Abstract-dynamic plasma sheath can severely interfere with the communication of hypersonic vehicles during atmospheric reentry. Theoretical and experimental results show that low-frequency (LF) electromagnetic (EM) waves could penetrate the plasma sheath, building a feasible method to solve the “radio blackout” problem. This paper discovers that the propagation of LF EM waves in plasmas is still influenced by parasitic modulation effects. Compared to microwave frequencies, the impact of parasitic modulation effects on signal modulation patterns is more distinct for LF EM waves. In contrast to the microwave frequency range, where the rotation direction of QPSK signal constellation points changes with the ratio of plasma frequency to electromagnetic wave frequency, in the LF range, the constellation points undergo limited clockwise rotation. This phenomenon can be attributed to the unique magnetic field propagation mechanism of LF EM waves in dynamic plasmas. This paper analyzes the mechanism of this specific parasitic modulation effect and discovers a sinusoidal transformation relationship between amplitude attenuation and phase shift. Meanwhile, the experimental and simulation results proved that the time-varying plasma could cause the parasitic modulation effect of LF EM wave, resulting in a limited clockwise rotation of orthogonal phase-shift keying constellation points, which is consistent with the theoretical analysis.

When a hypersonic vehicle reentry into the atmosphere, the high-density plasma sheath generated by strong aerodynamic heating may shield the aerospace telemetry, tracing, and control (TT&C) signal in the microwave frequency band. The high-density plasma sheath may cause the interruption of the TT&C between ground station and vehicle for several to ten minutes.1–4 This phenomenon is known as “radio blackout.”

To allow the uninterrupted monitoring of spacecraft reentry, several methods have been proposed to mitigate radio blackout.4–11 The existing mitigation methods mainly fall into two categories: changing the propagation environment or the electromagnetic (EM) wave propagation mode. Changing the propagation environment involves interventions that chemically or physically control the plasma spatial distribution and reduce the electron density at the antenna window. Changing the EM wave propagation mode includes changing the frequency of the EM waves, improving the EM wave transmission capacity, establishing the plasma propagation channel model of the corresponding frequency band, and improving the existing communication methods to reduce the information error rate. These methods are still being continuously explored, deriving more optimized and reasonable feasible solutions to promote the method of mitigate radio blackout.

In recent years, expanding the possibilities of new propagation windows has been proposed as a potential solution.12 In accordance with the theory of EM wave propagation,13 when the EM wave frequency is far below than the plasma frequency (namely, ω c ω p), the efficiency of energy transfers from the EM wave to plasma decreases. Hence, the attenuation of low-frequency (LF) EM waves (Note: in this paper, the term “low frequency” differs from the standard radio frequency spectrum definition. Here, the term low frequency refers to frequencies below the microwave range.), which means the EM wave frequency is significantly lower than the plasma frequency, will be significantly lower than that of high-frequency EM waves. In this context, Liu et al. discovered in their research that LF EM waves exhibit unique magnetic field attenuation characteristics when propagating through plasmas.14 Unlike microwave EM waves, the frequency of LF EM waves is significantly lower than the plasma frequency, resulting in significantly lower attenuation of the magnetic component of LF EM waves in dynamic plasmas compared to the attenuation of the electric component.15 Consequently, using the magnetic field component of LF EM waves to maintain the minimum essential communications may be considered a feasible solution for mitigating radio blackout.16 

When a LF magnetic field is incident on a plasma, induced currents are formed on the plasma surface. The path of these induced currents is constrained by the geometric shape of the plasma.17 On the other hand, microwave EM waves, with wavelengths significantly smaller than the size of the plasma sheath, are not affected by the plasma model. For example, in the case of a cylindrical plasma model, the induction current forms a path similar to a multi-turn coil along the plasma surface, generating an induced magnetic field that weakens the incident LF magnetic field. Furthermore, the magnitude of the induction current is closely related to the conductivity of the transmission medium and the plasma sheath can be considered as a dielectric layer with a complex permittivity and dynamic and time-varying characteristics. Moreover, Xie et al. experimentally verified the attenuation mechanism of the LF magnetic component through ground-based trials.17–19 Thus, the unique attenuation mechanism of the magnetic component of LF EM waves and the dynamic conductivity of the transmission medium contribute to the distinct propagation mechanism of LF EM waves in plasma.

Meanwhile, the dynamic time-varying characteristics of the plasma sheath can cause amplitude and phase parasitic modulation on the propagation of communication signals.20,21 For the microwave band, the parasitic modulation effect has been confirmed as the main causes of communication deterioration.22 Yang et al. pointed out that the dynamic plasma sheath can cause phase fluctuations in microwave signals and lead to a specific rotation of MPSK constellation.20 For the LF band, recent studies have touched on the propagation characteristics of EM waves in dynamic plasma sheaths,16 but there has not been much detailed mechanism analysis on the parasitic modulation effects. Therefore, it is necessary to analyze the mechanism of the LF parasitic modulation effect to find feasible solutions to eliminate or mitigate the impact of the parasitic modulation effects.

