Enhancing Ranging Precision in OFDM-Based LEO Navigation: Signal Design and Receiver Implementation

  • NAVIGATION: Journal of the Institute of Navigation
  • January 2026,
  • 73
  • navi.741;
  • DOI: https://doi.org/10.33012/navi.741

Abstract

Emerging low Earth orbit (LEO) satellites offer new opportunities for navigation augmentation. This paper investigates the potential of orthogonal frequency division multiplexing (OFDM) signals for LEO satellite navigation, focusing on challenges arising from carrier frequency offsets (CFOs) in low signal-to-noise ratio (SNR) environments. We comprehensively analyze the navigation properties of OFDM signals, assessing two synchronization sequence (SS) candidates for their resilience against CFOs. Our findings suggest that the m-sequence effectively mitigates integer CFOs while minimally impacting the receiver’s ranging estimation in the presence of fractional CFOs. Additionally, we introduce an SS detection architecture that integrates differential coherent accumulation (DCA) with a near-optimal likelihood ratio test (NOLRT). This DCA-NOLRT-based LEO receiver enhances detection reliability and sensitivity, effectively managing residual fractional CFOs and improving detection probabilities in low-SNR scenarios. Numerical simulations and terrestrial experiments validate the proposed framework’s capability to minimize CFO-induced ranging errors, even under demanding conditions in LEO navigation scenarios.

Keywords

1 INTRODUCTION

Navigation challenges, particularly those related to spoofing and multipath interference in urban areas, have persisted despite significant advancements over the past decades. Low Earth orbit (LEO) satellites, which operate at lower altitudes than medium Earth orbit or geostationary satellites, aim to enhance communication services while offering considerable benefits for navigation augmentation. These benefits include shorter signal propagation distances and increased signal power (Ardito et al., 2019), which are particularly advantageous in complex urban settings.

LEO satellites utilize three main types of navigation signals: global navigation satellite system (GNSS)-like signals (Wang et al., 2018; Wu et al., 2022), self-designed signals (Deng et al., 2023; Yin et al., 2019), and orthogonal frequency division multiplexing (OFDM) signals, which are typically used for communications (Graff & Humphreys, 2024; Neinavaie & Kassas, 2023). For instance, the Luojia-1A satellite (Wang et al., 2018), which broadcasts a GNSS-like signal, was launched to test its effectiveness in enhancing positioning accuracy and real-time kinematic performance, taking advantage of the satellite’s high velocity and close proximity to Earth. However, this approach does not support high-speed data transmission, thus limiting its applicability in scenarios that demand high navigation data rates, such as space exploration, communication, and high-precision surveying (Yang et al., 2020). Alternatively, a broadband multicarrier-based navigation modulation using OFDM with a binary offset carrier (BOC) scheme has been proposed by Deng et al. (2023), whereas a multiscale non-orthogonal multiple access (MS-NOMA) technique has been proposed by Yin et al. (2019). Both methods demonstrate strong potential for integrating positioning and communication signals, although the widespread adoption of such custom modulation schemes by existing LEO constellations may take time owing to compatibility and relevant hardware upgrade considerations. OFDM signals, recognized for their robustness against multipath interference, capability for high-speed data transmission, and low implementation complexity, have found applications in popular commercial LEO constellations such as Starlink, OneWeb, and Orbcomm (Kassas et al., 2023). The increasing deployment of LEO satellites globally has sparked interest in exploiting OFDM signals for long-term navigation applications in next-generation GNSSs (Dai et al., 2010). As a result, the significant limitations of GNSS-like and self-designed signals, along with the inherent benefits of OFDM signals, make OFDM a promising option for LEO navigation applications.

However, employing OFDM in LEO ranging and navigation tasks introduces unique challenges that require careful consideration. A primary concern is the severe carrier frequency offsets (CFOs) caused by the rapid relative motion between the satellites and ground-based receivers. Such CFOs lead to time and frequency synchronization errors (Fan et al., 2021), critically affecting the bit error rate (BER) and degrading the ranging accuracy outcomes—key metrics in LEO navigation (Huang et al., 2021). Given the stringent requirements for precise time-frequency synchronization in ranging and navigation tasks and the fact that navigation signals experience much larger CFOs, there is an urgent need for a robust strategy to effectively address these CFOs.

The correction algorithms of CFOs have been extensively discussed within the context of third-generation partnership project (3GPP) long-term evolution (LTE) and fifth-generation new radio (NR), which generally fall into two categories: transmitter-side techniques and receiver-side techniques. Transmitter-side techniques involve custom training sequences or null subcarriers (Gul et al., 2012, 2015; Meng et al., 2020), which fundamentally address CFOs but require specific signal design modifications, potentially adding time costs when various OFDM signal parameters are adapted in current LEO systems. In comparison, receiver-side techniques rely on the time or frequency properties of successive repeated symbols, cyclic prefixes (CPs), or oversampling (Choi et al., 2010; Jeon et al., 2011; Van de Beek et al., 1997). Additionally, an OFDM tracking loop has been described by Shamaei and Kassas (2021) to handle subtle Doppler shifts between adjacent OFDM symbols. Nevertheless, these methods generally require a large number of OFDM symbols to achieve satisfactory performance.

Furthermore, the algorithms previously mentioned (Choi et al., 2010; Gul et al., 2012, 2015; Jeon et al., 2011; Meng et al., 2020; Shamaei & Kassas, 2021; Van de Beek et al., 1997) primarily address Doppler shifts in terrestrial systems, which have a limited CFO range. This range is inadequate for LEO navigation systems, which experience significantly higher relative velocities compared with ground-based user movements. To address the challenge of large-CFO mitigation, a two-step approach has been proposed by Kim et al. (2001), based on a timing synchronization algorithm that separately compensates for fractional and integer CFOs, effectively extending the CFO compensation range. Moreover, to specifically handle the higher Doppler shift encountered in satellite systems, the characteristics of the Zadoff–Chu (ZC) sequence and the satellite channel have been utilized by Huang et al. (2021). This method also adheres to the two-step procedure, in which fractional CFOs are estimated first, followed by integer CFOs.

