Candidate Design of New Service Signals in the NavIC L1 Frequency Band

  • NAVIGATION: Journal of the Institute of Navigation
  • June 2025,
  • 72
  • (2)
  • navi.695;
  • DOI: https://doi.org/10.33012/navi.695

Abstract

Satellite navigation payloads use a constant-envelope composite signal to efficiently operate their high-power amplifiers in the saturation region. This composite signal consists of multiple signals that are multiplexed at the baseband level to support various services. The complexity of the signal multiplexing technique increases with multi-level signals. Here, we propose designing new service signals for Navigation with Indian Constellation (NavIC) in the L1 frequency band. The NavIC L1-band open civilian service signal is a multi-level design. We propose multiplexing new service signals to this multi-level signal at a single frequency and multiple frequencies without interfering with existing navigation service signals while maintaining backward compatibility. We present a novel concept for preserving the power spectral density criteria in the optimization framework to meet interoperability requirements and present an optimal power-sharing and modulation scheme. Results show that the single-frequency and multi-frequency methods for multiplexing new service signals both achieve maximum multiplexing efficiency.

Keywords

INTRODUCTION

Global navigation satellite systems (GNSSs) transmit several spread-spectrum signals on the same radio frequency (RF) band. All GNSS service providers broadcast interoperable and inter-compatible navigation signals. Moreover, all GNSS service providers, including the Global Positioning System (GPS), Galileo, Globalnaya Navigazionnaya Sputnikovaya Sistema (GLONASS), Quasi-Zenith Satellite System (QZSS), BeiDou, and Navigation with Indian Constellation (NavIC), provide interoperable open civilian service in the L1 frequency band (1559–1610 MHz), with many GNSS service providers transmitting inter-compatible open civilian and restricted service signals in the L1 frequency band. These signals include GPS’s L1 C/A, P(Y)-code, and M-code, Galileo’s L1 public regulated service (PRS), GLONASS’s L1-C/A and P-code, and BeiDou’s B1I and B1A (Morton et al., 2021; Hein et al., 2006; Kaplan & Hegarty, 2017). The International Telecommunication Union (ITU, 2020) assigns the L1 band as a radio navigation satellite service for safety-of-life applications. Satellite-based augmentation systems (SBASs) also operate in the same frequency range to augment open civilian satellite-based navigation services, e.g., the GPS L1 C/A signal, that use pseudorandom noise codes from the GPS family of codes. The United States’ Wide Area Augmentation System, the European Geostationary Navigation Overlay Service, India’s GPS-Aided Geo-Augmented Navigation, the Michibiki Satellite Augmentation System (MSAS), Russia’s System for Differential Corrections and Monitoring, and the BeiDou Satellite-Based Augmentation System are all SBASs. The L1 frequency band is congested for radio navigation satellite services, which imposes several limits on proposed new services (open or restricted service signals) to safeguard incumbent services. GNSS service providers must ensure that the proposed signals are compatible with all open, restricted/authorized L1 signals.

Second-generation NavIC satellites transmit an interoperable open civilian service signal in the L1 frequency range (Upadhyay et al., 2024). The open service signal has two components: data and pilot components. The NavIC system plans to provide a new navigation service in the L1 frequency band in addition to the present open civilian service signal (Bhadouria & Upadhyay, 2022; Bhadouria et al., 2023). Furthermore, the potential addition of a new service signal (NSS) with better accuracy and an improved jamming margin compared with the open civilian signal is currently under study (Bhadouria & Upadhyay, 2022; Bhadouria et al., 2023). The NSS will have both data and pilot components. However, the NavIC L1-band open civilian service signal is a multi-level modulated signal with an overall envelope to ensure that it is constant and satisfies multiplexed binary offset carrier (MBOC) modulation power spectral density (PSD) requirements, i.e., MBOC(6,1,1/11). Introducing a new service in the NavIC L1-band system requires multiplexing the multi-level modulation signal and NSSs at the baseband level to avoid utilizing separate payload RF chains, modulators, high-power amplifiers (HPAs), and output section filters. At the baseband level, onboard signal multiplexing is required to achieve a constant envelope modulus, which enhances amplifier performance (Bhadouria et al., 2022; Yao et al., 2017). As the L1 frequency band is congested owing to multiple operational open civilian and restricted services provided by GNSS service providers, it is imperative to investigate the carrier frequency for the new NavIC service signal in the L1 frequency band to avoid intersystem interference. Hence, we present multi-level single-frequency and multi-frequency signal multiplexing designs to add NSSs at the same frequency and at an offset frequency, respectively.

