Certain sensor systems involve nonlinear sensors that utilize a known time-periodic bias signal to excite the sensors to oscillate. A target signal is detected by noting its effect on the sensor's oscillation level-crossing statistics. These sensing techniques are accurately represented via the dynamics of overdamped bistable systems; as such, their solutions (in the absence of any driving signals or noise) are those that decay rapidly to one of the stable steady states of the detector system. Yet, for nonlinear sensors to effectively serve as detectors of target signals, the sensors need to be operated as a device that switches between its stable attractors, thereby enabling one to quantify the target signal via its effect on the sensor switching dynamics. A bias signal that promotes this switching can be provided by a signal generator onboard the sensor system, however this can increase the power budget of the sensor as well as contribute to the sensor's noise floor.
A sensor system employing a plurality of nonlinear sensors utilizes a coupling network that interconnects the sensors to induce inherent oscillations in the sensor system. This approach replaces the need for bias signal generation either onboard the sensor system or via a source external to the sensor system.
Other objects, advantages and new features of the invention will become apparent from the following detailed description of the invention when considered in conjunction with the accompanied drawings.
A coupling network inherently induces oscillation in coupled non-linear sensors in the absence of an external bias signal or a signal generator signal provided onboard the employed sensors. As an example, by coupling a given number of nonlinear sensors using cyclic boundary conditions and uni-directional (one-way signal flow) coupling, one can generate oscillatory solutions past a critical value of coupling coefficient. Referring now to
{dot over (x)}1=−x1+tan h(c(x1+λx2+ε))
{dot over (x)}2=−x2+tan h(c(x2+λx3+ε))
{dot over (x)}3=−x3+tan h(c(x3+λx1+ε)) (1)
Notice that the (unidirectional) coupling term, having strength λ, (which in this example is assumed to be equal for all three elements) is inside the nonlinearity term, a direct result of the mean-field nature of the description (in the fluxgate magnetometer, the coupling is effectuated through the induction in the driving/excitation “pick up” coil of the magnetometer). In the equations above, xi(t) represents the magnetic flux in the ith magnetometer using suitably normalized units, and c is a (temperature-dependent) parameter for each magnetometer element. The individual dynamics of each element are bistable for c>1. For the equations above, state variables x1, x2, and x3 provide a way to introduce the initial conditions of the magnetometers. Finally, ε is a weak target signal that is provided as a magnetometer input. Typically, it is this signal that is desired to be detected.
A simple numerical integration of (1) (starting with non-identical initial conditions) reveals oscillatory behavior for λ<λc where λc is a critical threshold value of coupling strength. It will become apparent later that λc<0 in the convention adopted in (1). The oscillations are non-sinusoidal, with a frequency that increases as the coupling strength decreases away from λc. For λ>λc, however, the system quickly settles into a steady state that depends on the initial conditions. In experimentation, randomization of the initial conditions was found to easily occur due to inherent noise in the sensor system. Even a slight variation in the initial conditions, away from x1=x2=x3, will push the system into the oscillatory solution. For practical purposes, operational constraints (e.g. a noise-floor) will compel non-equal initial conditions.
For the system described by Eq. (1), we may use the underlying nonlinear dynamics to obtain the critical coupling strength parameter λc (for the onset of oscillations) as well as the oscillation frequency ω, in terms of the system and target signal parameters:
The summed oscillations are not sinusoidal. However, they tend to be sinusoidal for large coupling strength magnitude (λ<<λc; recall that λc<0). It is instructive to note that there is a precise 2π/3 phase difference between solutions, see
Numerical simulations and calculations with (3) show that ω is very sensitive to small changes in the target signal strength ε; in addition, the mean value of the oscillation amplitude is non-zero for finite ε. Both of these effects can be used to quantify a very weak “target” signal ε. A very small power source should suffice to sustain the oscillations once the sensor system initially oscillates.
The summed response X(t) of the sensors has been observed to be particularly sensitive to the presence of a target signal. Numerical simulations show that the mean amplitude of X(t) can be an order of magnitude or more in excess of the corresponding response of a single uncoupled sensor that is externally driven to generate oscillations similar to those shown in
In the presence of a noise-floor in each nonlinear sensor, one would expect not to observe a significant change (introduced solely by the noise) in the frequency ω, as long as the noise strength is much smaller than the energy barrier height in the absence of coupling, noting that the generated oscillations are suprathreshold. The noise-floor also provides needed non-identical initial conditions in the elements of the array.