To date, there has been limited discussion on the inherent properties of the synchronization sequences (SSs) and receiver structures of OFDM in low signal-to-noise ratio (SNR) scenarios regarding their resistance to CFO-induced ranging shifts. This gap largely arises because most anti-CFO methods depend on precise CFO estimation and subsequent compensation, which are primarily effective in mediumto high-SNR scenarios (above –15 dB) (Laourine et al., 2007). Consequently, the techniques developed by Kim et al. (2001) and Huang et al. (2021) may not be well suited for LEO satellite-to-ground platforms. These platforms experience high path loss due to long propagation distances (Zhen et al., 2020), resulting in significantly lower SNRs compared with terrestrial networks. Such reductions in SNR can lead to inaccuracies in CFO estimations, ultimately causing residual CFOs in the received signal. To the best of our knowledge, there is still a need for a comprehensive comparison of the inherent properties of different sequences and the development of an SS detection structure that enhances large-CFO resistance in low-SNR scenarios, without relying on precise CFO estimation.

Motivated by the challenges highlighted above, this paper presents a concise strategy for tackling large CFOs from a system perspective, addressing both the transmitter and receiver sides for effective ranging. On the transmitter side, we extend our previous work (He et al., 2024) by demonstrating the superiority of OFDM modulation over other candidate schemes and showing that the m-sequence possesses stronger inherent resistance to both fractional and integer CFOs. Based on these findings, we specify the structure of the navigation signal to be transmitted, integrating m-sequences in the OFDM navigation signal. On the receiver side, we improve time-of-arrival (TOA) estimation by combining a near-optimal likelihood ratio test (NOLRT) detector (Yin et al., 2020) with the differential coherent accumulation (DCA) algorithm (Qiu et al., 2012) in the receiver, effectively resolving the ambiguity issues inherent in DCA. This DCA-NOLRT architecture not only boosts the SS detection probability by enhancing the receiver sensitivity but also effectively manages fractional CFOs in LEO systems, which typically operate in low-SNR scenarios.

Compared with existing literature, the main contributions of this work are highlighted as follows:

  1. Unlike the work by Gul et al. (2015) and Huang et al. (2021), we provide a comprehensive assessment of the inherent properties of both SS candidates in managing fractional and integer CFOs. Our analysis reveals that the m-sequence exhibits superior CFO resistance, making it particularly suitable as an SS for OFDM navigation signals in LEO satellite systems.

  2. We introduce an DCA-NOLRT-based SS detection architecture to enhance the receiver sensitivity and capability to achieve accuracy under relatively low SNRs. In contrast to the work by Shamaei and Kassas (2021), which addresses fractional CFOs only during the tracking stage, the proposed SS detection architecture suppresses the impact of fractional CFOs early on, ensuring timely and reliable ranging of the receiver.

  3. Building on our previous work (He et al., 2024), the reliability of our proposed LEO navigation system is validated through extensive simulations and terrestrial experiments. These simulations incorporate CFOs, low SNRs, and LEO channel variations to extensively assess the system’s ranging accuracy. Despite the challenges of replicating LEO channel impairments on the ground, our experimental results confirm that the framework significantly minimizes CFO-induced ranging errors, demonstrating robust performance in extreme conditions.

The remainder of this paper is organized as follows: Section 2 presents the signal model and analyzes several navigational properties of OFDM signals. Section 3 examines the performance of two SS candidates in handling CFOs and discusses the rationale for selecting the m-sequence as the navigation signal, along with a detailed description of our LEO navigation signal structure. Section 4 introduces the DCA-NOLRT-based LEO receiver. Section 5 presents the results of our simulation and terrestrial experiment and their analysis. Finally, Section 6 concludes this paper.

2 BASEBAND OFDM SIGNAL MODEL

Here, the baseband models of the OFDM modulation scheme are introduced. As shown in Figure 1, the OFDM architecture enables efficient parallel data transmission by dividing the available frequency spectrum into M orthogonal subcarriers. These subcarriers are closely packed with partial overlap at a spacing of f0, each modulated with a segment of the navigation message, modeled as follows:

Figure 1

Block diagram of the OFDM transmitter and receiver framework. S/P and P/S denote serial-to-parallel and parallel-to-serial conversion, respectively.

s(t)=k=0M1d(k)ej2πfkt 1

where fk=kf0 is the frequency of the k-th subcarrier and the baseband modulated data {d(k)}k=0M1 represent the m-sequence or navigation messages, depending on the transmission time t.

Modern OFDM signals generate discrete-time samples s[n] by first zero-padding the sequence {d(k)}k=0M1 to length N as follows:

dzp(k)={d(k),0kM10,MkN1 2

The OFDM signal is then obtained by applying the inverse fast Fourier transform (IFFT) with N points:

s[n]=k=0N1dzp(k)ej2πnkN,0nN1 3

This represents the time-domain discrete-time OFDM signal after the IFFT, where the original M subcarriers are mapped into N time samples, effectively oversampling the signal at a rate of Ts=1Nf0 to improve spectral shaping. A CP is then appended to s[n] at the beginning of each OFDM symbol, resulting in scp[n] for transmission.

The discrete received signal r[n], sampled at the same frequency as the transmitter after down-conversion, is given by the following:

r[n]=h[n]scp[n]+w[n]=k=0N1h(n)dzp(k)ej2πf^k(nκ)+w[n] 4

where h[n] denotes the channel impulse response, w[n] is the noise term, κ denotes the real TOA, which is regarded as the propagation delay between the onboard transmitter and the terrestrial receiver, f^k is the frequency of the k-th subcarrier of the received signal, and Δf=f^kfk denotes the existing fractional CFO.

3 TRANSMITTER

In this section, we introduce the detailed structure of our OFDM navigation signal design, focusing specifically on ranging tasks under the demanding conditions associated with rapid LEO motion and low SNRs. We then explore several navigation properties, including potential ranging accuracy, anti-interference capability, and power efficiency, to assess the suitability of OFDM modulation for navigation tasks.