Regarding PSD requirements and receiver design, a signal multiplexing method must be backward compatible with multi-level modulation signals. Additionally, a signal multiplexing strategy must provide adjustable onboard power-sharing of individual signals and onboard switchability of additional service signals. In the L1 frequency band, Galileo employs composite binary offset carrier (CBOC) modulation (Avila-Rodriguez et al., 2006; Rebeyrol et al., 2006), multiplexing a bipolar PRS signal with a multi-level CBOC signal over a single frequency to obtain a constant envelope modulus. This technique of multiplexing multi-level and bipolar signals must be implemented via a more general method (Yao & Lu, 2017).

Multiplexing multi-level signals over single and multiple frequencies requires phase- and waveform-domain processing (Yao & Lu, 2021). In multi-level phase-optimized constant-envelope transmission, multi-level signals are multiplexed over multiple frequencies via phase optimization (Zhang et al., 2013). In this case, an approximate analytical expression can derive the PSD needed for signal coordination. Waveform-domain processing provides an exact analytical expression of the multiplexed signal (Zhang et al., 2012). Constant-envelope multiplexing with intermodulation construction (CEMIC) multiplexes multi-level signals over single and multiple frequencies by optimizing the input signal amplitude. The CEMIC approach provides a constant envelope modulus by superimposing desired signals with intermodulation components. CEMIC imposes no limits on the signal number, power-sharing, waveform, or phasing. In multi-frequency constant-envelope multiplexing based on equivalent signal vectors, multi-level signals are multiplexed over multiple frequencies for high efficiency and flexibility (Ma et al., 2019). Multi-frequency constant-envelope multiplexing considers the signal state probability and homogeneous equations to multiplex multi-level signals over multiple frequencies, improving power leakage and computational complexity (Chen et al., 2021). Signal multiplexing optimization is not limited by computational complexity or convergence time, as it is a one-time process that does not need real-time optimization. However, the CEMIC and multi-frequency constant-envelope multiplexing schemes do not consider constraints on the power ratio between multi-level signals, which is required for meeting specific PSD criteria, e.g., MBOC(6,1,1/11) for L1-band open service signals. Modified CEMIC (MCEMIC) multiplexes bipolar signals over a single frequency while integrating backward-compatibility constraints into the optimization framework to minimize changes in the onboard navigation system and ground receivers (Bhadouria et al., 2022), achieving greater efficiency than CEMIC. It is possible to expand the MCEMIC approach to multiplex multi-level and multi-frequency signals to form a composite signal with a constant envelope modulus while preserving the PSD criteria of multi-level signals.

We propose a design for the new NavIC L1-band service signals by extending the MCEMIC multiplexing scheme to support multi-level and multi-frequency signals and introduce a novel concept for preserving PSD to ensure the interoperability of L1-band open service signals. We provide a case study of multiplexing NSSs with the existing NavIC L1-band open service signal to form a constant-envelope composite signal. We also suggest optimal modulation schemes for NSSs and provide hardware results of the proposed signal multiplexing techniques.

This work provides the following contributions:

  • An optimization approach is provided for extending the existing MCEMIC scheme to the case of multi-level and multi-frequency signals with a NSS.

  • A novel concept of PSD preservation is introduced in the optimization framework to satisfy the MBOC(6,1,1/11) PSD requirement in interoperable L1-band open civilian service signals.

  • A practical system engineering approach is presented for determining the modulation scheme, power-sharing options, and optimum frequency offset (for multi-frequency cases).

  • The effectiveness of the proposed multiplexing approach is demonstrated by utilizing actual hardware findings for multiplexing multi-level NavIC L1-band open service signals and NSSs over a single frequency and over multiple frequencies in the NavIC L1 frequency band.

In the following sections, this article presents the proposed multi-level multiplexing method, elaborating its conceptual and implementation details, system engineering procedure, and hardware performance.

SYSTEM MODEL

NavIC transmits interoperable open civilian service signals over the L1 frequency band via second-generation NavIC satellites. These multi-level signals have a constant envelope modulation (Upadhyay et al., 2024; Upadhyay & Bhadouria, 2021; Upadhyay et al., 2020) and meet the PSD criteria of MBOC, i.e., MBOC(6,1,1/11), which is essential for interoperability (Hein et al., 2006).