Thus, based on the propagation equivalent model of the LF magnetic field in a cylindrical time-varying plasma,16 this paper has analyzed the mechanism of the LF parasitic modulation effect. We simulated the amplitude attenuation and phase shift of LF EM wave propagation in the plasma sheath and derived the relevant formulas for amplitude and phase variations. The analysis reveals that there is a sinusoidal correlation between the amplitude attenuation and phase shift, and within the range of phase-shift values, the amplitude and phase consistently maintain a positive correlation. To analyze the specific clockwise rotation of constellation maps, we also derived the coordinate formula of QPSK signal constellation points propagating in plasma. Numerical simulations are conducted to evaluate the influence of the parasitic modulation effect on the propagation of phase modulation signal under different parameters. The increase in carrier frequency results in a reduction in the penetration capability of LF signals through the plasma sheath, while an increase in the plasma collision frequency can mitigate the distortion of the signals. Meanwhile, we verified the parasitic modulation effect of LF EM wave in the dynamic plasma sheath by the experiment.

The remainder of this article is organized as follows. Section II illustrates the propagation mechanism of LF EM waves in the dynamic plasma sheath and derives the specific correlation between signal amplitude attenuation and phase shift. Section III deduces the constellation point function of the QPSK signal and simulates the parasitic modulation effect of LF EM waves in dynamic time-varying plasma. Section IV experimentally verifies the parasitic modulation effect of low-frequency magnetic wave. A detailed discussion, conclusion, and possible extensions are given in Sec. V.

Time-varying plasma angular frequency ω p ( t ) is23,24
(1)
where Ne is the electron density ( / m 3) and e is the number of electron charges ( 1.6 × 10 19 C), ε0 is the vacuum dielectric constant ( 8.854 × 10 12 F / m), and me is the electronic mass ( 9.1 × 10 31 kg). Then, the time-varying complex permittivity of dynamic plasma ε r ( t ) is25,
(2)
where ω p ( t ) is the time-varying plasma angular frequency (rad/s), ven is the collision frequency (rad/s), ω c = 2 π f c is the angular frequency of the LF magnetic field (rad/s), and fc is the frequency of LF magnetic field (Hz). When in the conductive medium, the time-varying complex dielectric constant ε r ( t ) can be expressed by the following formula with time-varying conductivity:26 
(3)
where σ ( t ) is time-varying conductivity. By comparing the coefficients of Eqs. (1) and (2), the time-varying conductivity of dynamic plasma σ ( t ) can be written as
(4)
As ω c v e n, by substituting Eq. (1) into Eq. (4), the time-varying conductivity of the dynamic plasma σ ( t ) is simplified as16 
(5)
Additionally, the skin effect will influence the propagation characteristics of EM waves in dynamic plasmas. Therefore, we analyzed the skin depth of the plasma sheath. The skin depth δ of the plasma sheath can be expressed using the following formula:
(6)
where μ0 is the vacuum permeability. Table I lists the settings for Ne, ve, skin depth at 10 MHz of a RAM-C vehicle at different altitudes at 10 MHz.27,28 For a 10 MHz LF magnetic field wave, at an altitude of 40 km, the electron density in the typical plasma sheath standoff region is 1.41 × 10 12 / cm 3, with a collision frequency of 1.6 × 10 9 / s. Calculating using the formula (6) as per the reference, the skin depth is 31.989 mm. When LF signals propagate within the dynamic plasma sheath, if the skin depth is greater than the thickness of the plasma sheath, the skin effect can be neglected. Therefore, to mitigate the impact of the skin effect, new requirements are proposed for the practical placement of LF antennas. As indicated in the calculation of the plasma sheath in reference,15 during the actual placement of LF antennas, it is recommended to position the antennas in the region of high plasma density and low thickness near the front end of the spacecraft, where the plasma thickness is less than 40 mm. Hence, in the subsequent theoretical derivations, we disregard the influence of the skin effect.
TABLE I.

Typical parameter settings for the plasma sheath during the reentry phase of a RAM-C vehicle.

Altitude (km) N e ( cm 3 ) v e ( s 1 ) Skin depth at 10 MHz (mm)
40  1.41 × 10 12 / cm 3  1.6 × 10 9 / s  31.989 
30  1.00 × 10 13 / cm 3  7.1 × 10 9 / s  25.285 
21  5.03 × 10 10 / cm 3  27.1 × 10 9 / s  696.5 
Altitude (km) N e ( cm 3 ) v e ( s 1 ) Skin depth at 10 MHz (mm)
40  1.41 × 10 12 / cm 3  1.6 × 10 9 / s  31.989 
30  1.00 × 10 13 / cm 3  7.1 × 10 9 / s  25.285 
21  5.03 × 10 10 / cm 3  27.1 × 10 9 / s  696.5 
Sun et al. revealed that the channel response of the cylindrical time-varying plasma sheath can be expressed equivalently by the transmission coefficient T(t),16 which is expressed as
(7)
where H 0 ( t ) is the incident LF magnetic field outside the plasma, H i ( t ) is the instantaneous transmitted LF magnetic field inside the plasma, and k = ( μ 0 e 2 r d f c ) / ( 2 m e v e ). Figure 1 illustrates a simplified cylindrical model of the LF plane wave incident on the plasma along the z direction and the electric field incident along the positive x axis. The time-varying attenuation coefficient and phase-shift coefficient of the transmitted LF magnetic field can be obtained from the transmission coefficient as16 
(8)
(9)
FIG. 1.