The first block of the time-domain signal s(t) transmitted by LEO satellites is the SS, which is crucial for enabling reliable ranging estimation. We further investigate the inherent properties of candidate SSs within the OFDM framework to evaluate their effectiveness in maintaining ranging accuracy in the presence of both fractional and integer CFOs. Our comprehensive assessment demonstrates that the m-sequence significantly outperforms the ZC sequence, leading to its selection as the SS in our OFDM-based navigation signals.

3.1 Navigation Signal Structure

In this section, we introduce the frame structure of the OFDM navigation signal transmitted from LEO satellites. As illustrated in Figure 2, a LEO navigation frame consists of two primary components: the SS block (SSB) and the data block. The SSB primarily facilitates time synchronization between the locally generated replica and the receiver, which is essential for accurate recovery of navigation messages conveyed by the data block. Meanwhile, the data block transmits crucial navigation messages from the LEO satellite that assist in aligning the receiver's clock with the onboard transmitter clock.

Figure 2

The proposed OFDM-based LEO navigation signal structure

Each navigation frame is composed of four slots, with each slot containing 14 symbols. The first slot, designated as the SSB, transmits repeated m-sequences during the initial 10 symbols. The subsequent three slots serve as data blocks. Within these blocks, the remaining symbols are dedicated to transmitting essential navigation messages, which play a critical role in enabling timing synchronization and computing the TOA κ. To facilitate channel estimation and Doppler tracking, pilots are inserted every five subcarriers, thereby improving the synchronization accuracy. A specific time interval is also introduced between each slot, resulting in a total frame duration of Tframe=1 ms, enabling precise alignment with the pulse-per-second signal generated by onboard GNSS receivers. Detailed parameters are listed in Table 1.

View this table:
Table 1 Specifications of the Proposed OFDM Navigation Signal

3.2 Navigation Properties of OFDM Modulation

In this paper, we adopt the OFDM modulation scheme as our ranging signal, rather than traditional GNSS-like navigation signals (Wang et al., 2018), owing to its superior performance, particularly in high-ranging-accuracy and anti-interference capabilities against multipath and in-band signal disturbances. These attributes significantly enhance the reliability and precision of navigation systems, which are critical for dynamic environments such as those encountered by LEO satellites. This section presents a detailed theoretical analysis and performance comparison of six modulation schemes: BOC(1,1), BPSK(1), BPSK(10), BOC(10,5), and two OFDM configurations with subcarrier spacings (SCSs) of 60 kHz and 120 kHz (denoted as OFDM(60) and OFDM(120), respectively). Both OFDM configurations use M = 276 subcarriers, corresponding to nominal bandwidths of 16.5 MHz and 33 MHz, respectively. Through systematic evaluation, we demonstrate the viability of the OFDM scheme as a robust and precise ranging solution for our application.

Ranging Accuracy

To evaluate the ranging accuracy potential, the auto-correlation function (ACF) is first adopted. The sharpness of the ACF peak serves as a key indicator for achievable ranging resolution, where narrower ACF peaks correspond to higher precision in time-delay (κ) estimation (Liu et al., 2014). As shown in Figure 3(a), OFDM signals exhibit evident sensitivity to the SCS configuration. Increasing the SCS from 60 kHz to 120 kHz reduces the ACF peak width significantly. This substantial narrowing demonstrates the potential for enhanced ranging accuracy through SCS optimization. Notably, the OFDM(120) configuration achieves ACF sharpness comparable to that of BOC(10,5), a signal modulation widely recognized for high-precision satellite navigation applications.

Figure 3

Performance of ranging accuracy for different modulation schemes (a) ACFs of different modulation schemes, (b) Gabor bandwidth as a function of front-end bandwidth.

In addition to ACF analysis, we employ the Gabor bandwidth to further quantify the signal characteristics related to ranging accuracy. The Gabor bandwidth quantifies the frequency spread of a signal’s energy (Amoroso, 1980), which is expressed as follows:

ΔfGabor=Br/2Br/2f2G(f)df 5

where G(f) is the normalized power spectral density (PSD) of the signal and Br denotes the front-end bandwidth of the receiver.

A higher Gabor bandwidth corresponds to a broader frequency spread, which enhances code-tracking precision and reduces uncertainty in the TOA estimation of κ. As illustrated in Figure 3(b), the Gabor bandwidth of OFDM signals is directly influenced by their SCS when the number of subcarriers is fixed. Specifically, the Gabor bandwidth for OFDM(60) exceeds that of all other modulation schemes except BOC(10,5) and OFDM(120). The Gabor bandwidth for OFDM(120) surpasses that of BOC(10,5) when the front-end bandwidth exceeds 33 MHz. This finding demonstrates that OFDM signals with a larger SCS and consequently a wider signal bandwidth achieve a higher Gabor bandwidth, which translates to superior code-tracking performance. With a sufficient SCS, OFDM modulations can surpass all other modulation schemes evaluated in this study.

Power Efficiency and Bandwidth Requirement

The PSD and power containment percentages are plotted in Figures 4(a) and 4(b), respectively, to evaluate the power efficiency and determine the bandwidth requirements for different modulations. Figure 4(a) shows that the OFDM signal has a flat main lobe, which includes the majority of its energy, whereas the PSD of the other modulations exhibits pronounced peaks and valleys. This flat main lobe indicates that OFDM is a power-efficient modulation scheme, as it concentrates its energy uniformly across the frequency range. However, as the main lobe of the OFDM signal becomes wider, the signal strength per unit frequency decreases, necessitating a more sensitive receiver to process the wideband OFDM signal.

Figure 4

Power efficiency and bandwidth requirement for different modulation schemes (a) PSD of the listed modulations, (b) Power containment of the listed modulations.