We represent a multi-level signal (sSBOC(t)) as follows:

sSBOC(t)=sSBOCp(t)+jsSBOCd(t)1

where sSBOCd(t) and sSBOCp(t) are the data and pilot components of sSBOC(t). We represent the data and pilot components of the multi-level signal as follows:

sSBOCp(t)=αsBOC(1,1)p(t)βsBOC(6,1)p(t)2

sSBOCd(t)=γsBOC(1,1)d(t)+ηsBOC(6,1)d(t)3

where α, β, γ, and η are the coefficients of the BOC(1,1) and BOC(6,1) components, which satisfy the following relationships:

α+β+γ+η=1;η=αβγ;α+γ=1011;β+η=1114

η is a parameter that depends on α, β, and γ and controls the envelope of the composite signal. As shown in Equations (1)–(4), the envelope of the multi-level signal has a constant modulus, i.e., |sSBOC(t)| = 1, and satisfies the MBOC PSD criteria. Time-domain plots and correlation properties of the data and pilot components of the multi-level signal are displayed in Figure 1, showing that both the data and pilot components are multi-level and have a non-smooth main lobe of the auto-correlation curve.

FIGURE 1

Characteristics of multi-level data and pilot signals; time-domain plots of multilevel data and pilot signals (left); autocorrelation plots of multi-level data and pilot signals (right)

Multi-level modulation components make it difficult to include additional signals while maintaining the envelope of the composite signal. Although research on constant-envelope multiplexing of multi-level signals is limited, recent studies have presented an MCEMIC technique to add signal power deviation in order to maximize multiplexing efficiency. The MCEMIC approach has higher multiplexing effectiveness than CEMIC for bipolar signals over a single frequency while preserving signal power (Bhadouria et al., 2022).

Here, we extend the MCEMIC technique for multiplexing multi-level signals. Furthermore, to satisfy the power ratio given in Equation (4) for the multi-level signal to maintain the MBOC PSD, we fuse constraints related to the power ratio in the optimization framework of the MCEMIC technique to support backward compatibility for the already planned multi-level signal. Figure 2 shows the overall block-level implementation of the onboard MCEMIC technique based on a satellite navigation payload.

FIGURE 2

Block diagram of a typical satellite navigation payload with the MCEMIC technique

Figure 2 shows a transmitter in which four signals are multiplexed via MCEMIC to create a constant-envelope composite signal (s1(t),s2(t),s3(t), and s4(t)). The composite signal (s(t)) is up-converted by an RF oscillator and amplified once (HPA). Generating a composite signal (sRF(t)) with a constant envelope maximizes HPA efficiency. A bandpass filter (BPF) limits out-of-band emission and transmits in-band signals without distortion. We propose adding NSSs to the NavIC L1 multi-level signal. NSSs must be multiplexed with the multi-level signal. The satellite navigation payload must multiplex multi-level data (multi-level-D), multi-level pilot (multi-level-P), NSS-data (NSS-D), and NSS-pilot (NSS-P) components. The multiplexed composite signal (s(t)) shown in Figure 1 is represented as follows:

s(t)=i=14si(t)+IM(t)5

where:

si(t)=n=cnipi(tnRci)6

Here, cni is the product of the spreading code and the data of the ith signal, and Rci is the code rate of the spreading code of the ith signal. IM(t) is the superposition of multiple intermodulation terms inserted to ensure that the envelope of s(t) has a constant modulus. The pulsed signal pi(t) has a non-zero amplitude for t[0,1/Rci) and can be represented as follows:

pi(t)=k=0Mi1akiψTsi(tkTsi)7

where Mi is the modulation index of the ith signal and Tsi{1/(MiRci)} is the sub-chip interval of the ith signal. ai defines the shape vector of length Mi for the ith signal, and aki is the kth element. ψTsi(t) is a unit rectangular pulse of duration Tsi.

Considering si(t) of the form si(t)=n=Picnipi(tnRci)ej(2π(fif0)t+ϕi) in

Equation (5), we obtain the following:

s(t)=i=14n=Picnipi(tnRci)ej(2π(fif0)t+ϕi)+IM(t)8

where Pi is the power of the ith signal; fi and φi are the frequency and initial phase of the ith signal, respectively; and f0 is the common center frequency for all signals. We impose the condition fi = f0; i ∈ [1,4] when multiplexing signals over a single frequency. This condition may not hold when multiplexing signals over multiple frequencies.

