초록 ▼

A system and method for detecting turbulence includes several mobile platforms, a mobile platform velocity sensor, and several electromagnetic energy transmitters and receivers. The receivers receive the energy transmitted by the transmitter(s) after it has traveled along a path subject to the turbu

A system and method for detecting turbulence includes several mobile platforms, a mobile platform velocity sensor, and several electromagnetic energy transmitters and receivers. The receivers receive the energy transmitted by the transmitter(s) after it has traveled along a path subject to the turbulence. The receivers detect alterations of the energy caused by the turbulence and filter the alterations for effects of the mobile platform velocity (on which either a transmitter or receiver is located). Additionally, the system may create a three-dimensional model of the. In another preferred embodiment, the present invention provides a method of detecting turbulence using a mobile platform. The method includes receiving electromagnetic energy that has traveled along a path subject to the turbulence and determining the alteration to the energy caused by the turbulence. The alterations are filtered of the effects of the velocity of the mobile platform on which the receivers are preferably located.

대표청구항 ▼

What is claimed is: 1. A mobile platform comprising a receiver configured with at least two antennas to: receive a plurality of signals from a plurality of signal sources remote from the platform along a plurality of paths; condition the received signals to obtain one or more signals representative

What is claimed is: 1. A mobile platform comprising a receiver configured with at least two antennas to: receive a plurality of signals from a plurality of signal sources remote from the platform along a plurality of paths; condition the received signals to obtain one or more signals representative of clear air turbulence; condition one of the received signals to obtain a global positioning signal; determine directions to the signal sources; use the directions to obtain time varying vectors representing air conditions along the signal paths; and use the time varying vectors to locate the turbulence. 2. The mobile platform according to claim 1, wherein at least one signal source is included in a positioning system. 3. The mobile platform according to claim 1, wherein the receiver and at least one antenna are further configured to reject a portion of the received signal to obtain the positioning signal, and use the rejected portion to obtain a signal representative of the turbulence. 4. The mobile platform according to 1, wherein to obtain a signal representative of the turbulence, the receiver and at least one antenna are configured to: detect an alteration in a received signal; use the alteration to obtain an indication of the turbulence; and adjust the turbulence indication to account for motion of the platform. 5. The mobile platform according to claim 4, wherein the receiver and at least one antenna are further configured to: use at least one signal representing the platform motion in six degrees of freedom to determine motion-induced phase and frequency shifts in the received signal; and use the shifts to adjust the turbulence indication. 6. The mobile platform according to claim 4, wherein the receiver and at least one antenna are further configured to: use at least two frequencies received from one of the signal sources to detect an effect of ionospheric scintillation on the received signal from the one of the sources; and filter the detected effect from the turbulence indication. 7. The mobile platform according to claim 1, wherein the mobile platform is an aircraft. 8. The mobile platform according to claim 1, comprising first and second antennas, the receiver and antennas further configured to: use a velocity of the platform and a distance between the first and second antennas to determine a time delay between receiving of a given received signal by the first antenna and receiving of the given received signal by the second antenna; use the time delay to determine a coefficient of correlation between turbulence indications from the first and second antennas; and use the coefficient of correlation to minimize error in the turbulence indications. 9. An aircraft comprising a receiver configured with at least two antennas to: receive two or more signals from two or more signal sources remote from the aircraft along two or more paths; smooth one of the the received signals to obtain a positioning signal; use the unsmoothed received signals to obtain one or more signals representative of clear air turbulence; determine directions to the signal sources; use the directions to obtain time varying vectors representing air conditions along the signal paths; and use the time varying vectors to locate the turbulence. 10. The aircraft according to claim 9, the receiver and at least one antenna further configured to: detect a magnitude and rate of an alteration in one of the unsmoothed received signals; and convert the detected magnitude and rate to an indication of the turbulence. 11. The aircraft of claim 10, wherein the alteration comprises a change in one or more of the following: phase, frequency, and intensity. 12. The aircraft of claim 10, wherein the receiver and at least one antenna are further configured to: determine a frequency shift and/or phase shift in at least one signal representing linear and rotational movement of the aircraft; and adjust the turbulence indication based on the frequency shift and/or phase shift. 13. The aircraft of claim 10, wherein the receiver and at least one antenna are further configured to: invert a signal representing ionospheric scintillation detected in one of the received signals; and apply the inverted signal to the turbulence indication. 14. The aircraft of claim 9, comprising first and second antennas, the receiver and antennas further configured to: use a velocity of the aircraft and a distance between the first and second antennas to determine a time delay between receiving of a received signal on the same path by the first and second antennas; use the time delay to determine a coefficient of correlation between turbulence indications from the first and second antennas; and use the coefficient of correlation to minimize error in the turbulence indications. 15. An aircraft comprising a receiver configured with at least two antennas to: receive two or more signals from two or more satellites along two or more paths; smooth one of the the received signals to obtain information for an application on the aircraft; use the unsmoothed received signals to obtain one or more signals representative of clear air turbulence; determine directions to the satellites; use the directions to obtain time varying vectors representing air conditions along the signal paths; and use the time varying vectors to locate the turbulence. 16. The aircraft of claim 15, wherein a received signal provides information relating to one or more of the following: positioning, weather, and communication. 17. The aircraft of claim 15, wherein one of the satellites is included in a positioning system, the receiver and at least one antenna further configured to: reject a portion of the received signal from the one of the satellites to obtain a positioning signal; and use the rejected portion to obtain a signal representative of the turbulence. 18. The aircraft of claim 15, comprising first and second antennas, the receiver and antennas further configured to: correlate signals received from the antennas to reject signal variation from satellite timing error; and use the correlation to minimize error in a signal representative of the turbulence. 19. The aircraft of claim 15, the receiver and at least one antenna further configured to: detect an alteration in a received signal; use the alteration to obtain an indication of the turbulence; and adjust the turbulence indication to account for ionospheric scintillation and motion of the aircraft. 20. The aircraft of claim 19, wherein to account for motion of the aircraft comprises to use at least one signal representing linear and rotational movement of the aircraft in six degrees of freedom to determine a motion-induced frequency shift and/or phase shift in a received signal.