To complement the analysis of power efficiency, Figure 4(b) provides insights into the specific receiver bandwidth requirements for different modulations. Typically, the front-end bandwidth Br of the receiver should be equal to at least the 90% power bandwidth β90% to ensure efficient reception (Betz, 2001). According to Figure 4(b), the β90% of the OFDM signal is broader than that of the BPSK(1) and BOC(1,1) signals and relatively similar to that of BPSK(10) and BOC(10,5), depending on the specific values of SCS and subcarrier number M. Thereby, while OFDM is power-efficient, a wider bandwidth is required for reception compared with narrower modulations to fully utilize the potential of OFDM. Collectively, these results demonstrate that OFDM not only optimizes the energy distribution but also requires careful receiver design to handle its wider frequency characteristics.

Anti-Interference Capacity

Anti-interference capacity is a critical factor for potential navigation signals. The multipath error envelope (MEE), particularly within the context of a two-ray signal model, serves as a critical criteria for assessing the impact of multipath on tracking performance and ranging accuracy. The MEE is given as follows (Liu et al., 2014):

ϵ±aBr/2Br/2G(f)sin(2πft)sin(πfd)df2πBr/2Br/2fG(f)sin(πfd)[1±acos(2πft)]df 6

where a is the multipath-to-direct signal amplitude ratio and the receiver correlator spacing is denoted by d. The symbols “+” and “–” represent the phase relationship between the multipath signal and the direct line-of-sight signal. “+” indicates that the signals are in phase (0°), causing constructive interference, whereas “–” indicates that they are 180° out of phase, causing destructive interference.

We compute the MEE for a front-end bandwidth of 35 MHz. As shown in Figure 5(a), the OFDM(120) signal exhibits minimal multipath errors compared with other modulation schemes when a = 0 1. and d = 0 05. This result highlights the potential of OFDM modulation for maintaining precise tracking when facing multipath interference.

Figure 5

Performance of anti-interference properties for different modulation schemes (a) MEE with a prefiltering bandwidth of 35 MHz, (b) SSC values for different modulation schemes.

The spectral separation coefficient (SSC) is employed to assess the interference level when a navigation signal candidate, sharing the same frequency band with other signals, is received. The SSC is defined as follows (Liu et al., 2014):

kid=Gi(f)Gd(f)df 7

where Gi(f) and Gd(f) are the normalized PSD of the signals considered as the interference and desired signals, respectively. When both the interference and desired signals employ the same modulation scheme, Gi(f) and Gd(f) are identical. In such cases, kid serves as a measure of self-interference SSC. Otherwise, kid measures the cross-interference SSC.

Figure 5(b) shows the SSC values for cross-interference between example signals, displayed off the diagonals, with self-interference values indicated along the diagonals of the plot. For cross-interference SSC, it is evident that both the OFDM and BOC(10,5) signals exhibit relatively low SSC values among the various modulation schemes, indicating a lower likelihood of interference. For self-interference SSC, OFDM signals demonstrate superior resistance to intersystem interference, whereas BOC(10,5) signals are comparatively more vulnerable in cases of matched spectrum interference. Considering the significant advantages of OFDM in maintaining higher accuracy in timing output and offering superior interference resistance, we have selected OFDM as our preferred modulation scheme for LEO navigation signals.

3.3 Synchronization Sequence

In this section, we evaluate two prominent SSs, the ZC sequence and the m-sequence, for their suitability in LEO navigation. The primary goal is to precisely estimate the transmission delay κ using a maximum likelihood (ML)-based detection method for accurate ranging. Known as the TOA, these delays κ are critical for navigation accuracy but are significantly impacted by both integer and fractional CFOs in LEO satellite environments, as discussed above. Thus, our choice of SS primarily depends on the ability of each sequence to ensure accurate κ estimations under integer and fractional CFOs.

Integer CFO

The m-sequence exhibits a defining characteristic under integer CFOs: when the frequency shift exceeds one SCS, i.e., when an integer CFO occurs, the correlation peak disappears, leaving only noise, as shown in Figure 6(b). This phenomenon can be mathematically represented as follows (Kaplan & Hegarty, 2017):

Figure 6

Correlation peak detection results for the ZC sequence and m-sequence (a) Correlation peak of the ZC sequence, (b) Correlation peak of the m-sequence. For both panels, the colorbar denotes the normalized correlation peak amplitude.

|RI,m(ΔfI,Δκ)|=1N|n=0N1c1(n+κ)c2(n+κ)|={|sinc(ΔfI)|,ifκ=κ1N,ifκκ 8

where ΔfI=fISCS1 is the normalized integer CFO, κ′ is the estimated TOA, Δκ=κκ is the timing shift, fI denotes the true integer CFO, and c2(n)=c1(n)ej2πfInN, with c1(n) being an m-sequence of length N, generated by a maximal length linear feedback shift register.

The susceptibility of the m-sequence to integer CFOs is clearly demonstrated; there is no correlation peak when such CFO conditions exist in systems based on m-sequence SSs. Interestingly, this vulnerability to integer CFOs proves advantageous for our ranging applications. This advantage arises because, after performing a two-dimensional search within specific frequency ranges and successfully detecting an m-sequence, we ensure that the integer CFO is accurately compensated using the ML estimate of the TOA (Hua et al., 2014):

κ=argmax|RI,m(ΔfI,Δκ)|2 9

Furthermore, residual fractional CFOs do not significantly impact the TOA κ′ estimation of the m-sequence, as will be elaborated upon in the following section. Therefore, if the m-sequence is successfully detected, the estimated κ′ should align precisely with the actual delay, remaining unaffected by any CFOs.

In contrast, the ZC sequence behaves differently under conditions of integer CFOs. As illustrated in Figure 6(a), the correlation peaks of the ZC sequence persist even in the presence of an integer CFO between the ZC sequence and its local replicas. When subject to an integer CFO, the correlation result of the ZC sequence, omitting noise, is mathematically represented as follows (Gul et al., 2012):

|RI,zc(ΔfI,Δκ))|=α|n=0N1ej2π(μ(κNgκ)+fI)nN|,κκκ+Ng 10

where μ is the root of the ZC sequence, which is received with a delay of κ samples. Ng and N represent the lengths of the CP and SS, respectively.

