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Remote SensingRemote Sensing
  • Review
  • Open Access

6 July 2026

28 Pages

3D Gaussian Splatting for Large-Scale Remote Sensing: A PRISMA-Informed Scoping Review of Scalability, Geometric Reliability, and Benchmarking Across UAV/Aerial and Satellite Imagery

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1
College of Future Information Technology, Fudan University, Shanghai 200433, China
2
Shanghai-Africa International Joint Laboratory for Optoelectronic Remote Sensing and Early Warning in Disaster Mitigation, Shanghai 201900, China
3
Institute of Optoelectronics, Fudan University, Shanghai 200433, China
4
Shanghai Etherspace Technology Co., Ltd., Shanghai 200129, China
This article belongs to the Section AI Remote Sensing

Highlights

What are the main findings?
  • A faceted four-axis taxonomy organizes remote-sensing 3DGS by platform, sensor model, scalability strategy, and geometric supervision.
  • Existing scaling strategies improve efficiency, but metric reliability still depends on sensor modeling, geometric constraints, and product-level evaluation.
What are the implications of the main findings?
  • UAV/aerial and satellite 3DGS should be evaluated with platform-aware, supervision-explicit, and multi-metric protocols rather than a single undifferentiated ranking.
  • The proposed benchmark framework links visual fidelity, computational cost, metric geometry, product utility, and failure behavior for more reproducible remote-sensing evaluation.

Abstract

3D Gaussian Splatting (3DGS) offers efficient explicit rendering, but large-scale remote-sensing use remains fragmented across UAV/aerial photogrammetry, satellite reconstruction, large-scene scaling, surface modeling, and geospatial evaluation. We present a Preferred Reporting Items for Systematic Reviews and Meta-Analyses (PRISMA)-informed scoping review based on 55 core studies identified through Web of Science, Scopus, IEEE Xplore, and supplementary searches completed on 3 June 2026. A faceted taxonomy organizes the literature by platform, sensor model, scalability strategy, and geometric supervision. The synthesis shows that partitioning, hierarchy, compression, and feed-forward inference improve scalability but do not guarantee metric geometry. Reliable deployment additionally requires sensor-consistent projection, geometric or georeferencing constraints, explicit supervision labels, and product-level evaluation. In control-point-free settings, internal consistency should be distinguished from independently validated accuracy. We therefore propose a platform-aware benchmark framework that jointly records visual fidelity, computational cost, metric geometry, product utility, failure behavior, and reproducibility metadata for UAV/aerial, satellite, and hybrid settings.

1. Introduction

Large-scale remote sensing increasingly requires reusable 3D representations for visualization, measurement, orthophoto production, surface modeling, and geospatial analysis. Plausible novel view synthesis (NVS) alone is insufficient: useful models must preserve geometry, tolerate appearance change, and support products such as digital surface models (DSMs), heights, and georeferenced measurements [1,2,3,4,5,6].
Neural Radiance Fields (NeRFs) established differentiable scene reconstruction, while S-NeRF, Sat-NeRF, and EO-NeRF exposed the importance of shadows, transient objects, rational polynomial coefficient (RPC) cameras, and geometric constraints in satellite imagery [7,8,9,10]. 3DGS replaces repeated ray sampling with explicit anisotropic Gaussians and rasterization, but its vanilla form does not address push-broom/RPC sensors, georeferencing, large-area scaling, or mapping-grade geometry [1]. Subsequent work has combined partitioning, level-of-detail (LoD) rendering, compression, and generalizable prediction with LiDAR guidance, camera refinement, temporal or semantic modeling, surface constraints, and product-oriented evaluation [11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27].
This PRISMA-informed scoping review contributes a 55-study corpus, a faceted taxonomy separating observation conditions from methodological responses, a supervision-aware synthesis of scalability and geometry, and a benchmark reporting framework covering tracks, costs, metrics, failures, and machine-readable metadata. It does not claim the underlying LiDAR, RPC, surface, or georeferencing techniques as new; it organizes them for more defensible comparison across UAV/aerial and satellite settings.

2. Review Design, PRISMA Methodology, and Analytical Framework

This article is a PRISMA-informed scoping review rather than a quantitative meta-analysis. PRISMA 2020 is used to report identification, screening, eligibility, inclusion, and protocol status transparently [28]. Supplementary File S1 contains the checklist and Figure 1 summarizes selection.
Figure 1. PRISMA 2020 flow diagram for the identification, screening, eligibility assessment, and inclusion of studies in the 55-study core corpus.