The target signal may be quantified, for example, via the change in oscillation frequency of the sensor system as well as through a computation of the mean values <xi(t)> or <X(t)>, or even through spectral or level-crossing techniques.
Turning now to further details of
As can be seen, fluxgates 18n are coupled through electronic circuits 34n where the (voltage) readout of one fluxgate signal 20n (i.e. the derivative signal of the flux detected by the sensing coil of the fluxgate device) is amplified by differential voltage amplifier 24n (such as an instrumentation amplifier with a very high impedance). At this point, the amplifier may be used to trim out any d.c. in the fluxgate output. Following this, the signal is passed through an integrator 26n to convert the derivative signal seen by the sensing coil back to a “flux” form to conform this system closely to the model of equation (1). The use of a “leaky” integrator at this stage helps to minimize divergence caused by any small d.c. signal that might have leaked through the voltage amplifier stage. Typically, the output of the integrator is also accompanied by d.c. that is removed before the signal is passed to the other fluxgates. This is accomplished by employing a filter 28n such as a Sallen-Key second-order high pass filter. This filter is placed immediately after the integrator, with the filter parameters tuned to work at a specific frequency (the mean oscillating frequency of the coupled system). The signal then passes through amplifier 30n to achieve adequate gain to drive the downstream adjacent fluxgate. After this amplification stage, the signal passes through voltage-to-current converter (V-I converter) 32n in its final step to drive the primary (driving) coil of the next-in-line fluxgate. This converter also has a gain factor but it is set at a fixed value during the construction of the coupling circuits. The gain is set at much less than unity so that one volt in the signal does not convert to one ampere in the voltage-to-current converter stage.
As can be seen, the setup repeats for the other two coupling circuits for the remaining fluxgates and all values of the coupling circuit parameters are closely matched from one set to the other. Each stage of the coupling circuit also can be used with high speed and high precision operational amplifiers to further minimize time delay and to more closely conform the circuits to the model of equation (1) as knowledge of state variable xi is known in the model.
Referring now to
The phenomena described herein can be extended to a wide class of nonlinear dynamic sensor systems. For example, a system of coupled overdamped Duffing sensing elements described via quartic potentials:
{dot over (x)}1(t)=ax1−bx13+λ(x1−x2)
{dot over (x)}2(t)=ax2−bx23+λ(x2−x3)
{dot over (x)}3(t)=ax3−bx33+λ(x3−x1) (4)
The bifurcation mechanism leading to oscillations for this sensor system is different from the fluxgate array described above; nonetheless, the same qualitative features appear in the overall response of the system. It has been observed that the oscillatory behavior in the sensor system does not occur in a single unforced sensor. Even when coupled, the number of elements, initial conditions, and the type of coupling, all contribute to the emergence of this behavior. Hence, the disclosure herein provides new considerations in enhancing the utility and sensitivity of a large class of nonlinear dynamic sensors, such as fluxgate magnetometers for magnetic fields, ferroelectric detectors for electric-fields, or piezo-electric detectors for acoustics applications.
System resolution (defined as the mean residence times difference in the stable states of a threshold detector into which the summed output of the sensor system is fed) can be enhanced by carefully tuning the array (via the system parameter λ) to just beyond the onset of the oscillations. This works particularly well, when one has a reasonable a priori knowledge of the target signal values involved in a particular application, or when the target signal can be suitably gated (limited) to avoid saturating the system. Referring to
As discussed, a variety of mechanisms is available to quantify a target signal when using the sensor system described herein. The target signal may be quantified via its effect on the frequency of the induced system oscillations, as well as the shift in the mean value of this frequency. The residence time readout method can also be used to discern the target signal. As those skilled in the art will realize, the circuitries required for these detection methods are quite simple; in particular, no feedback circuit is required.
Though in
Obviously, many modifications and variations of the invention are possible in light of the above description. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as has been specifically described.
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