Simplified model of an LF plane wave incident on the cylindrical time-varying plasma.

FIG. 1.

Simplified model of an LF plane wave incident on the cylindrical time-varying plasma.

Close modal

According to Eqs. (7) and (8), the curve of attenuation coefficient α k ( t ) and phase-shift coefficient β k ( t ) varying with average plasma density N e ¯ are simulated by the parameter values as follows.

The numerical simulations adopt an average plasma density N e ¯ varying from 1 × 10 11 / cm 3 to 1 × 10 13 / cm 3, a collision frequency ve of 1.5 × 10 9 / s, a radius of the cylindrical time-varying plasma r of 50 mm, a thickness d of 40 mm, a length l of 1500 mm, and an EM wave frequency fc of 10 MHz. The electron density fluctuation is set to σ Δ = 0.3. The simulation results are shown in Fig. 2.

FIG. 2.

Curve of component variation with plasma density N e ¯ (a) attenuation coefficient αk and (b) phase-shift coefficient βk.

FIG. 2.

Curve of component variation with plasma density N e ¯ (a) attenuation coefficient αk and (b) phase-shift coefficient βk.

Close modal

In accordance with the simulation results, as the average plasma density increases, the attenuation coefficient and phase-shift coefficient of the signal monotonically decrease. It can be inferred that LF EM waves will still be affected by the dynamic plasma sheath, resulting in parasitic modulation effects on the signal. Both αk and βk are functions of N e ¯, and larger time-varying plasma frequencies can cause more severe amplitude attenuation and phase shift of the signal simultaneously. Therefore, we not only need to study the independent characteristics of attenuation coefficient and phase-shift coefficient, but also need to jointly consider and discuss the correlation between them. With the exponential variation of the time-varying plasma frequency, the phase-shift coefficient of the signal remains negative and within the range of ( π 2 , 0 ). So, compared to the previously discovered intermediate frequency parasitic modulation effect, the LF parasitic modulation effect will cause smaller phase rotation on the signal, and the rotation angle is within the range of ( π 2 , 0 ).

In this section, the correlation between amplitude attenuation and phase attenuation of the transmission coefficient of LF EM waves in the cylindrical plasma sheath special effect model is derived and simulated.

Because the phase rotation caused by LF parasitic modulation always falls within the range of ( π 2 , 0 ) and monotonically varies with the time-varying plasma density, the phase-shift coefficient of the signal is correspondingly mapped to the time-varying plasma density. According to Eq. (8), the following relationship can be obtained:
(10)
Then, we substitute Eq. (13) into Eq. (7) to get the expression of α k ( t ) with β k ( t ),
(11)
We adopt an average plasma density N e ¯ varying from 1 × 10 11 / cm 3 to 1 × 10 13 / cm 3. Then, we simulated Eq. (10) and obtained the curve as shown in Fig. 3. It can be seen from the Fig. 3 that with the change of plasma density Ne, the channel amplitude attenuation coefficient and phase-shift attenuation coefficient of the time-varying plasma channel present a positive correlation curve and the phase-shift value is negative. Yao et al. pointed out that if there is a strong negative correlation between amplitude and phase, the constellation rotates counterclockwise; on the contrary, the constellation rotates clockwise.29 Therefore, the constellation would rotate clockwise after the LF signal passes through the dynamic plasma sheath.
FIG. 3.

Curve of attenuation coefficient α k ( t ) vs phase-shift coefficient β k ( t ).

FIG. 3.

Curve of attenuation coefficient α k ( t ) vs phase-shift coefficient β k ( t ).

Close modal

In this section, we analyzed the constellation point function of the QPSK signal and simulated the propagation of LF magnetic field waves in the plasma sheath to verify the special rotation of the QPSK signal.

The transmission coefficient T(t) can be represented by α k ( t ) and β k ( t ) as
(12)
The differential QPSK phase modulation signal can be expressed as
(13)
where fc is the EM wave frequency, and Es is the energy per symbol. After passing through the time-varying plasma sheath, the QPSK signal becomes
(14)
According to Eq. (10), the attenuation coefficient α k ( t ) and phase-shift coefficient β k ( t ) are modulated to the magnitude and phase of the QPSK signals by time-varying plasma. The constellation points do no longer gather round the four fixed points ( 2 2 , 2 2 ) , ( 2 2 , 2 2 ) , ( 2 2 , 2 2 ) , ( 2 2 , 2 2 ). The modulated constellation points could be written as
(15)
(16)
Then, the module (amplitude) of the constellation points corresponds to the phase angle. From Eq. (13), the coordinates of each constellation point can be expressed as
(17)
(18)
Substitute Eqs. (7) and (8) into Eqs. (16) and (17), we can obtain the relevant expressions for I and Q as follows:
(19)

Based on Eq. (13), the propagation of QPSK LF wave signals in dynamic plasma has been simulated. The numerical simulations adopt an average plasma density N e ¯ of 5 × 10 11 cm 3, a collision frequency ve of 2 × 10 9 / s, a radius of the cylindrical time-varying plasma r of 50 mm, a thickness d of 40 mm, a length l of 1500 mm, and an EM wave frequency fc of 10 MHz. The electron density fluctuation is set to σ Δ = 0.3.