2.1. Review Questions

The review asks: (1) how 3DGS is adapted to UAV/aerial and satellite sensing; (2) which scalability, sensor-model, and geometric constraints govern reliable large-scale use; and (3) which benchmark and reproducibility gaps prevent fair comparison.

2.2. Review Scope

We include explicit Gaussian scene representations and closely related radiance-field antecedents relevant to optical UAV/aerial and satellite image-based reconstruction. Hybrid aerial–ground work is retained when it informs scale, sensor modeling, fusion, or geospatial products. The scope excludes SAR, hyperspectral, thermal, LiDAR-only, underwater, and non-image reconstruction except as methodological context. General 3DGS and sparse-view surveys already cover the broader field [29,30,31]; this review focuses on the tension between rendering efficiency and sensor-consistent, product-level geometry.

2.3. Information Sources and Search Strategy

Web of Science, Scopus, and IEEE Xplore were searched and reconciled with prior Google Scholar screening, manuscript seed references, arXiv/publisher checks, and backward/forward citation chasing. The final search and corpus-reconciliation date was 3 June 2026. Search families combined 3DGS terms with remote sensing, UAV/aerial, satellite, scalability, geometry, and benchmark terms; Supplementary Table S2 records source-specific queries, dates, filters, and counts. Figure 2 links search, screening, coding, and synthesis.
Figure 2. Overview of the PRISMA-informed review design and analytical workflow. The schematic complements the PRISMA flow diagram by showing how record screening, paper-level coding, and the four analytical axes lead to the taxonomy and benchmark framework.

2.4. Eligibility Criteria

Core studies had to present a 3DGS method, substantive adaptation, or directly relevant radiance-field antecedent for large-scene or optical UAV/satellite reconstruction and provide enough methodological or evaluation detail for coding. Secondary reviews, standards, imagery/software sources, non-optical modalities, and application records without relevant method or evaluation evidence were excluded from the core corpus; boundary records were retained only as context. Supplementary Table S2 documents decisions and exclusion codes.

2.5. Study Selection Process

Records were merged and deduplicated by DOI and normalized title, screened by title/abstract, and assessed at full text. The first author performed initial screening and coding; borderline cases were checked with coauthors and the corresponding author. No automation tool excluded records. The pre-PRISMA draft contained 43 seed studies; database retrieval and reconciliation added 12 eligible studies, yielding the final 55-study corpus used throughout the manuscript and Supplementary Table S1 [19,20,21,22,23,24,25,26,27,32,33,34].

2.6. Study Selection Results

The search identified 279 records (225 database and 54 supplementary records). After removing 62 duplicates, 217 records were screened, 138 excluded, and 79 full texts assessed. Twenty-four were excluded, leaving 55 core studies (Figure 1).

2.7. Data Extraction and Coding

Supplementary Table S1 records citation metadata, corpus role, platform, sensor model, scene extent, initialization, priors, camera handling, representation, scalability strategy, geometric supervision, supervision class, target product, visual/geometry/cost metrics, benchmark relevance, limitations, and code/project availability. The first author applied a predefined matrix; ambiguous entries were checked against source papers and discussed with coauthors. The two principal evaluation lenses are rendering efficiency (time, memory, storage, Gaussian count, compression, and scale) and geometric reliability (height error, surface consistency, completeness, geo-alignment, orthophoto validity, and failures).

2.8. Synthesis Strategy

Heterogeneous platforms, sensors, scenes, supervision, metrics, and outputs precluded meta-analysis. We therefore used a narrative and thematic synthesis organized by platform, sensor model, scalability strategy, and geometric supervision. Original quantitative results are reported descriptively within their dataset and protocol rather than pooled.

2.9. Risk of Bias, Certainty Assessment, and Review Limitations

No intervention-style risk-of-bias or certainty tool was applied to this computational corpus; interpretability was instead assessed through sensor/model disclosure, supervision, metrics, costs, code/data availability, and reported limitations. Important limitations are rapidly changing preprints, less reproducible Google Scholar/citation chasing, heterogeneous protocols, and the absence of a shared executable benchmark. Preprint claims are therefore phrased as author-reported, and the benchmark is demonstrated with published scorecard entries rather than rerun experiments.