It can be inferred from Equation (10) that the time delay κ of the ZC sequence is estimated as follows:

κ=argmax|RI,zc(ΔfI,Δκ)|2={κ|μ(κNgκ)+fI=pN} 11

where p is any integer. From Equation (11), it is evident that when an integer CFO fI exists, a peak can still be observed if μ(κNgκ)+fI=pN. This phenomena is referred to as frequency offset ambiguity (Chandramouli et al., 2019). Consequently, during the step of ZC sequence detection, the receiver cannot confirm whether it is affected by an integer CFO, which may increase the BER in data recovery. More critically, an integer CFO can induce a timing shift in the TOA estimation of κ, leading to frequency offset ambiguity. This introduces uncertainty in SS detection, making it difficult to determine whether the estimated TOA κ is influenced by a potential integer CFO.

Similar to ZC sequences, chirp signals are also influenced by frequency offset ambiguity, commonly referred to as range–Doppler coupling in radar signal processing. This effect causes a mismatch during matched filtering, ultimately degrading range estimation (Richards et al., 2010). To suppress this coupling and increase ranging accuracy, two closely spaced up-chirp and down-chirp pulses can be utilized to estimate and compensate for the observed Doppler shift. A similar approach can be applied to ZC sequences to address frequency offset ambiguity. However, this method significantly increases the correlation computational load, increasing the processing complexity of the receiver.

In contrast to both ZC sequences and chirp signals, the m-sequence offers a distinct advantage in terms of integer CFO compensation. Recall that the m-sequence generates a unique and unambiguous peak in the correlation matrix, as shown in Figure 6(b). This property highlights the m-sequence’s ability to support integer CFO compensation through straightforward searching across two-dimensional Doppler-phase ranges, validating its superior suitability for LEO ranging missions.

When the received data are affected by fractional CFOs, the subcarriers lose orthogonality, leading to inter-carrier interference and an increased ranging error. To understand the mathematical factors influencing the timing properties of the two candidate SSs under a fractional CFO, we define the correlation function |RF,(Δλ,Δκ)| for each candidate in the presence of fractional CFOs, following the approach given by Hua et al. (2014):

|RF,(Δλ,Δκ)|={|sinc(ΔλΔλΔκ)|,ifRF,=RF,zc|sinc(Δλ)Rm(Δκ)|,ifRF,=RF,m 12

where:

ΔλΔκμΔκ+lN,l=argminlZ|μΔκ+lN|13

and RF,∗ denotes the fractional correlation value for different SS candidates under fractional CFOs. Δλ=fFSCS<1denotes the normalized fractional CFO, and fF is the true fractional CFO value. The function |Rm(Δκ)| is defined as follows:

|Rm(Δκ)|={1ifΔκ=01NifΔκ0

As shown in Equations (12) and (13), unlike RF,m, the value of RF,zc depends on both the length N and root μ of the ZC sequence. In Equation (12),ΔλΔκ indicates the critical frequency offset for RF,zc at a specific incorrect shift offset of Δκ0. At this incorrect shift offset Δκ, with a fixed μ, the critical timing offset can have a small absolute value, which leads to a large value of RF,zc at a nonzero location Δκ0. This situation results in an undesirable increase from correct estimations when Δκ=0 in the correlation function, increasing the likelihood of incorrect timing estimation.

To evaluate the TOA estimation performance for both SS candidates under fractional CFOs, two key metrics have been introduced by Hua et al. (2014), i.e., the timing detection probability PΔκ(Δκ) and the timing error probability Pe. The timing detection probability PΔκ(Δκ) is expressed as follows:

PΔκ*(Δκ)=1WκHP(Δκ*=Δκκ)14

where κ* denotes the superior timing offset estimation and κ represents the actual timing offset, with Δκκκ defining their difference. The variable W refers to the length of the timing hypothesis window H. As demonstrated in Equation (14), PΔκ(Δκ) indicates the probability of different Δκ values corresponding to the superior detection. The timing error probability is given as follows:

Pe=1PΔκ(Δκ=0)15

where PΔκ(Δκ=0) quantifies the likelihood of the ML algorithm correctly outputting the actual TOA κ′ when κ′=κ between the transmitter and the receiver.

The value of P(Δκ=ΔκκH) is derived to be positively correlated with |RF,(Δλ,Δκ)| (Hua et al., 2014). As a result, when the ZC sequence is used as the SS,PΔκ(Δκ) can also become unexpectedly large, as RF,zc exhibits a large value at Δκ0. Consequently, PΔκ(Δκ=0) becomes relatively small, leading to a high Pe value across various SNRs. Figures 7 and 8 illustrate PΔκ(Δκ) and Pe for the m-sequence and ZC sequence, respectively, for a varying ZC root μ, under a time uncertainty window of |H| = 16, with N = 839 and a fractional CFO of Δλ = 0.55.

Figure 7

Probability of detection and timing error for the m-sequence and ZC sequence, with µ = 140 for the ZC sequence (a) Probability of detection for the m-sequence and ZC sequence for a fractional CFO of Δλ = 0.55, (b) Probability of timing error for the m-sequence and ZC sequence across various SNR levels.

Figure 8

Probability of detection and timing error for the m-sequence and ZC sequence, with µ = 367 for the ZC sequence (a) Probability of detection for the m-sequence and ZC sequence for a fractional CFO of Δλ = 0.55, (b) Probability of timing error for the m-sequence and ZC sequence across various SNR levels.

