The present invention relates to an image enhancer for detecting and identifying objects in turbid media. More specifically, but without limitation, the present invention relates to a laser system that can detect and identify objects in turbid media.
Laser systems have been and are continuing to be developed to detect and identify objects in turbid media (examples of turbid media include, but without limitation, seawater, clouds, and tissue). Operating a laser imaging system in such an environment is challenging due to the fact that light is both absorbed and scattered. Although the optical wavelength is typically selected to minimize absorption, the scattering experienced by an optical signal can severely degrade image quality. In highly turbid media, there may be plenty of light scattered back from the object of interest, but it is buried in the signal returning from the surrounding environment. A method for separating the unscattered (or minimally scattered) image bearing photons from the scattered, background light can be used to improve object detection and identification.
Several techniques have been developed for reducing the detrimental effects of scattered light. These approaches can be categorized according to the type of laser source and receiver combination and the scanning method used to create the image. All these types of systems are capable of creating an image, whether it is a synchronously scanned narrow beam and a narrow receiver field of view (narrow-narrow) or a flood-illuminated scene with a multiple pixel receiver (wide-narrow). The decision as to which configuration provides the best performance depends directly on the task at hand (i.e., above-water or below-water operation, size and depth of underwater object, water optical properties, etc.).
One type of known system is the Laser Line Scan (LLS) system. The Laser Line Scan (LLS) system includes a well-collimated continuous wave source and a narrow field of view receiver that are synchronously scanned over the object of interest. The bistatic configuration limits the common volume created by the source and receiver field of view overlap and reduces the contribution from scattered light. However, since the system uses a continuous wave source, no inherent time (depth) information is present in the detected signal, and post-processing using triangulation methods must be used to obtain object range information.
Pulsed laser sources are also used in several underwater laser-imaging systems to temporally discriminate against scattered light and to provide object range information. In the operation of a typical range-gated imaging system, a short (10-20 nsec) pulse is transmitted to a distant object, and the receiver is timed to open only when the reflected light returns from the object. A typical configuration is broad-beam illumination of the scene and a gated intensified camera receiver, although systems using photomultiplier tube receivers in both single and multiple pixel configurations have also been utilized. The Streak Tube Imaging Lidar (STIL) uses a pulsed laser transmitter in a ‘scannerless’ configuration. Instead of scanning the laser beam, a fan of light is used to illuminate a volume of water. The streak tube receiver can measure both the amplitude and range (time) of the collected slit of light, and a three-dimensional image is created when the system is operated from a moving platform. While the range-gated and STIL approaches are effective in minimizing background light, the sensitivity is ultimately limited by small-angle forward scattered light that induces image blurring.
Another type of underwater imager encompasses those that use temporal modulation of the transmitted light and subsequent synchronous detection of the modulation envelope at the receiver. The Underwater Scannerless Range Imager (USRI) uses a radio frequency modulation source that is coupled to both the timing of the laser transmitter and the gain of the image intensified CCD receiver. Object range information is obtained by measuring the phase difference between the transmitted and reflected signals simultaneously for each pixel of the receiver. However, multiple frames are required using different modulation schemes in order to extract the range information and to differentiate changes due to range variations from those due to intensity variations in the scene. Previous configurations used continuous wave sources, but a recent configuration implements a pulsed source and a range-gated receiver to minimize the volumetric backscatter signal.
Researchers at the Naval Air Systems Command (NAVAIR) are also developing a system that uses temporal modulation of the transmitted optical signal. However, in this approach, the optical receiver consists of a photodetector with sufficient bandwidth to recover the modulation envelope encoded on the optical signal. The resulting radio frequency signal is then processed using traditional radar signal processing techniques. This approach reduces the contribution by volumetric backscatter by using a modulation frequency that becomes strongly decorrelated with respect to the transmitted signal due to multiple scattering. A gain in image contrast is achieved when the modulation envelope emanating from an underwater object remains coherent relative to the original modulation signal. The phase information encoded on the detected modulation signal is processed to obtain object range information.