2.10. Protocol Registration

The review was not prospectively registered and no separate protocol was prepared. The questions, eligibility criteria, search, screening, coding, synthesis, and corpus-update procedure are documented here and in the Supplementary Materials.

3. Technical Background: From Photogrammetry and NeRF to 3DGS in Remote Sensing

In this section, we provide concise technical background needed for the rest of the review. Our goal is not to trace the full history of photogrammetry, NeRF, or Gaussian-based rendering. Instead, we briefly establish the common geometric language behind these methods and clarify why 3DGS became attractive for remote sensing, while also explaining why its vanilla formulation is insufficient for large-scale UAV and satellite scenarios.

3.1. Classical Photogrammetry Pipelines

Classical photogrammetry reconstructs scene geometry from multi-view image measurements by combining a sensor model, camera orientation, multi-view correspondence, and geometric optimization. In the most common ideal pinhole camera case, the image formation process can be written as
λ   u v 1 = K R t X Y Z 1 ,
where λ is a homogeneous scale factor; ( X , Y , Z ) ⊤ denotes a 3D point in the world coordinate system, written here in homogeneous form as ( X , Y , Z , 1 ) ⊤ ; ( u , v ) ⊤ denotes the corresponding image coordinate, written in homogeneous form as ( u , v , 1 ) ⊤ ; K is the intrinsic matrix; and ( R , t ) are the extrinsic parameters. Figure 3 illustrates the coordinate transformation under the ideal pinhole camera model.
Figure 3. The most common ideal pinhole camera model.
In practice, this projection model is usually embedded in a broader reconstruction pipeline that includes image orientation, bundle adjustment, dense matching, and surface generation.
For remote sensing, however, the projection operator is not always well represented by a simple pinhole model. UAV imagery may require distortion-aware frame-camera calibration, whereas commercial optical satellite imagery may originate from a rigorous sensor model (RSM), be distributed with rational polynomial coefficients (RPCs), or be converted into a local affine or refined approximate camera model for efficient optimization [2,9,10]. It is therefore convenient to write image formation in a unified form as
p = Π θ ( X ) ,
where Π θ ( · ) denotes a sensor-dependent projection function parameterized by camera, orbit, line-array, RPC, or local-approximation parameters θ . This compact notation is useful in the present review because later methods differ less in the existence of geometry than in how they model Π θ , refine θ , and exploit auxiliary constraints such as LiDAR, relative heights, or georeferencing [6,17].
For satellite imagery, the projection chain should be interpreted more explicitly. Commercial high-resolution satellite images may be generated from a rigorous push-broom or line-array sensor model, in which image formation is line-dependent rather than frame-based. If X = ( X , Y , Z ) ⊤ is an object-space point and x = ( ℓ , s ) ⊤ is the corresponding line–sample image coordinate, a simplified line-dependent model can be written as
t ℓ = t 0 + ℓ Δ t ,   x = ( ℓ , s ) ⊤ = Π RSM X ; θ RSM ( t ℓ ) ,
where t ℓ is the imaging time of line ℓ and θ RSM denotes time-dependent orbit, attitude, interior-orientation, and calibration parameters. This notation emphasizes that along-track and cross-track effects can be absorbed incorrectly when satellite images are treated as ordinary perspective frames.
In many practical satellite photogrammetry workflows, the physical sensor model is exposed to users through rational polynomial coefficients (RPCs). After normalizing object-space coordinates to ( X n , Y n , Z n ) , the RPC mapping is commonly expressed as
ℓ n = P ℓ ( X n , Y n , Z n ) Q ℓ ( X n , Y n , Z n ) ,   s n = P s ( X n , Y n , Z n ) Q s ( X n , Y n , Z n ) ,
where P ℓ , Q ℓ , P s , Q s are polynomial functions and ( ℓ n , s n ) are normalized line–sample coordinates. The pixel coordinates ( ℓ , s ) are then obtained through the corresponding image offset and scale parameters. Thus, RPC use in satellite 3DGS should be understood as a compact photogrammetric interface to the satellite image geometry, not as a rejection of rigorous sensor modeling.
Existing satellite 3DGS pipelines usually make this projection compatible with differentiable Gaussian optimization through RPC evaluation, RPC correction, or local affine approximation. At the review level, these choices can be summarized as
Π ref ( X ) = A img   Π RPC ( T obj X ) + b img ,
or, within a bounded tile and height range, by the first-order local approximation
Δ x ≈ J Π ( X 0 ) Δ X ,   J Π ( X 0 ) = ∂ Π ∂ X X 0 .
Here, A img and b img denote image-space affine correction terms, T obj denotes an object-space normalization or transformation, and J Π is the projection Jacobian evaluated around a local expansion point X 0 . These equations do not prescribe a single satellite 3DGS implementation. Rather, they identify the information that should be disclosed when reporting such methods: the projection interface, approximation domain, valid height range, refined variables, and whether the cost of camera/RPC refinement is included in the total runtime.
The limitations of these approximations should also be explicit. RPCs are compact approximations to the physical imaging model and should be used within their stated image extent, normalized-coordinate range, and height domain; residual biases may still require refinement. Local affine cameras are more restrictive because they are first-order approximations around a tile, an expansion point, and an assumed elevation range [6,16]. Their error can increase with tile footprint, off-nadir angle, terrain relief, sensor attitude variation, and distance from the local linearization point. In large-scale high-relief areas such as mountainous regions, a single affine approximation may absorb unmodeled push-broom and terrain-dependent effects as apparent surface deformation, leading to biased DSMs, warped geo-alignment, or block-boundary distortions. Satellite 3DGS papers should therefore report tile size, relief range, height interval, expansion point or linearization strategy, RPC-refinement residuals, and whether high-relief scenes are handled by smaller tiles, direct RPC evaluation, higher-order correction, or a more rigorous sensor model.