Figure 7 shows the case in which the chosen value of μ degrades the TOA estimation performance, specifically when μ =140. In Figure 7(a), ΔλΔκ=±1 and ±2 for timing offsets of Δκ=±6 and ±12, respectively. The small value of ΔλΔκ=±1 leads to relatively large values of |Rzc(Δλ,Δκ)|, resulting in multiple spurious peaks at κ±6 and ±12, in addition to κ=0. This result suggests a higher likelihood of erroneous detection at these offsets, which could mislead the receiver’s estimations of TOA κ′. In contrast, the m-sequence exhibits a single prominent peak only at κ=0 indicating more accurate κ′ estimations. Figure 7(b) supports these observations by showing that the m-sequence exhibits a sharp decrease in Pe as the SNR increases; conversely, the ZC sequence shows a more gradual decline, hindered by the four unexpected spurious peaks. These distinct patterns in Pe between the m-sequence and the ZC sequence persist across various fractional CFOs, λ0.

Figure 8 explores improvements in κ′ estimation performance for the ZC sequence, obtained by strategically selecting the root value as μ=367. In this case, the smallest ΔλΔκ=±521 When Δκ±7, which allows little effect on |RZCλ,κ|. The results in Figures 8(a) and 8(b) indicate that both the detection probability Pκ*κ and the error probability Pe of the ZC sequence now mirror those of the m-sequence, showcasing high detection accuracy and rapid declines in Pe, indicating a minimal degradation in timing performance.

These findings emphasize that while the ZC sequence can outperform the m-sequence in ranging capabilities under ideal conditions with no CFOs in random roots and may slightly surpass the m-sequence with fractional CFOs if the root is carefully selected, it has significant limitations. In contrast, the m-sequence offers a much more reliable performance owing to its regular structure, which ensures precise κ′ estimations without the need for selecting specific internal parameters, even in the presence of fractional CFOs. Moreover, the inherent property of the m-sequence allows it to compensate for the integer CFO through straightforward two-dimensional searching. In contrast, the ZC sequence struggles with frequency offset ambiguity, where integer CFOs induce timing shifts that impair κ′ estimation accuracy. Considering these strengths, the m-sequence emerges as the superior choice for our LEO ranging tasks, providing robustness and simplicity without the complications associated with parameter tuning or ambiguity from CFOs.

4 RECEIVER

Aside from signal design and transmission, the receiver plays a critical role in guaranteeing time synchronization and producing accurate TOA κ′ estimations under LEO navigation scenarios. This section introduces a novel DCA-NOLRT-based SS detection architecture to enhance receiver reliability and sensitivity and to reduce ranging errors when processing signals from an onboard transmitter.

As shown in Figures 7(b) and 8(b), even though no unexpected side peaks appear at Δk≠0 when m-sequences are used as the SS in the presence of fractional CFOs, the probability of timing error, Pe, still increases with CFO Δλ. The proposed receiver shows improved resistance to fractional CFOs, thereby enhancing its reliability in harsh LEO navigation scenarios without the need for additional CFO mitigation algorithms. Simultaneously, the sensitivity of the LEO receiver is increased, broadening its applicability in challenging environments with weak LEO signal reception.

4.1 Anti-Fractional CFO

The DCA algorithm (Qiu et al., 2012) is first adopted in the receiver to enhance the acquisition performance by improving the relative peak detection during acquisition. After the carrier wipe-off, the complex received signal r(t) is converted into a baseband signal. In line with classic cross-correlation-based OFDM synchronization methods, the m-th correlation output U(m) of r(t) is given by the following:

U(m)=1Nn=1Nr((m1)N+n)c(n)=|RF,m(Δλ,Δκ)|16

where c(n) is the local replica of the m-sequence. The SSB structure introduced in Section 3.1 assumes that the received OFDM signal contains L = 10 identical m-sequences. Therefore, the result of U(m+ 1) involves the integration of N subsequent samples of r(t) with the conjugate of the identical m-sequence c(n). This process is repeated L − 1 times to process all SSs in the received OFDM signal.

In the next step, the coherent integration outputs are multiplied by the conjugate of the subsequent output, which is given as follows:

Ddiff=|m=1L1U(m+1)U(m)|217

The multiplied result Ddiff is accumulated over a long period of time (L–1)*T0, where T0=1scs denotes the symbol time of the LEO signal. The output Ddiff of the DCA algorithm has a length of N. It is obvious that the DCA algorithm enhances the correlation gain of the LEO receiver, significantly improving its sensitivity to the SSB. A flowchart of the DCA algorithm is shown in Figure 9.

Figure 9

Diagram of the DCA algorithm

The LEO receiver’s anti-fractional CFO capability is also improved by utilizing the DCA algorithm. The error detection probability of U(m), m=1,..., –1 is the same as Pe expressed in Equation (15) because the continuous pieces of r(t) share the same CFO and timing offset. Thus, the timing error probability PePDCA of Ddiff after the DCA process can be given as follows:

PeDCA=|Pe|218

Based on Equation (18), because Pe<1,PeDCA, remains consistently lower than Pe, demonstrating a sharper decrease as the SNR increases. This trend indicates enhanced resistance to fractional CFOs following the adoption of the DCA algorithm.

A problem that arises in adopting the DCA algorithm in the LEO receiver is that this algorithm can potentially lead to periodic ranging errors. Owing to the accumulation process in the DCA algorithm, the initial length N * L of the received signal r(t) is now compressed into an N-length vector Ddiff. Consequently, integer ambiguity arises because the actual TOA of the OFDM signal cannot be determined owing to the compression of L repeated SSs into a single accumulation result, Ddiff. Even if the correlation peak of the SS is detected after the DCA process, it is still unclear which one of the L SSs is the first one to be detected. As a result, additional TOA estimation bias aside from noise distortion is introduced, leading to an intolerable ranging error.

