Method and system for the detection and measurement of air phenomena and transmitter and receiver for use in the system

• US 5,534,868 A
• Filed: 09/23/1994
• Issued: 07/09/1996
• Est. Priority Date: 03/26/1992
• Status: Expired due to Term

• Current Assignee: Susar A/S
• Original Assignee: Susar A/S
• Inventors: Gjessing, Dag K., Hjelmstad, Jens F.
• Primary Examiner(s): Sotomayor, John B.
• Application Number:
  US08/307,688
• Time in Patent Office: 655 Days
• Field of Search: 342/26, 342/460
• US Class Current: 342/26.00D
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 13/951 ground based
• CPC Class Codes: G01W 2001/003 Clear air turbulence detection or forecasting, e.g. for aircrafts
• CPC Class Codes: Y02A 90/10 Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Abstract

A system and method for the detection and measurement of atmospheric air movement irregularities such as wind velocity vector, clear air turbulence, aircraft induced vorteces and turbulence, by means of electromagnetic waves. An air volume (10) under investigation is illuminated by a transmitter (1, 1A, 1B) with a beam of coherent electromagnetic energy (1E), and a resulting wave field (2E) is received and subsequently coherently demodulated and processed in process means to derive information on the existence of the said atmospheric irregularities and furthermore to give specific measurements of related parameters. At least one receiver (2, 2A, 2B) for said resulting wave field (2E), which is due to scattering in said air volume (10), is positioned at a bistatic location having a selected distance (2R) from said transmitter (1, 1A, 1B). Said electromagnetic energy (1E) is transmitted at microwave frequencies in a concentrated beam. Transmitter and receiver antennas (1A, 1B, 2A, 2B), respectively, are directed so as to cover said air volume (10) with a scattering angle (Θ) chosen to have such a (low) value that scattering from atmospheric irregularities in said air volume (10) has a higher power than noise sources in the system.

Claims

1. A system for detecting and measuring atmospheric air movement conditions such as wind velocity vectors, clear air turbulence and aircraft-induced vortices and turbulence, comprising:

a transmitter for irradiating a selected volume of air with a coherent electromagnetic energy beam in the microwave frequency range;

at least one receiver, positioned at a location separated from said transmitter by a preselected distance, for receiving and coherently demodulating a scattered electromagnetic energy beam resulting from scattering of said coherent electromagnetic energy beam in said selected volume of air to develop a demodulated signal, wherein said transmitter and at least one receiver each comprise a local oscillator locked to a common reference which is independent of said irradiated electromagnetic energy beam; and

processor means for processing said demodulated signal from said at least one receiver and deriving quantitative information on said atmospheric air movement conditions therefrom;

wherein antennas of said transmitter and said at least one receiver are directed such that a scattering angle θ

of said scattered electromagnetic energy beam is small enough for said scattered electromagnetic energy beam to have a higher power than noise sources in the system.

2. A system according to claim 1, wherein said scattering angle θ

is smaller than 20°

.

3. A system according to claim 1, wherein at least one of the transmitter and receiver antennas are arranged such that radiated power in the direction of the other of said antennas is suppressed to reduce direct leakage of electromagnetic energy between said transmitter and said at least one receiver.

4. A system according to claim 1 or claim 3, wherein at least one of said transmitter and receiver antennas are adapted to be steered to provide a two- or three-dimensional map of said atmospheric conditions, and in particular of windshear conditions.

5. A system according to claim 1, wherein said transmitter and at least one receiver each comprise a local oscillator locked to a GPS signal as to a common reference.

6. A system according to claim 1, wherein said transmitter comprises means for transmitting at least two coherently related microwave frequencies.

7. A system according to claim 6, wherein said transmitter comprises spatially separated antennas for transmitting said coherently related microwave frequencies.

8. A system according to claim 6, wherein said transmitter comprises a single antenna for transmitting said coherent related microwave frequencies.

9. A system according to claim 6, wherein said processor means comprises narrow bandpass filter means for forming two receiver channels for said two transmitted frequencies.

10. A system according to claim 6, wherein said at least one receiver has a separate receiving aperture and separate bandpass filter for each transmitted frequency, and said processor means comprises a signal processor for multiplying a homodyned signal from said at least one receiver at each transmitted frequency to generate a time series signal having a spectrum which gives the directional Doppler shift of said scattered energy beam in any plane through said selected volume of air.

11. A system according to claim 10, wherein said at least one receiver comprises a coherent homodyne demodulator for each transmitted frequency that gives a directional Doppler shift.

12. A system according to claim 10, wherein said at least one receiver comprises a plurality of receiving apertures and a coherent homodyne demodulator for each aperture.

13. A system according to claim 1, wherein said processor means comprises means for performing Delta-K processing to achieve one-, two- or three-dimensional wave number representation of a scattering distribution in said selected volume of air.

14. A system according to claim 1, wherein said processor means comprises means for generating a visual image of said atmospheric conditions through use of an inversion algorithm.

15. A method for detecting and measuring atmospheric air movement conditions such as wind velocity vectors, clear air turbulence and aircraft-induced vortices and turbulence, comprising the steps of:

irradiating from a transmission location a selected volume of air with a coherent electromagnetic energy beam in the microwave frequency range;

receiving and coherently demodulating at a location separated from said transmission location by a preselected distance, a scattered electromagnetic energy beam resulting from scattering of said coherent electromagnetic energy beam in said selected volume of air to develop a demodulated signal, said demodulating being performed with reference to a common reference independent of said coherent electromagnetic energy beam; and

processing said demodulated signal and deriving quantitative information on said atmospheric air movement conditions therefrom;

wherein a scattering angle θ

of said scattered electromagnetic energy beam is chosen to be small enough for said scattered electromagnetic energy beam to have a higher power than noise sources in the system.