As shown in Fig. 4, with the channel response of time-varying plasma added to the simulation channel, the constellation points of the signal at the receiver are no longer concentrated in the ideal mapping position, and the constellation diagram has an obvious clockwise rotation phenomenon. The fundamental reason for the constellation rotation of the phase modulation signal is the strong correlation between the amplitude and phase of the signal in plasma.30 Moreover, the simulation results show that parasitic modulation will still occur when LF EM waves pass through the time-varying plasma. Therefore, for LF EM waves, time-varying plasma will still cause the parasitic modulation effect and produce multiplicative interference on QPSK, thus threatening the reliability of communication signals.

FIG. 4.

The constellation graph of QPSK signals after plasma (a) without plasma and (b) with plasma.

FIG. 4.

The constellation graph of QPSK signals after plasma (a) without plasma and (b) with plasma.

Close modal

Next, taking the constellation point in the first quadrant as an example, we simulated the correlation characteristics of the horizontal and vertical coordinates of the constellation point, namely, I and Q values, when the LF QPSK signal is affected by the parasitic modulation effect caused by the plasma sheath.

We adopt an average plasma density N e ¯ varying from 1 × 10 11 / cm 3 to 1 × 10 13 / cm 3. The channel parameters are consistent with the simulation above. The simulation results are shown in Fig. 5. As the average plasma density increases, the abscissa I of the constellation point shows a trend of first increasing and then decreasing, with the inflection point near the average plasma density of 2 × 10 17. At the same time, the vertical coordinate of the constellation shows a trend of decreasing first and then increasing, with the inflection point at the average plasma density greater than 1 × 10 18. Therefore, as the average plasma density increases, the constellation will exhibit a clockwise rotation phenomenon, as shown in Fig. 6. This is consistent with the constellation point rotation phenomenon in the simulation diagram in Fig. 4.

FIG. 5.

The variation diagram of constellation point coordinates with plasma density (a) the variation of I and (b) the variation of Q.

FIG. 5.

The variation diagram of constellation point coordinates with plasma density (a) the variation of I and (b) the variation of Q.

Close modal
FIG. 6.

The correlation of I and Q.

FIG. 6.

The correlation of I and Q.

Close modal

In this section, we simulate the effects of different carrier frequency and plasma collision frequency on the QPSK channel with dynamic plasma channel response and Gaussian noise. In order to evaluate the effect of parasitic modulation caused by time-varying plasma on demodulation at different carrier frequencies and collision frequencies, the error vector amplitude (EVM) of QPSK signals in plasma is measured in this simulation.

1. Effects of the carrier frequency on the propagation of the low-frequency waves in time-varying plasma

The numerical simulations adopt an EM wave frequency fc varying from 1 to 30 MHz, an average plasma density N e ¯ of 8 × 10 11 cm 3, a collision frequency ve of 2 × 10 9 / s, a radius of the cylindrical time-varying plasma r of 50 mm, a thickness d of 40 mm, and a length l of 1500 mm. The electron density fluctuation is set to σ Δ = 0.3. The simulation results are shown in Fig. 7. It is seen that with the increase in the carrier frequency, the phase rotation of the constellation is significantly intensified, and the distance between any two constellation points will rapidly decrease.

FIG. 7.

The constellation graph of QPSK signals with different EM wave frequency fc (simulation results) (a) f c = 1, (b) f c = 5, (c) f c = 10, and (d) f c = 30 MHz.

FIG. 7.

The constellation graph of QPSK signals with different EM wave frequency fc (simulation results) (a) f c = 1, (b) f c = 5, (c) f c = 10, and (d) f c = 30 MHz.

Close modal
EVM is commonly used to quantify the performance of digital radio transmitters or receivers. It represents the difference between the ideal or expected constellation point of the received signal and the actual position of that point in the signal's constellation diagram. The magnitude of the error vector is equal to the ratio of the power of the error vector to the reference power. The increase in EVM signifies a degradation in the modulation accuracy of the communication system. When the EVM reaches 100%, the signal is completely distorted. EVM can be defined as
(20)
where Perror is the ratio of the power of the error vector, and the Preference is the root mean square (RMS) power. As shown in the Fig. 8, when the carrier frequency of the signal is below 10 MHz, the EVM significantly raises with the increase in carrier frequency. It means that in the LF range, increasing the carrier frequency results in a decrease in the signal's penetration capability through the plasma sheath.
FIG. 8.

The EVM of QPSK signals after plasma with the carrier frequency fc (simulation results).

FIG. 8.

The EVM of QPSK signals after plasma with the carrier frequency fc (simulation results).

Close modal

2. Effects of the collision frequency on the propagation of the low-frequency waves in time-varying plasma

The numerical simulations adopt a collision frequency ve varying from 1 × 10 9 / s to 5 × 10 9 / s, an average plasma density N e ¯ of 8 × 10 11 cm 3, a radius of the cylindrical time-varying plasma r of 50 mm, a thickness d of 40 mm, a length l of 1500 mm, and an EM wave frequency fc of 10 MHz. The electron density fluctuation is set to σ Δ = 0.3. The simulation results are shown in the Fig. 9. With the increase in collision frequency of time-varying plasma, all constellation points show similar regular rotation, and the phase rotation degree of constellation gradually decreases, and LF EM wave is affected by dynamic plasma. As shown in the Fig. 10, with the growth of the collision frequency, the EVM gets smaller. When the collision frequency approaches to 2 × 10 9 / s, the EVM reduces to about 10%. This indicates that an increase in plasma collision frequency can reduce distortion in LF signals to some extent.