In previous embodiments of this modulated imaging system approach, a spectrum analyzer was used to produce the signal and the system produced a so-called “magnitude” image that was shown to have a nonlinear dependence on the object albedo (the term albedo may be defined, but without limitation, as ratio of the amount of electromagnetic energy reflected by a surface to the amount of energy incident upon it or the fraction of radiation striking a surface that is reflected by that surface). This non-linearity created a variety of sometimes unexpected features, such as contrast inversion, appearance of false elements in the image patterns, and the “emphasizing of the outlines” in object albedo patterns. In this system configuration, the irradiance distribution in the image plane is not proportional to the actual reflectivity of the object, the image is distorted, and its identification is difficult if impossible. This non-linearity is the main drawback of the conventional “magnitude” signal registration of previous system configurations.
For the foregoing reasons, there is a need for an image enhancer for detecting and identifying objects in turbid media.
The present invention is directed to an image enhancer that meets the needs enumerated above and below.
The present invention is directed to an image enhancer for detecting and identifying objects in turbid media. The image enhancer includes a laser for emitting an optical signal toward an object in a turbid medium, a modulator for modulating laser intensity of the laser, an RF source for driving the modulator and for providing a reference signal, an optical detector for detecting the modulated optical signal that is reflected from the object, the optical detector converting the reflected optical signal into an electrical signal, the electrical signal having RF and DC components, an I/Q demodulator for mixing the RF component of the electrical signal with the reference signal and producing in-phase and quadrature phase signal components that can be filtered, digitized, and processed such that both contrast and range images of the object are produced.
It is a feature of the present invention to provide an image enhancer that provides a clearer image of an object in turbid media.
It is a feature of the present invention to provide an image enhancer wherein the image is linear with respect to the object albedo.
It is a feature of the present invention to provide an image enhancer wherein the phase of the RF reference signal is matched to the backscatter phase.
It is a feature of the present invention to provide an image enhancer wherein modulation frequency is chosen so that the backscatter and subject signals can be analyzed separately at the receiver.
These and other features, aspects and advantages of the present invention will become better understood with reference to the following description and appended claims, and accompanying drawings wherein:
a is the uncorrected range image computed using Equation 11, and
The preferred embodiments of the present invention are illustrated by way of example below and in
In the description of the present invention, the invention will be discussed in a turbid environment, specifically water; however, this invention can be utilized for any type of need that requires use of an image enhancer. The image enhancer 10 may be used, but without limitations, in military operations, search missions, and biomedical imaging in tissue.
As shown in
In another embodiment of the invention, the DC component 70 of the electrical signal 65 is passed through a third low pass filter 610. The filtered DC component 71 may then be digitized simultaneously with the filtered in-phase signal component IF and the filtered quadrature phase signal component QF. The filtered DC component 71 is indicative of the baseline performance of an imager without modulation and is used for comparison purposes.
The operation of the preferred I/Q demodulator 500 can be best described by referring to
where AOBJ and ABSN are the amplitudes of the object signal and backscatter signal respectively, ω is the radial frequency, t is time, and φOBJ and φBSN are the corresponding phases of the object and background (in a given medium).