To address the periodic ranging errors due to potential misidentifications of the first reference symbol, we employ a NOLRT detector (Yin et al., 2020) for spectrum sensing to handle the ambiguity problem stemming from the DCA algorithm. This detector proves to be highly effective in reliably detecting weak OFDM signals with periodic pilots in cognitive radio networks. As depicted in Figure 10, when the locally generated pilot signal p(t) is perfectly synchronized with the pilot signal of the received OFDM signal r(t), the NOLRT detector unequivocally declares H1 as the decision. This decision is made based on the correlation value between r(t) and the complex conjugate of p(t) being greater than a predefined threshold, denoted as λNOLRT, given as follows (Yin et al., 2020):

Figure 10

Framework of the proposed NOLRT detector

TNOLRT=n=1N+NCP1Re{r(n)p(n)}H0H1λNOLRT19

where 𝒯NOLRT represents the test statistic of the NOLRT detector, λNOLRT is the corresponding decision threshold proposed by Yin et al. (2020), and NCP is the length of the CP.

As demonstrated in Equation (19), an incorrect selection of the first-arriving SS results in a misalignment between p(t) and r(t), causing the test statistic 𝒯NOLRT to fall below the λNOLRT threshold. By comparing 𝒯NOLRT for all L SS candidates, we can accurately identify the symbol that was received first. This approach helps to mitigate the additional ranging error caused by the DCA-induced integer ambiguity. Consequently, by integrating the DCA-NOLRT structure, SS detection becomes more feasible in low-SNR environments and more resilient to CFOs. Additionally, the threshold λNOLRT helps identify the specific first-arrived SS among all L candidates, ensuring precise ranging estimations.

5 EXPERIMENTS

In this section, we evaluate the ranging performance of the proposed LEO navigation framework through coordinated simulations and terrestrial experiments. All evaluations strictly follow the signal structure defined in Section 3.1 and detailed in Table 1, including truncation of the synchronization of the m-sequence from 511 to 276 samples to align with the M = 276 subcarrier specification. To assess the performance, we focused on two primary objectives: (1) analyzing the reduction in false detection rate of the proposed receiver when addressing fractional CFOs, as well as the enhanced sensitivity for SS detection under low-SNR conditions; (2) comparing the ranging performance of the ZC sequences and m-sequences under the DCA-NOLRT-based receiver architecture. Collectively, these evaluations validate the framework’s robustness in challenging operational environments.

5.1 Capabilities of the LEO Receiver

This section evaluates the resilience to fractional CFOs and the sensitivity of the proposed DCA-NOLRT-based receiver architecture. First, we assess how effectively the proposed receiver reduces the detection error rate of the m-sequence under different fractional CFO values Δλ and across various SNR levels. As shown in Figure 11, the timing error probability peDCA of the proposed LEO receiver decreases more rapidly than the traditional receiver’s timing error probability Pe as the SNR increases, demonstrating that the DCA-NOLRT architecture significantly enhances robustness against fractional CFOs. According to the analysis in Section 3.3, once the two-dimensional search detects the correlation peak of the m-sequence, the m-sequence guarantees a zero-residual integer CFO. To manage any remaining fractional CFOs, the DCA-NOLRT architecture improves signal detection robustness. Additionally, the SS design of the proposed LEO navigation signal leverages the m-sequence, which inherently offers stronger resilience to fractional CFOs compared with ZC sequences. Thus, the combined design of the DCA-NOLRT receiver and the LEO navigation signal ensures robust ranging performance in dynamic LEO scenarios with large CFOs.

Figure 11

Comparison of the detection error rate of Pe and PeDCA as a function of the SNR of the received signals

In our second experiment, we validate the enhanced sensitivity of the proposed DCA-NOLRT SS detection architecture by comparing it with the traditional non-coherent integration (NCI) method (Qiu et al., 2012). The results are presented in Figure 12. Coherent integration, commonly employed for OFDM time synchronization, is not suitable for our application because it requires increasing the number of subcarriers and bandwidth, which poses practical limitations. Figure 12 illustrates the correlation results: the DCA algorithm, represented by red lines, consistently outperforms the NCI method across various transmitted power levels in both the L = 10 and L = 20 scenarios. The blue dashed lines demonstrate that the NCI method exacerbates noise issues owing to a squared term, significantly reducing the sensitivity under weak signal conditions (Esteves et al., 2016; Manzano-Jurado et al., 2014). The results shown in Figure 12 underscore the superior effectiveness of the proposed DCA-NOLRT receiver architecture in LEO navigation tasks, particularly when the receiver must handle weak LEO signals with high precision.

Figure 12

ACFs for various L values and SNRs, demonstrating receiver sensitivity under the NCI and DCA methods (a) SNR = −10 dB, L = 10, (b) SNR = −15 dB, L = 10, (c) SNR = −10 dB, L = 15, (d) SNR = −15 dB, L = 15

5.2 Ranging Performance Validation

Numerical Simulations

The simulations in this section directly compare the ranging performance of ZC sequences and m-sequences under challenging LEO navigation conditions characterized by large dynamic CFO variations and low SNRs, using the proposed DCA-NOLRT-based receiver for a fair assessment. Each simulation condition was executed 20 times to ensure statistical reliability. Evaluations employ a modified non-terrestrial network tapped delay line-B (NTN-TDL-B) channel model (3GPP, 2018).While the standard NTN-TDL-B model fixes the satellite elevation at 50°,we extend the elevation angle range from 0° to 90° to simulate dynamic CFO behavior induced by elevation angle changes of the satellite. Within this modified NTN-TDL-B simulated environment, signals experience impairments commonly encountered in LEO navigation, such as delay spread causing temporal dispersion and CFOs from satellite motion. Detailed parameters are provided in Table 2.

View this table:
Table 2 Modified NTN-TDL Channel Simulation Parameters

The results in Figures 13(a) and 13(b) illustrate the ZC sequence performance across the full CFO shift range derived from satellite dynamics in Table 2. Figure 13(a) demonstrates that without mitigation, CFOs exceeding the SCS induce frequency ambiguity. Although signal detection is successful, such ambiguity introduces the timing shift analyzed in Section 3.1, resulting in step-like ranging errors. Furthermore, applying a CFO mitigation method (Van de Beek et al., 1997) proves largely ineffective or even counterproductive under these low-SNR impaired conditions, as shown in Figure 13(b). This adverse effect is due to inaccurate CFO estimation and compensation during the mitigation procedure, which introduces larger CFO errors than those without mitigation. As a result, even when the actual CFO falls below half the SCS (within the applicable range of the CFO mitigation method), CFO estimations exhibit destabilizing fluctuations that increase the ranging error magnitude. These findings highlight the challenges of traditional CFO estimation and mitigation strategies under harsh conditions of LEO navigation, especially when th SNR is low and channel impairments are considered.