3.2. NeRF for Remote Sensing: Strengths and Bottlenecks

NeRF maps 3D position and viewing direction to density and color and renders images through volumetric ray integration [7]. NeRF++, Mip-NeRF 360, S-NeRF, Sat-NeRF, and EO-NeRF extended this formulation to unbounded scenes, scale-aware sampling, shadows, transient objects, multi-date appearance, and RPC-compatible satellite cameras [8,9,10,35,36]. These methods demonstrate the main strengths of radiance fields for remote sensing: continuous scene representation, view-dependent appearance modeling, and joint optimization of radiometry and scene structure. Their repeated field queries and dense ray sampling, however, remain costly for large, sparse-view, or multi-date collections, while photometric supervision alone provides limited control over DSMs, absolute heights, and geo-alignment [10,16,37].
Sensor and reflectance effects have therefore motivated more specialized radiance-field designs. Although not developed specifically for remote sensing, RS-NeRF models rolling-shutter image formation and jointly optimizes row-dependent camera motion, making it transfer-relevant to aerial or UAV frame imagery affected by line-wise readout distortion [38]. SatensoRF replaces repeated hierarchical MLP evaluation with a multiscale tensor decomposition for large multi-date satellite images, reducing parameter count and computation while modeling non-Lambertian appearance and temporal inconsistency [39]. BRDF-NeRF further incorporates the physically motivated semi-empirical Rahman–Pinty–Verstraete reflectance model, guided volumetric sampling, and depth supervision to handle sparse optical satellite views and changing illumination [40]. These developments improve sensor and appearance compatibility, but they do not remove the core bottlenecks of volumetric integration, scene-specific optimization, metadata sensitivity, and weak guarantees for metric products.
The transition from implicit fields to explicit Gaussians reduces repeated neural-field queries but introduces different representation and rasterization constraints. Mip-Splatting addresses scale-dependent aliasing through a 3D smoothing filter and a 2D Mip filter [41]; StopThePop improves view consistency through hierarchical re-sorting and culling of projected splats [42]; and Compact 3D Gaussian Representation reduces Gaussian count and attribute storage through learnable masking, neural color encoding, and vector quantization [43]. Together, these works show that replacing NeRF with 3DGS shifts, rather than eliminates, the main bottlenecks—from dense ray sampling toward aliasing, visibility ordering, and memory/storage—which motivates the explicit 3DGS formulation discussed next.