The I/Q demodulator 500 may also include a zero degree splitter 505, a ninety degree splitter 510, a first mixer 515 and a second mixer 520. The splitters and mixers may be digital, analog or any type practicable. The zero degree splitter 505 separates the ARF(t) signal (the RF component 66 of the electrical signal 65) into equal components (0.5 ARF(t)) that are applied to the two different mixers (515 and 520). The reference signal 50 (ALO(t)) produced by the RF source 300 is also input to the I/Q demodulator 500, and can be described by the following equation:
A
LO(t)=ALO sin(ωt+φLO), (Equation 3)
wherein ALO is the amplitude of the reference signal 50, ω is the radial frequency, t is time, and φLO is the corresponding phase of the reference signal 50. The reference signal 50 is phase-locked to the radio frequency signal that is used to modulate the laser 100. The ninety degree splitter 510 separates the ALO (t) signal (the reference signal 50) into two components—an in-phase reference signal portion 51 and an out-of-phase reference signal portion 52. The in-phase reference signal portion 51 (described as 0.5 ALO sin(ωt+φLO)) is in-phase with the original ALO(t) signal or reference signal 50, and the out-of-phase reference signal portion 52 (described as 0.5 ALO cos(ωt+φLO)) is ninety degrees out of phase with the original signal or reference signal 50. One of the in-phase components of the ARF(t) signal, (0.5 ARF(t)), and the in-phase reference signal portion 51 (0.5 ALO sin(ωt+φLO)) are mixed by the first mixer 515. The first mixer 515 may be a RF mixer. The output from the first mixer 515 may then be passed through the first low-pass filter 600 to produce the filtered in-phase signal component IF. The following equation describes the filtered in-phase signal component IF (assuming a lossless I/Q demodulator and a lossless low pass filter):
I
F=0.125ALO[AOBJ cos(φOBJ−φLO)+ABSN cos(φBSN−φLO)]. (Equation 4)
The quadrature phase signal component Q is produced by mixing the other in-phase component of the ARF(t) signal (0.5 ARF(t)) with the ALO(t) signal component that is ninety degrees out of phase (the out-of-phase reference signal portion 52 and it is described as 0.5 ALO cos(ωt+φLO)). The other in-phase component of the RF component 66 of the electrical signal 65 (0.5 ARF(t)) and the out-of-phase reference signal portion 52 are mixed by the second mixer 520. The output from the second mixer 520 may then be passed through the second low-pass filter 605 to produce the filtered quadrature phase signal component QF. The following equation describes the filtered quadrature phase signal component QF (assuming a lossless I/Q demodulator and a lossless low pass filter):
Q
F=0.125ALO[AOBJ sin(φOBJ−φLO)+ABSN sin(φBSN−φLO)]. (Equation 5)
The filtered in-phase signal component IF and the filtered quadrature phase signal component QF are then digitized simultaneously by the analog-to-digital converter 700 and processed by the data processor 800, such that contrast and range images are produced.
The main advantage of using the I/Q demodulator 500 instead of a spectrum analyzer (or other types of components) used in previous system configurations can be understood by studying the equations relevant to the two receiver approaches. The signal that is captured when using the previous spectrum analyzer approach is the magnitude, M, of the detected RF signal (the detected signal 60):
M=√{square root over (I2+Q2)}∝√{square root over (AOBJ2+ABSN2+2AOBJABSN cos(φOBJ−φBSN))}. (Equation 6)
It is evident from Equation 6 that the magnitude is nonlinear with respect to the object return amplitude, AOBJ, except when φOBJ−φBSN=0, π. However, upon looking at Equations 4 and 5, it is clear that the filtered in-phase signal component IF and the filtered quadrature phase signal component QF (as well as the unfiltered signal components) are linear with respect to AOBJ. Furthermore, the reference signal phase, φLO, can be varied to optimize the images produced with the filtered in-phase signal component IF and the filtered quadrature phase signal component QF. For example, when φLO=φBSN,
I
F=0.125ALO[AOBJ cos(φOBJ−φBSN)+ABSN]
Q
F=0.125ALOAOBJ sin(φOBJ−φBSN). (Equations 7 and 8)
While the filtered in-phase signal component IF still contains both object (AOBJ) and backscatter (ABSN) amplitude components, the filtered quadrature phase signal component QF contains only the object amplitude component, AOBJ. Furthermore, if a modulation frequency is chosen so that the object and backscatter signals are ninety degrees out of phase (φOBJ−φBSN=nπ/2, where n is an odd integer), then:
I
F=0.125ALOABSN
Q
F=0.125ALOAOBJ. (Equations 9 and 10)
In this case, the filtered in-phase signal component IF is dependent on the backscatter amplitude, and the filtered quadrature phase signal component QF is directly proportional to the object amplitude. Therefore, this approach enables us to separate the object and backscatter signal components from the composite return signal. This was not possible with the previous inventions that measured only the return signal magnitude, which is independent of the reference signal phase and contains both object and backscatter components.