FIG. 9.

The constellation graph of QPSK signals with different collision frequency ve (simulation results) (a) v e = 1 × 10 9 / s, (b) v e = 5 × 10 9 / s, (c) v e = 10 × 10 9 / s, (d) v e = 30 × 10 9 / s.

FIG. 9.

The constellation graph of QPSK signals with different collision frequency ve (simulation results) (a) v e = 1 × 10 9 / s, (b) v e = 5 × 10 9 / s, (c) v e = 10 × 10 9 / s, (d) v e = 30 × 10 9 / s.

Close modal
FIG. 10.

The EVM of QPSK signals after plasma with the collision frequency ve (simulation results).

FIG. 10.

The EVM of QPSK signals after plasma with the collision frequency ve (simulation results).

Close modal

The experimental device includes a software radio module based on the graphic programming software LabVIEW for signal source, sink, signal modulation, and demodulation, as well as hardware peripherals such as USRP transmitter and receiver, power amplifier, ring antenna, iso-scale magnetic antenna, vacuum cavity, and time-varying plasma generator. The block diagram of the experimental device is shown in Fig. 11(a). The phase modulation signals (QPSK) were produced by LabVIEW with a carrier frequency of 10 MHz. The bit rate is 25 kbps. Then, the QPSK signal is converted into a radio frequency signal through USRPX310. After the radio frequency signal passes through the power amplifier, the ring transmitting antenna realizes the LF EM wave radiation of the scaled warhead position in the plasma environment. The distance between the warhead and the plasma spout is 200 mm. The receiving antenna is placed inside the scaled warhead, and a ceramic window is set on the surface of the warhead where the receiving antenna is placed for signal transmission. The rest of the warhead is made of stainless-steel material. During the experiment, the warhead was cooled down using a water-cooling system. The receiving antenna is connected to the USRP receiver outside the instrument cavity via a coaxial cable, and the signal is transmitted to the software radio receiver to observe the penetration signal status and record experimental data. Figure 11(b) shows the photograph of the experimental setup. Figure 11(c) shows the installation details of the receiving antenna. The setting of the magnetic field antenna can be referred to Ref. 18.

FIG. 11.

(a)Schematic of LF EM wave parasitic modulation effect verification experiment, (b) photograph of the experimental setup, and (c) installation details of receiving antenna.

FIG. 11.

(a)Schematic of LF EM wave parasitic modulation effect verification experiment, (b) photograph of the experimental setup, and (c) installation details of receiving antenna.

Close modal

The experiment utilized inductively coupled plasma (ICP) to generate the plasma. The power supply was an alternating current source with an oscillation frequency of 440 kV. The power supplied varied between 50 and 500 kW, and different frequencies were used to produce plasma in various states, thereby achieving a wide range of electron densities.31 As shown in Fig. 11(b), the plasma nozzle had a diameter of 220 mm, suggesting that the ejected plasma could be approximated as a cylindrical shape with a diameter of about 160 mm. The cone diameter of the warhead was 110 mm, and the average thickness of the plasma traversed by the EM waves was approximately 35 mm. In the experiment, plasma density waveforms were obtained using a combination of microwave and probe diagnostics. The microwave diagnosis system mainly includes three parts: a vector network analyzer (VNA), a high-temperature resistant focusing antenna, and a low loss stable phase cable.32  Figure 12 shows the measured plasma density values over a duration of 10 ms. The average plasma densities corresponding to different experimental conditions, as diagnosed, are 1.76 × 10 11 and 5.02 × 10 11 cm 3, with collision frequencies of 2.75 × 1 0 9 / s and 2.35 × 1 0 9 / s, respectively. Figures 12(a) and 12(b) indicate that the fluctuation levels of plasma density for experiment status 1 and status 2 are in the range of 0.2–0.25. The plasma density and collision frequency corresponding to different experimental states, as obtained from diagnostics, are presented in Table II. The specific process and principle of plasma generation can be found in Refs. 31–33.

FIG. 12.

Plasma density fluctuation waveforms under different experimental conditions. (a) N e = 1.76 × 10 11 and (b) N e = 5.02 × 10 11 cm 3.

FIG. 12.

Plasma density fluctuation waveforms under different experimental conditions. (a) N e = 1.76 × 10 11 and (b) N e = 5.02 × 10 11 cm 3.

Close modal
TABLE II.

Electron density and collision frequency of the two different voltages.

