System and method for assisting in the decking of an aircraft

1. A system for assisting in decking of an aircraft on a mobile platform, said mobile platform comprising a decking surface, said aircraft comprising a signal transmitter, and said decking surface of the mobile platform reflecting electromagnetic waves of signals transmitted by the signal transmitter of the aircraft, the system comprising:

means for determining flight commands to be executed by the aircraft, said means being configured to determine flight commands that dampen an impact of the aircraft on said mobile platform during the decking of the aircraft, said commands being a function of a position of the aircraft determined by locating means and extrapolation of movements of the mobile platform determined by prediction means, the locating means comprising at least two passive sensors spaced apart and fixed in proximity to the decking surface, the at least two passive sensors being configured to receive signals transmitted by the signal transmitter of the aircraft, each of the at least two passive sensors being a panel fixed in a plane orthogonal to the decking surface, each panel comprising antenna receivers distributed in the two dimensions of the plane of each panel, each panel being inclined about an axis orthogonal to the decking surface, and lighting beams of said panels intersecting at an azimuth angle above the decking surface.

2. The system according to claim 1 , wherein the antenna receivers of each panel are planar antennas assembled in blocks, the blocks being oriented, in the plane of each panel, identically for all of the sensors, and the blocks being distributed along the length of each panel.

3. The system according to claim 1 , wherein the mobile platform further comprises one or more side walls reflecting the electromagnetic waves, and wherein each panel is inclined about an axis orthogonal to the plane of said panel, at an angle α formed with the vertical of between 20° and 70°.

4. The system according to claim 1 , further comprising a local oscillator linked to the at least two passive sensors to produce a radio-interferometer that is configured to be applied to the signals transmitted by the signal transmitter of the aircraft.

5. The system according to claim 1 , wherein each of the at least two passive sensors is an optical camera.

6. The system according to claim 1 , further comprising a reference beacon joined to the mobile platform, the reference beacon oriented to transmit signals towards the at least two passive sensors.

7. The system according to claim 1 , wherein the aircraft is unmanned and able to be automatically guided remotely.

8. A method for assisting in decking of an aircraft on a mobile platform, at least two passive sensors being joined to said mobile platform, said mobile platform comprising a decking surface, said decking surface of the mobile platform reflecting electromagnetic waves of signals transmitted by a signal transmitter of the aircraft, each of the at least two passive sensors being a panel comprising antenna receivers distributed in the two dimensions of the plane of each panel, and each panel being inclined about an axis orthogonal to a plane of each panel, the method comprising:

transmitting signals from the aircraft;

receiving, by at least two passive sensors joined to the platform, the signals transmitted by the aircraft;

determining a position of the aircraft based on the received signals;

expressing the coordinates of the position of the aircraft relative to a frame of reference corresponding to an immobile platform;

predicting movements of the mobile platform;

formulating flight commands to orient the aircraft on its decking trajectory using the coordinates of the position of the aircraft and the predicted movements of the mobile platform to dampen an impact of the aircraft on the mobile platform during the decking of the aircraft; and

eliminating multiple paths in elevation and in azimuth by performing a spatial sampling of an amplitude of an interference signal received by at least one sensor in an elevation axis and by performing a spatial sampling of an amplitude of the interference signal received by at least one sensor in the azimuth axis.

9. The method according to claim 8 , wherein:

each panel is inclined about an axis orthogonal to a plane of each panel, by an angle α formed with the vertical of between 20° and 70°.

10. The method according to claim 8 , wherein the mobile platform transmits data through a radiofrequency channel to the aircraft using a transmitter, a power level for transmission by said transmitter being adjusted according to a distance measured between said mobile platform and the aircraft, such that the transmission power is reduced as the aircraft approaches the mobile platform.

11. The method according to claim 8 , wherein, for each of the at least two passive sensors, the position of the aircraft is determined by triangulation of measurements obtained from at least two passive sensors, and the independently determined positions of the aircraft are combined to improve reliability of the determination of the position of said aircraft.

12. The method according to claim 8 , wherein the signals transmitted from the aircraft and received by the at least two passive sensors of the mobile platform are single-frequency signals transmitted in band X or signals comprising a frequency-based comb of rays.

13. The method according to claim 8 , wherein formulating the flight commands to orient the aircraft on its decking trajectory comprises receiving navigation data obtained from aircraft instruments.