Figure 13

Ranging errors of the ZC sequence under NTN-TDL-B channel conditions for various SCS values The ZC sequences are truncated from 511 to 276 chips with root µ=20. (a) Results obtained without the CFO compensation method, (b) Results obtained with the CFO compensation method.

In contrast to the ineffective CFO mitigation strategies illustrated in Figure 13, Figure 14 presents ranging outcomes for the m-sequence obtained through a two-dimensional frequency-code phase search. Because m-sequences suffer no frequency ambiguity, no timing shift is induced when the correlation peak is detected. Consequently, across the full CFO shift range indicated on the x-axis, step-like ranging errors are effectively mitigated, and a satisfactory ranging accuracy is guaranteed. These results demonstrate the inherent resilience of the m-sequence against CFO effects, allowing accurate ranging estimation despite challenging conditions under LEO navigation scenarios.

Figure 14

Ranging errors of the m-sequence under NTN-TDL-B channel conditions for various SCS values

In Figure 14, the remaining fluctuations in ranging errors are primarily attributed to delay spread within the modified NTN-TDL-B model. Additionally, similar small fluctuations in ranging errors are observed in Figure 13(a) when the CFO is below the SCS, which are also caused by the simulated multipath delay spread. This consistent behavior under the modified NTN-TDL-B conditions indicates that the observed errors are primarily caused by multipath effects inherent in the channel model. Such multipath-induced errors can be effectively suppressed by employing a larger SCS. An increased SCS enhances the time resolution and signal bandwidth (Abrudan et al., 2013), thereby improving the ability to discriminate between line-of-sight and multipath signals. As a result, error fluctuations caused by multipath interference are significantly reduced.

Furthermore, for ZC sequences, larger SCS values significantly reduce frequency ambiguity-induced ranging errors over wider CFO ranges, as shown in Figure 13. This advantage explains the preference for wider SCSs in LEO navigation systems. However, when the available bandwidth is limited, increasing the SCS reduces the number of available subcarriers, thereby impairing data transmission efficiency. This inherent trade-off between transmission efficiency and CFO resistance represents a common challenge for LEO systems. To balance these competing factors, an SCS of 60 kHz is selected for our designed LEO signal configuration.

Terrestrial Ranging Experiments

In this section, we validate the ranging accuracy of the proposed LEO navigation framework through a terrestrial experiment. The experimental setup, illustrated in Figure 15, consists of a custom-designed navigation transmitter (Tx) and a receiver (Rx) based on an Ettus Universal Software Radio Peripheral (USRP) X310. The receiver is controlled by the USRP hardware driver software on a host PC, which stores received signal samples for offline postprocessing. The positions of the transmitter and receiver are accurately surveyed using a u-blox EVK-F9P receiver. The transmitter is located at 31.0269865°N, 121.4400866°E, with an elevation of 18 m, and the receiver is located at 31.0273907°N, 121.4404318°E, with an elevation of 23 m. The ground-truth distance calculated between the transmitter and receiver is 61.30 m.

Figure 15

Experimental hardware used in ground tests

To emulate challenging LEO signal conditions, a 1-W navigation signal is attenuated by 60 dB before transmission to simulate path loss. Furthermore, an 80-kHz CFO is manually introduced offline, with a changing rate of 100 Hz/s, to mimic the dynamic Doppler shifts typical in LEO navigation scenarios. These configurations replicate low-SNR and time-varying CFO conditions within a controlled ground environment.

We calculate the range between the transmitter and receiver every 6 s of each epoch. As shown in Figure 16, the ranging errors across different estimation epochs are presented, with a root mean square error of 3.34 m, validating the effectiveness of the proposed LEO navigation framework under harsh conditions. It is important to clarify that in the ground experiments, we were unable to fully replicate the delay spread and other channel impairments characteristic of the NTN-TDL-B channel. This limitation is the primary reason why the ranging errors observed in the ground experiments are generally smaller than those in Figure 14.

Figure 16

Ranging performance of the proposed LEO navigation framework in ground experiments

By combining the ranging performance results from both numerical simulations and ground tests, the reliability of our proposed LEO navigation signal and receiver framework is demonstrated. The system achieves satisfactory ranging accuracy in simulations and even better performance in controlled ground experiments, highlighting its robustness under challenging conditions of LEO navigation.

6 CONCLUSION

This paper investigated the challenges of ranging estimation in OFDM-based LEO navigation systems in harsh environments. We introduced a system-level LEO navigation approach designed to operate under conditions of low SNRs and large CFOs. The suitability of SS candidates for maintaining ranging accuracy was evaluated, revealing that the m-sequence consistently ensures reliable ranging accuracy whereas the ZC sequence is prone to step-like ranging errors. Furthermore, a DCA-NOLRT SS detection structure was developed for the receiver, significantly enhancing the sensitivity of SS detection and resilience to CFOs in challenging conditions. Numerical simulations and experimental results validated the robust performance of the proposed LEO navigation framework design in maintaining accurate ranging estimations under circumstances of low SNRs, significant CFOs, and other channel impairments. A limitation of this study is that the analysis and experiments were confined to the S-band. Because the CFO increases with the signal’s center frequency, higher-frequency bands are expected to experience larger CFOs and a higher risk of integer ambiguities. As part of future work, the proposed framework will be extended and validated for X-band systems to assess its robustness under more extreme frequency conditions.

HOW TO CITE THIS ARTICLE:

He, Y., & Xu, B. (2026). Enhancing ranging precision in OFDM-based LEO navigation: Signal design and receiver implementation. NAVIGATION, 73. https://doi.org/10.33012/navi.741

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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