Status Voltage (kV) Electron density(cm−3) Collision frequency (s)
5.99  1.76 × 1011  2.75 
7.00  5.02 × 1011  2.35 
Status Voltage (kV) Electron density(cm−3) Collision frequency (s)
5.99  1.76 × 1011  2.75 
7.00  5.02 × 1011  2.35 

Figures 13(a), 13(b), 13(d), and 13(e) show the phase changes of the constellation graph of QPSK signals before and after the LF EM wave passes through the dynamic plasma sheath with an average electron density of 1.76 × 10 11 cm 3 and 5.02 × 10 11 cm 3. The experimental results were obtained by a software radio receiver program written by USRPX310 and LabVIEW. As shown as in Fig. 13(b), as the LF EM wave passes through the plasma, the constellation is no longer focused on the ideal position, and the constellation appears obvious rotation. Meanwhile, as shown as in Fig. 14, the eye map trajectory becomes unclear and the opening angle becomes smaller. Thus, it confirming that the LF signal is still affected by the parasitic modulation effect in the plasma environment. In Figs. 13(e) and 14(e), with the increase in plasma density, the rotation of constellation is significantly intensified, and the production distance between any two points is obviously decreased. The eye trace gradually becomes chaotic and the opening and closing degree significantly decreases, which further deteriorates the performance of the system. Therefore, as the average plasma density increases, the signal exhibits stronger parasitic modulation effects, which imposes more severe interference on the signal.

FIG. 13.

The constellation graph of QPSK signals after plasma with different electron density ( N e = 1.76 × 10 11 cm 3) (a) experimental (without plasma), (b) experimental (with plasma), (c) simulation (with plasma) ( N e = 5.02 × 10 11 cm 3), (d) experimental (without plasma), (e) experimental (with plasma), and (f) simulation (with plasma).

FIG. 13.

The constellation graph of QPSK signals after plasma with different electron density ( N e = 1.76 × 10 11 cm 3) (a) experimental (without plasma), (b) experimental (with plasma), (c) simulation (with plasma) ( N e = 5.02 × 10 11 cm 3), (d) experimental (without plasma), (e) experimental (with plasma), and (f) simulation (with plasma).

Close modal
FIG. 14.

The eye diagram of QPSK signals after plasma with different electron density ( N e = 1.76 × 10 11 cm 3) (a) experimental(without plasma), (b) experimental(with plasma), (c) simulation(with plasma) ( N e = 5.02 × 10 11 cm 3), (d) experimental(without plasma), (e) experimental(with plasma), and (f) simulation(with plasma).

FIG. 14.

The eye diagram of QPSK signals after plasma with different electron density ( N e = 1.76 × 10 11 cm 3) (a) experimental(without plasma), (b) experimental(with plasma), (c) simulation(with plasma) ( N e = 5.02 × 10 11 cm 3), (d) experimental(without plasma), (e) experimental(with plasma), and (f) simulation(with plasma).

Close modal

To demonstrate the consistency between the experimental results and the theoretical analysis, we simulated the experimental results based on the propagation equivalent model of the LF magnetic field in cylindrical time-varying plasma. The simulation parameters (including electron density and plasma thickness) should be the same as the experimental conditions. As shown in Figs. 13(c), 13(f), 14(c), and 14(f), the simulation results are basically consistent with the experimental results in terms of constellation attenuation and phase rotation changes, which proves the reliability of theoretical derivation.

Subsequently, we conducted simulations of the constellation diagrams for a 12 GHz microwave signal and a 10 MHz LF signal, both under the same plasma parameters. From the Fig. 15, it can be observed that both microwave and LF signals exhibit rotation in their constellation diagrams. Under the same plasma parameters, the LF signal experiences less attenuation in amplitude and phase shift compared to the microwave signal. Additionally, to provide a more refined comparison of the parasitic modulation effects on LF magnetic field waves and microwave EM waves, we simulated the amplitude modulation depths of LF magnetic field waves and microwave EM waves under different plasma densities. The amplitude modulation level is defined as follows:
(21)
where E amax ( t ) represents the maximum value of the amplitude envelope, and E amin ( t ) represents the minimum value of the amplitude envelope. The simulation results are presented in Fig. 16, where the blue line represents the 10 MHz LF signal, and the red line represents the 12 GHz microwave signal. Fig. 16 reveals that when the plasma density is below 1 × 10 12 cm 3, the LF signal undergoes significantly less parasitic modulation compared to the microwave signal. As the plasma density reaches 3 × 10 11 cm 3, the parasitic modulation level for the microwave signal remains largely between 0.85 and 1, indicating near complete modulation, while the parasitic modulation level for the LF signal remains between 0.5 and 0.7. With increasing plasma density, the parasitic modulation level for the LF signal significantly increases. However, even at plasma densities higher than 1 × 10 12 cm 3, the parasitic modulation of the LF signal remains slightly lower than that of the microwave signal. These findings suggest that LF EM waves have a stronger penetration capability in dynamic plasma compared to microwave EM waves.
FIG. 15.

Comparison of the parasitic modulation (constellation graph N e = 5 × 10 11 cm 3) (a) f c = 10 MHz and (b) f c = 12 GHz.

FIG. 15.

Comparison of the parasitic modulation (constellation graph N e = 5 × 10 11 cm 3) (a) f c = 10 MHz and (b) f c = 12 GHz.

Close modal
FIG. 16.

Comparison of amplitude modulation depth under different plasma densities).

FIG. 16.

Comparison of amplitude modulation depth under different plasma densities).