We define the general form of the MCEMIC method to obtain the formulation of IM(t) such that s(t) = Ae, where A is an arbitrary constant taken as A = 1 with no loss of generality and ϕ is an arbitrary phase. Based on Equation (5), IM(t) can be represented as follows:

IM(t)=ejϕi=14n=Picnipi(tnRci)ej(2π(fif0)t+ϕi)9

The solution of Equation (9) is nontrivial; multiple values of the design parameters Pi and ϕi satisfy Equation (9) simultaneously. However, with the assumption that all of the onboard signals of the form shown in Equation (7) are synchronized and periodic, the span of ai and ej(2π(fif0)t) becomes finite. Hence, Equation (9) can be solved by posing it in an optimization framework with Pi and ϕi as the design (optimization) parameters for a given ai and fi. For a uni-level signal, ai is bipolar, i.e., aki=±1;k[0,Mi1], and for multi-level cases, ai takes Ki(KiMi) values such that 0<aki1;k[0,Mi1]. In the case of single-frequency transmission, ej2π(fif0)t1; whereas for multi-frequency cases, ej2À(fif0)tej2À(fif0)nTs, 0 ≤ nL provided that L {= 1/(fif0)Ts} is an integer, where Ts{=1/LCM(Rci)} is the sampling duration. Here, LCM(·) is defined as the least common multiple. The intermodulation term (IM(t)) is also a multi-level chip sequence that is orthogonal to the signal si(t) (Yao et al., 2017) and satisfies the following:

E(IM(t)si*(t))=ciHPλ=010

where ci is an F×1(FLi=14Ki) vector defined as ci=cniaiej(2π(fif0)nTs). P is a positive definite diagonal matrix, and λ is the Nλ × 1 realization of IM(t). Furthermore, it is shown that ciHλ=0; the basis of λ, i.e., C¯, is obtained from Gram-Schmidt orthonormal expansion of the matrix C = [c1, c2,..., c4] (Leon et al., 2012), which results in an augmented matrix C0=[C,C¯].

It is important to note that the cardinality of the vector ci, i.e., F, is critical for maximizing the multiplexing efficiency. The signal type determines the cardinality of ci ; for example, if ci ; i ∈ [1,4] makes the orthonormal basis and strict equality is held, i.e., F=Li=14Ki.

Bipolar single-frequency multiplexing has less cardinality than multi-level multi-frequency multiplexing. Signal multiplexing for multi-level signals requires care, as this process is more complicated. When enumerating signal value combinations, we must consider the fact that multi-level data and pilot signals are not independent. The next segment discusses the challenges that arise in multi-level multiplexing design.

In matrix notation, Equation (5) is written as follows:

i=14si(t)Cws;λC¯wim11

Hence, s(t)C0w, where w=[wsT,wimT]T and ws=[P1,,P4]T.

The MCEMIC-based cost function for reducing the power of intermodulation terms and minimizing the deviation in the power of the desired signals is formulated as follows:

C(W)=12Λwb212

where b=[ejϕi,Z]T. Z is a zero vector with length Nλ, and ϕi is a vector containing the initialization phases of ws weights. Λ is an L × L diagonal matrix that preserves the power of the desired signals to support backward compatibility, given by the following:

Λ=[ΛE00I]13

where L is the length of the vector w, which is defined by L = 4 + Nλ. ΛE is a 4 × 4 power-sharing preservation matrix denoted by the following:

ΛE=[ε1P10000ε2P200000ε4P4]14

where ε1 is the penalty factor to minimize the deviation of power-sharing of the ith desired signal.

The optimization is formulated as follows:

argminw(C(w))15

such that:

|C0w|=116

However, we add another constraint for multi-level signals in Equations (15) and (16), which we require in order to meet the MBOC PSD criteria for interoperability in the L1 frequency band. According to Equation (4), this constraint is given as follows:

α+γβ+η=1017

Considering ws(1) and ws(2) as the weights of the sSBOCp(t) and sSBOCd(t) signals, respectively, we can use Equation (1) to obtain the following:

α+βγ+η=ws(1)ws(2)=6446=ζSBOC18

Hence, we extend the MCEMIC method for multi-level and multi-frequency signals with an additional multi-level-based PSD constraint. Using the Lagrange method (Pierre, 1986), the cost function for optimization is represented as follows:

(w)=C(w)+λ12sHGs+λ2wHDw19

where D is derived based on Equation (18):

D=[DE000]20

DE is a 2 × 2 matrix, given by the following:

DE=[1ζSBOCζSBOCζSBOC2]21

The second term in Equation (19) arises from the constant-modulus constraint given in Equation (16) (Yao et al., 2017). Here, G{=diag(g1,g2,,gNλ)} is a diagonal matrix whose entries are given by the following:

gk={1,kG+1,kG22

where G+ represents the L / 2 higher values of the magnitude-wise sorted values present in s and, similarly, G represents the L / 2 lower values in s.

