CONTINUOUS HIGH-ACCURACY LOCATING METHOD AND APPARATUS

• US 20110273324A1
• Filed: 04/13/2011
• Published: 11/10/2011
• Est. Priority Date: 04/22/2010
• Status: Abandoned Application

• Current Assignee: Eurocopter
• Original Assignee: Eurocopter
• Inventors: Petillon, Jean-Paul
• Application Number:
  US13/085,770
• Publication Number:
  US 20110273324A1
• Time in Patent Office: Days
• US Class Current: 342/118
• CPC Class Codes: G01S 13/878 Combination of several spaced transmitters or receivers of known location for determining the position of a transponder or a reflector G01S13/874 takes precedence

Abstract

Method and apparatus for locating an object (2) that is to be located relative to a reference object (1), by electrically generating a locating signal (SL) by modulating a carrier signal with pseudo-noise. The modulation is continuous and of the ultra-wideband (UWB) type. Analysis using a cross-correlation function between said locating signal (SL) and received reflected signals (SRR1, SRR2) serves to segregate waves that have followed a direct path and any interfering waves that have followed indirect paths, so as to be able to deduce therefrom the shortest overall propagation time corresponding to those of said locating waves (OL) that have followed direct paths. The invention applies in particular to a rotary wing aircraft, e.g. a helicopter drone.

Claims

1. A method of locating an object that is to be located relative to a frame of reference associated with a reference object, the method including electrically generating a locating signal by modulating a carrier signal with pseudo-noise, this modulation spreading the spectrum of said locating signal, said locating signal being transmitted in the form of locating waves using at least one wave transmitter, such locating waves being received and transformed into a received reflected signal of electrical form, the received reflected signal being processed so as to determine at least the propagation time of said locating wave, which propagation time is used to calculate a relative position for said objects;

wherein the method comprises the following steps;

electrically generating said locating signal and transmitting said locating wave from the reference object, the modulation of said carrier signal with said pseudo-noise being continuous and of the ultra-wideband (UWB) type;

reflecting said locating waves by reflector means situated on the object that is to be located;

receiving locating waves by at least two receiver means disposed on the reference object, each transforming the locating waves into a respective received reflected signal in electrical form;

analyzing the received reflected signals by means of a cross-correlation function between said locating signal and each of the received reflected signals, in order to segregate locating waves that have followed a direct path and any interfering locating waves that have followed indirect paths; and

deducing the shortest propagation time corresponding to those of the locating waves that have followed a path without interfering reflection.

2. A locating method according to claim 1, wherein in order to generate the locating signal electrically by modulation, the carrier signal and the pseudo-noise signal are in the microwave electromagnetic frequency range, and the UWB type modulation possesses a relative bandwidth substantially equal to 0.5.

3. A locating method according to claim 2, wherein the frequency of the carrier signal is substantially equal to 2.4 GHz, and the frequency of the pseudo-noise is substantially equal to 600 MHz.

4. A locating method according to claim 2, wherein the locating signal conveys information between the object that is to be located and the reference object, in particular locating information transmitted from the reference object to the object that is to be located.

5. A locating method according to claim 1, wherein in order to generate the locating signal electrically by modulation, the carrier signal and the pseudo-noise lie in the acoustic frequency range of the ultrasound type, being equal to at least about 20 kHz.

6. A locating method according to claim 1, wherein when the locating waves are reflected by active reflector means in the acoustic frequency range, a frequency change is performed within the locating signal in order to avoid interfering coupling by the Larsen effect.

7. A locating method according to claim 1, wherein the locating wave is transmitted in the form of light.

8. A locating apparatus for locating an object that is to be located relative to a frame of reference associated with a reference object, wherein the locating apparatus is designed to implement the method according to claim 1.

9. A locating apparatus according to claim 8, wherein the object for locating is an aircraft, and the reference object with which said reference frame is associated is a ship.

10. A locating apparatus according to claim 9, wherein the object for locating is the center of an area for landing on the deck of a ship and the reference object associated with said reference frame is an aircraft.

11. A locating apparatus according to claim 8, wherein said reflector means are of the active type.

12. A locating apparatus according to claim 8, wherein said reflector means are of the passive type, in particular of the retroreflector type for a locating light-wave, or of the cube corner reflector type for a microwave electromagnetic locating wave.

13. A locating apparatus according to claim 8, wherein when transmission is performed in the form of microwave electromagnetic waves, transmitters and receivers for said locating waves both on the reference object and on the object that is to be located are constituted respectively by transmitter and receiver antennas.

14. A locating apparatus according to claim 8, wherein when transmission is performed in the form of acoustic waves, a transmitter and sensors of said locating waves on the reference object and on the object that is to be located are respectively a transmitter loudspeaker and receiver microphones.

15. An aircraft of the type for implementing the method according to claim 1, wherein the aircraft is a rotary wing aircraft.