Close modal

This paper focus on the effect of parasitic modulation caused by time-varying plasma on the phase modulation of LF EM wave, which is been theoretically analyzed. Experimental and simulation results confirm that LF EM waves are affected by parasitic modulation when passing through time-varying plasma. However, compared to microwave EM waves, LF EM waves exhibit unique parasitic modulation mechanisms. They experience significantly lower levels of parasitic modulation, and under the influence of parasitic modulation, the constellation diagram of LF QPSK signals only undergoes limited clockwise rotation. Additionally, the comparative simulations between microwave and LF signals under the same plasma parameters demonstrate that LF EM waves have stronger penetration capabilities in time-varying plasma. Therefore, using LF waves in maintaining the minimum essential communication may be a more reliable choice than microwave EM wave transmission. Furthermore, numerical simulation results indicate that reducing the carrier frequency or increasing the plasma collision frequency can enhance the penetration capability of LF signals through the plasma sheath. In the future, communication systems suitable for LF ionospheric communication can be developed based on the influence of plasma parameters on LF waves.

This work was supported in part by the National Natural Science Foundation of China under Grant No. 62071355.

The authors have no conflicts to disclose.

Yuxuan Gao: Data curation (supporting); Formal analysis (equal); Investigation (equal); Methodology (equal); Software (equal); Validation (equal); Visualization (equal); Writing – original draft (supporting); Writing – review & editing (equal). Xiaoping Li: Formal analysis (equal). Min Yang: Conceptualization (equal); Formal analysis (equal); Funding acquisition (equal); Methodology (equal); Project administration (equal); Resources (equal); Supervision (equal); Validation (equal); Writing – review & editing (equal). Kai XIE: Funding acquisition (equal); Project administration (equal); Resources (equal); Supervision (equal); Writing – review & editing (equal). Longjie Qiao: Data curation (equal); Investigation (equal); Methodology (equal); Software (lead). Haoyan Liu: Writing – review & editing (equal). Chengguang Li: Formal analysis (equal). Donglin Liu: Resources (equal). Lei Quan: Resources (equal). Mingxing Wu: Formal analysis (equal).

The data that support the findings of this study are available from the corresponding author upon reasonable request.