The gradient of C(w) is given by the following:

wC(w)=κ1(ΛTΛwΛTb)+κ2(C0HGs)+κ3Dw23

The gradient-descent-based iterative update is given as follows:

wi+1=wiμ(wC(w))24

where μ is a parameter that controls the step size, κ1 is a weight factor for the receiver transparency error, κ2 is the constant-envelope error weight factor, and κ3 is the PSD error weight factor in the proposed optimization framework. It is critical to observe that the magnitude of the constant-modulus error term is greater than that of the other errors. Hence, it is intuitive to maintain higher values for κ1 and κ3 compared with κ2 . Accordingly, we set μ = 1e−5, κ1 = 10, κ2 = 1, and κ3 = 10 in the analysis.

It is essential to note that the proposed algorithm is an iterative-type method. Hence, careful attention is needed when selecting the initial values of the optimization parameter. Not all values provide equal multiplexing efficiency. Moreover, a solution with higher efficiency may not have practical relevance for the overall system performance. For example, the high-efficiency multiplexing solution may reduce the power-sharing of one or more signals below the acquisition/demodulation threshold. Hence, incorporating the system engineering aspects into the signal design requires a practical solution. The following section describes the criteria for selecting the initial power-sharing of the desired signal. Moreover, it also considers the requirements to minimize inter- and intra-system interference by selecting the optimum modulation and frequency of the proposed NSS in the NavIC L1 frequency band.

SYSTEM ENGINEERING ASPECTS FOR SIGNAL DESIGN

This section explains details of the system engineering aspects that are essential for NSS design. We explore the link design to ensure the availability of the required minimum received isotropic power (RIP) level of the NSS.

Selection of Weights via Link Design

We characterize the satellite navigation signals by their minimum RIP levels. It is important to note that most GNSS systems use direct-sequence spread-spectrum signals. The RIP level of the signals is designed to be below the thermal noise floor level of the receiver, meaning that the pre-correlation signal-to-noise ratio at the receiver input has a considerable negative value, i.e., on the order of approximately –20 dB. Thus, the selection of weights for the desired signals, i.e., ws, is a dominant procedure for onboard composite signal design. This work uses link design to estimate the initial value of ws to meet the required minimum RIP level at the receiver end. Table 1 shows the minimum RIP levels of various interoperable open civilian service signals with MBOC PSD in the L1 frequency band.

View this table:
TABLE 1

Minimum RIP Level (in dBW) of Various Interoperable Open Civilian Signals in the L1 Band

IGSO: inclined geosynchronous orbit; MEO: medium Earth orbit

We observe that the worst-case RIP value for the pilot signal is –162.25 dBW for interoperable signals. Hence, considering the power levels of various interoperable signals, the NavIC multi-level pilot signal requires a minimum RIP level of –162.25 dBW. Based on this requirement, two ratios for power-sharing between the NSS-D and NSS-P are selected, i.e., 1/3 and 1/2; details are provided in Table 2.

View this table:
TABLE 2

Calculation of the Minimum RIP Level (in dBW) for Multi-Level Pilot and NSS-P Signals

EIRP: effective isotropic radiated power

The power-sharing of both multi-level signals and the NSS must ensure suitable signal acquisition and tracking performance. Hence, it is essential to note that equal power-sharing between multi-level signals and the NSS is the optimum choice. Once the RIP levels of the desired signals are estimated, the next step in the signal design is to minimize inter- and intra-system interference. In this work, we consider two cases for the NSS design. First, the NSS is multiplexed at the exact center frequency of the multi-level signal, i.e., 1575.42 MHz; second, the NSS is multiplexed at a higher frequency with an offset of 15.345 MHz. A cosine phasing BOC, BOCc(15,2.5), yields a minimum inter- and intra-system interference value for single-frequency multiplexing. For multi-frequency multiplexing, BPSK(5) modulation with a 15.345-MHz-higher frequency offset with respect to the 1575.42-MHz center frequency shows minimum inter- and intra-system interference. Details are provided in Appendix I. Hence, we pursue these two signal types as candidates for the NSS in system design.