The method for selecting the modulation frequency is based upon observing the frequency dependence of the magnitude of the RF signal, M(f). In the past, it was observed in both experimental and computer simulation results that under certain conditions, maxima and minima were observed in the dependence of M on the modulation frequency. The cause of these signal amplitude fluctuations as a function of modulation frequency was found to be due to constructive and destructive interference of the modulation envelope between the backscatter and object return signals. Therefore, the features of M(f) are dependent on the phase difference between the object and backscatter return signals, φOBJ−φBSN. This is shown in
To illustrate the advantages of the current invention, experimental results obtained using the old methods and the current invention will now be compared. The results obtained without modulation will also be shown to provide a baseline performance level. The target or object 20 used for these measurements was a flat piece of metal with a ‘bulls eye’ pattern and is shown in
An additional advantage of the new approach is that it has the potential to enhance the accuracy of the phase calculated from the in-phase signal component I and the quadrature phase signal component Q:
φRF−φLO=tan−1(Q/I) (Equation 11)
where φRF is the phase of the composite return signal and φLO is the reference signal phase. This phase measurement capability is useful when imaging three-dimensional objects where φOBJ varies as a function of position across the object surface. However, upon examination of the equations of the filtered in-phase signal component IF and the filtered quadrature phase signal component QF (Equations 4 and 5), it is clear that there are two phase terms: one for the object, φOBJ−φLO, and one for the backscatter, φBSN−φLO. To isolate the object phase term, the effect of the backscatter must be removed. This can be accomplished using the new approach described previously. By selecting a reference point so that φLO=φBSN and φBSN=φOBJ−nπ/2 (for odd integer n), the backscatter phase term is removed and the backscatter amplitude can be determined (Equations 9 and 10). The object phase can then be calculated by
The range measurements calculated using Equations 11 and 12 for the flat target (the object 20) images shown in
The method for detecting and identifying objects in turbid media includes emitting an optical signal toward an object in a turbid medium, modulating the optical signal, providing a reference signal, detecting a portion of the modulated optical signal that is reflected from the object, converting the portion of the modulated optical signal into an electrical signal, separating the electrical signal into its RF and DC components, mixing the RF component of the electrical signal with the reference signal, producing an in-phase signal component and a quadrature phase signal component from the mixed signals, and filtering, digitizing and processing the in-phase signal component and the quadrature phase signal component such that contrast and range images of the object are produced.
In the preferred embodiment of the method, the in-phase signal component and the quadrature phase signal component are filtered prior to being digitized and processed. Additionally, the method may include separating the reference signal into an out-of-phase reference signal portion and to an in-phase reference signal portion, mixing half of the RF component of the electrical signal with the out-of-phase reference signal portion such that the quadrature phase signal component is produced, and mixing the other half of the RF component of the electrical signal with the in-phase reference signal portion such that the in-phase signal component is produced. The preferred method utilizes the above described equations and calculations.
When introducing elements of the present invention or the preferred embodiment(s) thereof, the articles “a,” “an,” “the,” and “said” are intended to mean there are one or more of the elements. The terms “comprising,” “including,” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements.
Although the present invention has been described in considerable detail with reference to a certain preferred embodiments thereof, other embodiments are possible. Therefore, the spirit and scope of the appended claims should not be limited to the description of the preferred embodiment(s) contained herein.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without payment of any royalties thereon or therefor.