Abstract: For reducing a risk potential of an aircraft, a safety device for the aircraft is provided, said aircraft having a flight control device for flight control of the aircraft based on global position coordinates and/or flight altitude values of the aircraft detected by a sensor apparatus of the flight control device. The safety device comprises a flight altitude detection apparatus configured to detect a current flight altitude of the aircraft independently of the sensor apparatus, a determination apparatus configured to determine whether the current flight altitude of the aircraft detected by the flight altitude detection apparatus exceeds a predetermined maximum altitude, and a rescue apparatus configured to interrupt the flight control of the aircraft when the current flight altitude of the aircraft detected by the flight altitude detection apparatus exceeds the predetermined maximum altitude.

Abstract: According to the present invention, a method and a device for determining a physical quantity at a plurality of locations are provided. The method according to the invention comprises approaching the plurality of locations in a first predetermined direction, wherein at each location of the plurality of locations a first measured value of the physical quantity is measured, approaching the plurality of locations in a second predetermined direction substantially opposite to the first predetermined direction, wherein at each location of the plurality of locations a second measured value of the physical quantity is measured, and establishing a determination value for the physical quantity at a respective location of the plurality of locations based on the first and second measured values of the physical quantity which have been measured at the respective location.

Abstract: In accordance with the invention, a flying machine is provided comprising at least two passive lift elements arranged substantially radial-symmetrically about a yaw axis of the flying machine, wherein the passive lift elements are configured to jointly generate a torque at the yaw axis upon movement of the flying machine substantially in parallel to the yaw axis. The flying machine further comprises active lift generating means, which are arranged substantially at distal ends of the passive lift elements.