RESULTS AND DISCUSSION

Comparison of MCEMIC and CEMIC Methods for Multi-Level Signals

To compare the performance of MCEMIC with that of the existing CEMIC method (Yao et al., 2017), we simulated multiplexing of the four signals depicted in Figure 3. It can be observed that both signal 1 and signal 2 have multiple levels. In addition, the initial power distribution among signals 1, 2, 3, and 4 is 20%, 30%, 20%, and 30%, respectively. Furthermore, signal 1 and signal 2 are maintained in the in-phase channel, whereas signal 3 and signal 4 are maintained in the quadrature channel.

FIGURE 3

Time-domain plots of four signals

We investigate both single- and multi-frequency cases. As shown in Figure 4, the proposed MCEMIC methods have a higher multiplexing efficiency than the existing CEMIC method (Yao et al., 2017). The first four bars represent the power distribution for the desired signals, while the fifth bar represents the total power of the intermodulation signals. For case scenarios involving a single frequency, MCEMIC is 1.5% more efficient than CEMIC. Moreover, MCEMIC achieves a 0.8% improvement in multiplexing efficiency for multi-frequency cases.

FIGURE 4

Comparison of MCEMIC and CEMIC methods for multi-level signal multiplexing: single-frequency multiplexing (left) and multi-frequency multiplexing (right)

MCEMIC-BASED SIGNAL DESIGN AND PERFORMANCE ANALYSIS

This section discusses the results of the proposed NSS in the NavIC L1 frequency band with the existing NavIC multi-level signal. The phasing of the multi-level data and multi-level pilot components has not been changed to maintain backward compatibility, and the power-sharing ratio between the multi-level data and multi-level pilot components was not modified to meet the MBOC PSD. We analyze two options in light of L1 congestion. The first option is multiplexing multi-level signals and the NSS over a single frequency, where the NSS and multi-level signals have the same center frequency. Here, we use split-spectrum approaches to explore frequency diversity. The second option is multiplexing multi-level signals and the NSS over multiple frequencies. In this case, a signal frequency offset isolates the PSDs. Based on interference analysis, we explore two modulation methods for the NSS. We suggest cosine phasing BOC, i.e., BOCc(15,2.5), for the single-frequency case and BPSK(5) for the multi-frequency case with a 15.345-MHz NSS offset.

The link architecture determines the NSS data-to-pilot signal power-sharing ratio, i.e. ζnss, and GNSS receivers use the pilot signal instead of the data signal for improved acquisition and tracking performance. The receiver uses a coherent phase-locked loop, as the pilot signal contains no data. This approach delivers a 6-dB relative advantage. In addition, the receiver uses a longer integration interval to acquire/track the pilot signal, leading to higher pilot signal power-sharing.

Single-Frequency and Multi-Level Multiplexing Analysis

The NSS-D and NSS-P signals are modulated with BOCc(15,2.5) for a single-frequency multiplexing option. Four signals must be multiplexed to create the constant-envelope composite signal. The multi-level data and pilot signals are multi-level, whereas the NSS-D and NSS-P signals are bipolar. To evaluate the performance of the proposed multiplexing method, we explore a total of four power-sharing combinations between existing multi-level signals and the NSS (multi-level: 30%, 40%, 50%, and 70%; NSS: 70%, 60%, 50%, and 30%). Because the NSS-D and NSS-P components can have four different value combinations in the initial phases, we evaluate sixteen possible combinations for the proposed scheme. Table 3 displays the findings for ζnss = 1/3. For ζnss = 1/2, details are provided in Appendix II of this manuscript. However, it is observed that the performance for ζnss = 1/2 is inferior when considering the overall system requirements. Hence, we consider ζnss = 1/3 for the analysis. We studied various power-sharing options for individual signals, evaluating all potential combinations of NSS-D and NSS-P phasing. Case 4 shows the most efficient multiplexing, but case 15 shows optimal performance. Case 15 has nearly comparable multi-level and NSS powers, at 41% each. Figure 5 displays the simulation constellation diagram and PSD for case 15. The composite signal has a constant envelope and incorporates multi-level modulation and BOCc(15,2.5).

FIGURE 5

Constellation (left) and PSD (right) for single-frequency multiplexing with ζnss = 1/3

View this table:
TABLE 3

Power-Sharing Options (in %) for Various Phase Relationships of NSS-D and NSS-P Signals with ζnss = 1/3 for Multiplexing with Multi-Level Signals Over a Single Frequency

η denotes the multiplexing efficiency; I indicates the in-phase channel; Q denotes the quadrature channel.