1.
L.
Ge
,
L.
Gao
,
Xiao
,
S.
Gong
,
Shuai
, and
M.
Liu Sheng
, “
The requirements and strategy analysis for TT&C of near space vehicles
,”
Nat. Def. Sci. Technol.
33
,
37
40
(
2012
).
2.
M.
Gong
,
J.
Tan
,
D.
Li
,
Z.
Ma
,
G.
Tian
,
J.
Wang
, and
L.
Meng
, “
Review of blackout problems of near space hypersonic vehicles
,”
J. Astronaut.
39
,
1059
(
2018
).
3.
Z.
Shen
and
L.
Meng
, “
Requirements and strategy analysis of TT&C used for ultrasonic speed aircraft
,”
Aerospace Electronic Warfare
(
2010
), pp.
31
34
.
4.
E. D.
Gillman
,
J. E.
Foster
, and
I. M.
Blankson
, “
Review of leading approaches for mitigating hypersonic vehicle communications blackout and a method of ceramic particulate injection via cathode spot arcs for blackout mitigation
,” Technical Report No. NASA/TM-2010-216220 (NASA,
2010
).
5.
M.
Keidar
,
M.
Kim
, and
I. D.
Boyd
, “
Electromagnetic reduction of plasma density during atmospheric reentry and hypersonic flights
,”
J. Spacecr. Rockets
45
,
445
453
(
2008
).
6.
Y.
Li
,
B.
Luo
,
W.
Guo
, and
S.
Li
, “
Feasibility analysis of using Ka-band of TRDS to support wireless communication for spacecraft reentry
,”
Manned Spacefl.
21
,
582
588
(
2015
).
7.
T.
Su
, “
Chinese academy of sciences
,” Ph.D. thesis (
Xi'an Institute of Optics and Precision Mechanics
,
2020
).
8.
Z.
Qing
, Ph.D. thesis,
Harbin Institute of Technology
,
2020
.
9.
X.
Zuo
,
D.
Xu
,
J.
Liu
, and
R.
Yao
, “
Research on terahertz TT&C communication performance of hypersonic vehicle
,”
Flight Control Detect.
4
,
1
8
(
2021
).
10.
L.
Shi
,
Y.
Liu
,
S.
Fang
,
X.
Li
,
B.
Yao
,
L.
Zhao
, and
M.
Yang
, “
Adaptive multistate Markov channel modeling method for reentry dynamic plasma sheaths
,”
IEEE Trans. Plasma Sci.
44
,
1083
1093
(
2016
).
11.
H.
Wei
,
Y.
Liu
,
L.
Shi
,
B.
Yao
, and
X.
Li
, “
Bit error rate and channel capacity performance of telemetry modulation methods under typical reentry plasma sheath channel
,”
IEEE Trans. Plasma Sci.
47
,
4950
4960
(
2019
).
12.
H.
Zhang
,
M.
Yang
,
W.
Bao
,
X.
Li
, and
J.
Wang
, “
Short-frame fountain code for plasma sheath with ‘communication windows
,’”
IEEE Trans. Veh. Technol.
69
,
15569
15579
(
2020
).
13.
V. L.
Ginzburg
, “
The propagation of electromagnetic waves in plasmas
,” in
International Series of Monographs in Electromagnetic Waves
,
1970
.
14.
D.
Liu
,
X.
Li
,
K.
Xie
, and
Z.
Liu
, “
The propagation characteristics of electromagnetic waves through plasma in the near-field region of low-frequency loop antenna
,”
Phys. Plasmas
22
,
102106
(
2015
).
15.
D.
Liu
,
X.
Li
,
Y.
Liu
,
K.
Xie
, and
B.
Bai
, “
Attenuation of low-frequency electromagnetic wave in the thin sheath enveloping a high-speed vehicle upon re-entry
,”
J. Appl. Phys.
121
,
074903
(
2017
).
16.
B.
Sun
,
K.
Xie
,
Y.
Liu
,
Y.
Zhang
,
S.
Guo
, and
P.
Ma
, “
Experimental investigation on the dynamic propagation characteristics of low-frequency electromagnetic waves in cylindrical time-varying enveloping plasma generated by a shock tube
,”
IEEE Trans. Plasma Sci.
50
,
250
260
(
2022
).
17.
K.
Xie
,
S.
Guo
,
B.
Sun
,
L.
Quan
, and
Y.
Liu
, “
Modeling and experimental study of low-frequency electromagnetic wave propagation in cylindrical enveloping plasma produced by a shock tube
,”
Phys. Plasmas
26
,
073509
(
2019
).
18.
G.
Shaoshuai
,
X.
Kai
,
S.
Bin
,
X.
Ruoyao
, and
L.
Yan
, “
Experiment on low-frequency electromagnetic waves propagating in shock-tube-generated magnetized cylindrical enveloping plasma
,”
Plasma Sci. Technol.
23
,
075401
(
2021
).
19.
K.
Xie
,
B.
Sun
,
S.
Guo
,
L.
Quan
, and
Y.
Liu
, “
Experimental apparatus for investigating the propagation characteristics of the low-frequency electromagnetic waves in hypersonic plasma fluid generated by shock tube
,”
Rev. Sci. Instrum.
90
,
073503
(
2019
).
20.
A.
Demetriades
and
R.
Grabow
, “
Mean and fluctuating electron density in equilibrium turbulent boundary layers
,”
AIAA J.
9
,
1533
1538
(
1971
).
21.
T. C.
Lin
and
L. K.
Sproul
, “
Influence of reentry turbulent plasma fluctuation on EM wave propagation
,”
Comput. Fluids
35
,
703
711
(
2006
).
22.
S. G.
Ohler
,
B. E.
Gilchrist
, and
A. D.
Gallimore
, “
Electromagnetic signal modification in a localized high-speed plasma flow: Simulations and experimental validation of a stationary plasma thruster
,”
IEEE Trans. Plasma Sci.
27
,
587
594
(
1999
).
23.
M.
Yang
,
X.
Li
,
D.
Wang
,
Y.
Liu
, and
P.
He
, “
Propagation of phase modulation signals in time-varying plasma
,”
AIP Adv.
6
,
055110
(
2016
).
24.
D.
Gregoire
,
J.
Santoru
, and
R.
Schumacher
, “
Electromagnetic-wave propagation in unmagnetized plasmas
,”
Technical Report No. 1992-03-01
(
Hughes Research Labs, Malibu CA
,
1992
).
25.
M. A.
Heald
,
C. B.
Wharton
, and
H. P.
Furth
, “
Plasma diagnostics with microwaves
,”
Phys. Today
18
(
9
),
72
(
1965
).
26.
V. L.
Ginzburg
, The Propagation of Electromagnetic Waves in Plasmas, International Series of Monographs on Electromagnetic Waves Vol. 7 (Pergamon Press, 1970).
27.
R. F.
Harrington
, Time-Harmonic Electromagnetic Fields (IEEE Press, 2001).
28.
R. A.
Hartunian
,
G. E.
Stewart
,
S. D.
Fergason
,
T. J.
Curtiss
, and
R. W.
Seibold
, “
Causes and mitigation of radio frequency (RF) blackout during reentry of reusable launch vehicles
,”
Technical Report
No. ATR-2007(5309)-1 (
Aerospace Corporation
,
2007
).
29.
C.
Swift
,
F.
Beck
,
J.
Thomson
, and
S.
Castellow
, Jr.
, “
The entry plasma sheath and its effect on space vehicle electromagnetic systems
,” Technical Report No. N71-21101 (NASA, 1970).
30.
B.
Yao
, Ph.D. thesis,
Xidian University
,
2019
.
31.
C.
Zhao
,
X.
Li
,
Y.
Liu
,
D.
Liu
,
C.
Sun
,
J.
Zhang
, and
W.
Bao
, “
A phase shift group delay-based approach to resolving the phase ambiguity problem in plasma microwave diagnostics
,”
J. Appl. Phys.
132
,
213303
(
2022
).
32.
L.
Xiaoping
,
Z.
Chengwei
,
L.
Yanming
,
J.
Zhang
,
L.
Donglin
,
S.
Chao
, and
B.
Weimin
, “
Research on the method of dual-frequency microwave diagnosis of plasma for solving phase integer ambiguity
,”
Plasma Sci. Technol.
23
,
095501
(
2021
).
33.
C.
Zhao
,
X.
Li
,
Y.
Liu
,
D.
Liu
,
C.
Sun
,
G.
Ma
,
L.
Tian
, and
W.
Bao
, “
Research on plasma electron density distribution based on microwave diffraction
,”
Plasma Sources Sci. Technol.
31
,
015007
(
2022
).