraft, wherein the set of items of elevation information indicates, for a first part of the geographical area, an actual item of geographical elevation information and, for a second part of the geographical area, an item of elevation information that differs from the actual geographical elevation information, wherein the second part of the geographical area includes a first special area in which the aircraft may only be operated under a restriction specifying a noise-reduced operation of the aircraft or a maximum or minimum flight speed of the aircraft, and wherein the item of elevation information differing from the actual geographical elevation information is evaluated in order to actuate an operating component of the aircraft such that the aircraft complies with a specified limit value for noise emission or flight speed included in the restriction when the aircraft is operated in the first special area.