It is important to observe that the number of constellation points is significantly lower than the expected value, i.e., 32 instead of 64. This difference is primarily due to the dependence between the multi-level data and pilot signals. Because these signals are not independent, we must consider this condition when enumerating the possible combinations of signals to generate a matrix C0. In this case, any mismatch results in a high correlation loss of up to 3 dB, rendering the overall multiplexing technique ineffective. Furthermore, because the number of effective constellation points is reduced, the degrees of freedom for optimization are decreased, resulting in slightly lower multiplexing efficiency.

Multi-Frequency and Multi-Level Multiplexing Analysis

Based on the spectral compatibility analysis, we consider BPSK(5) modulation offset by 15.345 MHz from the 1575.42-MHz center frequency on the higher side as the desired option for multi-frequency multiplexing. Similar to single-frequency multiplexing, this case also considers two values of ζnss; i.e., ζnss = 1/3 and ζnss = 1/2. Table 4 shows the results for ζnss = 1/3. We observe that case 15 results in optimum performance based on the system requirements. Furthermore, the multi-frequency analysis for case 15 achieves approximately 1.7% higher efficiency than single-frequency multiplexing. The power-sharing ratio between multi-level data and multi-level pilot signals is preserved for the case of MCEMIC. In contrast, for the case of CEMIC, the power-sharing ratio changes by approximately 1%, thus violating the PSD requirement. Figure 6 shows the simulated constellation plot and the PSD of the proposed option for the multi-frequency multiplexing case. We used a sampling rate of 61.38 MHz to simulate this signal.

FIGURE 6

Constellation (left) and PSD (right) for multi-frequency multiplexing with ζnss = 1/3

View this table:
TABLE 4

Power-Sharing Options (in %) for Various Phase Relationships of NSS-D and NSS-P Signals with ζnss = 1/3 for Multiplexing with Multi-Level Modulation Signals Over Multiple Frequencies

η denotes the multiplexing efficiency; I represents the in-phase channel; Q represents the quadrature channel.

It is important to observe that the number of constellation points is significantly less than the expected value, i.e., 64 against 256 possible constellation points. As already mentioned, the multi-level data and multi-level pilot signals are dependent. Moreover, the sampling of carrier results is performed in order pairs, which causes the sampled offset carrier vector to be correlated across time, resulting in a further reduction in the constellation points. Consequently, we must use additional caution when enumerating the possible combinations.

Hardware Implementation Results

We verified the performance of the proposed multiplexing technique on hardware for case 15 with ζnss = 1/3. For this, we generated a composite signal through a vector signal generator (Keysight Technologies, E8267D) and applied a vector signal analyzer (Rohde & Schwarz, FSW43) to demodulate the signal. Table 5 presents the performance of the proposed method for both single- and multi-frequency multiplexing. An error vector magnitude (EVM) is typically used as a performance metric to characterize satellite navigation payloads (Upadhyay et al., 2014). We observed that the measured EVM is less than 10%, which is within the required performance. Other modulation-related parameters are within the desired limits; more details are provided in Appendix III.

View this table:
TABLE 5

Hardware Results for Single- and Multi-Frequency Multiplexing with ζnss = 1/3 for Case 15

I represents the in-phase channel; Q represents the quadrature channel. rms: root mean square.

CONCLUSION

The signal multiplexing approach proposed herein adds an NSS to the existing NavIC L1-band open civilian service signals in a comprehensive way. We used the MCEMIC multiplexing technique to multiplex multi-level signals over a single frequency and multiple frequencies while preserving the interoperability of NavIC L1-band open service signals with other GNSS L1-band open service signals. The proposed MCEMIC method outperformed the existing CEMIC method with respect to multiplexing efficiency by 1.5% and 0.8% for multi-level single- and multi-frequency cases, respectively. The proposed MCEMIC preserves the power-sharing ratio between the multi-level data and pilot signals. At the same time, the CEMIC method results in a deviation of approximately 1% in the desired power-sharing ratio. We analyzed candidate modulation schemes and power-sharing options for multiplexing signals over a single frequency and multiple frequencies with an optimum frequency offset. The multi-frequency multiplexing technique achieves slightly higher efficiency than the single-frequency multiplexing technique. Moreover, we proposed a BPSK(5) modulation scheme for the NavIC L1-band NSS with data and pilot components, with a power ratio of 1/3, multiplexing with multi-level NavIC L1-band open civilian service signal over multiple frequencies at a 15.834-MHz-higher frequency offset with respect to the 1575.42-MHz center frequency.

