Abstract: The invention relates to a method for determining the phase difference between a first clock signal (CK1) received by a first electronic component (CE1) and a second clock signal (CK2) received by a second electronic component (CE2), comprising the steps of: S10) transmitting a first calibration signal (S12); S20) measuring a first delay (T1); S30) transmitting a second calibration signal (S21); S40) measuring a second delay (T2); S50) measuring the number (n) of clock pulses between the transmission of the first calibration signal (S12) and the active edge of the first clock signal (CK1) consecutive to the active edge of the second calibration signal (S21); S60) determining the phase difference depending on the parity of the number (n) of clock pulses.

Abstract: Provided is an aircraft having a spherical body which generates buoyancy or which may generate buoyancy when filled with gas, wherein the aircraft further comprises four actuation units arranged on the surface of the body for movement of the aircraft in a translation and/or rotation through air, and at least one camera arranged on or in the surface of the body. Further provided is a method for providing optical information to a person in the environment of a flying aircraft, a method for providing optical information about an object and/or surveying of an object, a method for transmission of acoustic information and a method for observing or tracking an object.