HOW TO CITE THIS ARTICLE

Bhadouria, V. S., Upadhyay, D. J., Majithiya, P. J., & Bera, S. C. (2025). Candidate design of new service signals in the NavIC L1 frequency band. NAVIGATION, 72(2). https://doi.org/10.33012/navi.695

ACKNOWLEDGMENTS

The authors are grateful to Shri. Sumitesh Sarkar, Associate Director of SAC, and Shri. Nilesh Desai, Director of SAC, ISRO, for their support, guidance, and encouragement during this work.

APPENDIX I Spectral Compatibility of NSSs with Other GNSS Signals

Interference from undesired signals affects the quality of the received signal and is quantified in terms of the spectrum separation coefficient. With Gs(f) and Gi(f) denoting the normalized PSD of the desired and interfering signal, respectively, the spectrum separation coefficient, κssc, between the desired and the interfering signal is given by the following:

κssc=βr2βr2Gs(f)Gi(f)df(x)

The definition of κssc considers the assumption of longer spreading codes to neglect weak cross-correlation degradation. From (x), we observe that the value of κssc between the NSS and the existing signals should be as low as possible. Table I.1 shows κssc values between the NSS and all existing GNSS signals in the L1 frequency band for a bandwidth of 30.69 MHz, detailing the interference caused by the NSS on all possible existing signals over the L1 band. The first column of Table I.1 indicates the modulation type and its respective frequency offset from the L1-band center frequency (1575.42 MHz).

View this table:
TABLE I.1

κssc (dB/Hz) Values Between NSS and GNSS Signals in the L1 Band for 30.69-MHz Bandwidth

The frequency offset was calculated with respect to 1575.42 MHz.

As shown in Table I.1, for a single-frequency case, BOCc(15,2.5) obtains the best spectral isolation from all present or planned open service and restricted service signals in the L1 frequency band. The results indicate that the subcarrier at 15.345 MHz yields the best spectral isolation, which ensures inter-compatibility of the proposed NSS with other signals in the same frequency band, as this is the prime requirement for all service signals. Hence, using 15.345 MHz as a frequency offset for the multi-carrier case is an intuitive choice for obtaining optimum results.

APPENDIX II Results for ζnss =1/2

Table II.1 and Table II.2 present results for the ratio between the NSS-D and NSS-P signals when ζnss =1/2 for the NSS design.

View this table:
TABLE II.1

Power-Sharing Options (in %) for Various Phase Relationships of the NSS-D and NSS-P Signals with ζnss = 1/2 for Multiplexing with the Multi-Level Signal Over a Single Frequency

η denotes the multiplexing efficiency; I represents the in-phase channel; Q represents the quadrature channel.

View this table:
TABLE II.2

Power-Sharing Options (in %) for Various Phase Relationships of the NSS-D and NSS-P Signals with ζnss = 1/2 for Multiplexing with the Multi-Level Signal Over Multiple Frequencies

η denotes the multiplexing efficiency; I represents the in-phase channel; Q represents the quadrature channel.

APPENDIX III Hardware Implementation Results for ζnss =1/3 and Case 15

Single-Frequency and Multi-Level Case

We verified the performance of the proposed multiplexing technique on hardware for case 15 with ζnss =1/3. For this, we generated a composite signal through a vector signal generator (Keysight Technologies, E8267D) and used a vector signal analyzer (Rohde & Schwarz, FSW43) to demodulate the signal. Figures III.1 and III.2 show the measured PSD and the measured constellation, respectively. An EVM is typically used as a performance metric to characterize satellite navigation payloads (Upadhyay et al., 2014). We observed that the measured EVM is less than 10%, which is within the required performance.

FIGURE III.1

Hardware results for the PSD of single-frequency multiplexing with ζnss =1/3

FIGURE III.2

Hardware results for the constellation of single-frequency multiplexing with ζnss =1/3

Multi-Frequency and Multi-Level Case

Figures III.3 and III.4 show the measured PSD and constellation for case 15 with ζnss = 1/3, respectively. We observed that the measured EVM is less than 10%.

FIGURE III.3

Hardware results for the PSD of multiple-frequency multiplexing with ζnss =1/3

FIGURE III.4

Hardware results for the constellation of multi-frequency multiplexing with ζnss = 1/3

This is an open access article under the terms of the Creative Commons Attribution License, which permits use, distribution and reproduction in any medium, provided the original work is properly cited.

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