3.3. Original 3DGS: Explicit Gaussians and Differentiable Rasterization

3DGS replaces implicit per-sample field evaluation with an explicit set of learnable Gaussian primitives [1]. Each Gaussian is associated with a 3D mean μ k , an opacity o k , an anisotropic covariance matrix Σ k , and view-dependent appearance parameters, typically represented by spherical harmonics. A Gaussian kernel centered at μ k can be written as
G k ( x ) = exp   − 1 2 ( x − μ k ) ⊤ Σ k − 1 ( x − μ k ) .
To ensure that Σ k remains positive definite during optimization, it is commonly parameterized through rotation and scaling as
Σ k = R k   S k S k ⊤   R k ⊤ ,
where R k is a rotation matrix and S k is a diagonal scaling matrix [1].
For rendering, the 3D Gaussian is projected into the image plane using a local affine approximation of the camera transform. If W denotes the world-to-camera linear transform and J the Jacobian of the projective mapping around the Gaussian center, the projected covariance can be written as
Σ k 2 D = J   W   Σ k   W ⊤ J ⊤ ,
Here, the depth dimension is omitted after local linearization, so Σ k 2 D denotes the 2 × 2 image-plane covariance used for rasterization. After reducing the local covariance to the image-plane dimensions [1], the contribution of the k-th Gaussian to a pixel p is then modeled by a screen-space opacity
α k ( p ) = o k exp − 1 2 ( p − μ k 2 D ) ⊤ ( Σ k 2 D ) − 1 ( p − μ k 2 D ) ,
and final rendering is obtained by front-to-back alpha compositing:
I ^ ( p ) = ∑ k = 1 K T k ( p ) α k ( p ) c k ,   T k ( p ) = ∏ j < k 1 − α j ( p ) ,
where the Gaussians are depth-sorted before splatting. Figure 4 summarizes the standard pipeline of the original 3DGS method.
Figure 4. The standard pipeline of original 3DGS method.
Compared with NeRF, 3DGS stores geometry and appearance in explicit rasterizable primitives, which enables rapid rendering and adaptive densification from sparse Structure-from-Motion (SfM) initialization [1,29]. The same volumetric flexibility weakens surface guarantees in poorly observed areas. 2D Gaussian Splatting (2DGS) addresses this with surface-oriented splats and depth/normal regularization, while CityGaussianV2 couples large-scene efficiency with stronger geometry [13,44].

3.4. Why Remote Sensing Is Different

Generic 3DGS benchmarks usually assume perspective cameras, dense coverage, bounded scenes, and image-space evaluation. Remote sensing adds distortion-aware UAV cameras, push-broom/RPC satellite geometry, weak or anisotropic parallax, multi-date radiometry, large spatial extent, geodetic coordinates, and mapping products. Consequently, remote-sensing methods must address sensor consistency, scalable optimization, geometric supervision, and product-level validation rather than NVS alone [2,3,6,16,17].

4. Taxonomy of 3DGS for Large-Scale Remote Sensing

Chronology alone does not explain why large-scale 3DGS methods differ. We therefore use a faceted taxonomy with four descriptors: platform, sensor model, scalability strategy, and geometric supervision. Platform and sensor models describe observation conditions; scalability and supervision describe methodological responses. The axes may correlate and are not mutually exclusive. Figure 5 summarizes this structure.
Figure 5. A faceted four-axis taxonomy for 3D Gaussian splatting in large-scale remote sensing. The platform and sensor-model axes describe observation conditions, while the scalability and geometric-supervision axes describe methodological responses. The axes are comparability descriptors rather than mutually exclusive or statistically independent classes.

4.1. Platform Axis: UAV, Satellite, and Cross-Platform Settings

UAV/aerial methods often exploit perspective or distortion-aware cameras, SfM/LiDAR support, GCPs, georeferencing, structural priors, or orthophoto supervision [2,3,4,5,15,24,25,26,27,45]. Satellite methods face long stand-off distance, weak parallax, push-broom/RPC geometry, shadows, and temporal change, motivating affine/RPC modeling, camera refinement, uncertainty, and height-product evaluation [6,9,16,17,18,19,20,21,22,23]. Hybrid methods such as Horizon-GS address cross-altitude integration [46].

4.2. Sensor-Model Axis: From Perspective Cameras to RPC-Compatible Splatting

Generic 3DGS assumes calibrated perspective cameras; remote sensing may require UAV distortion models, pose/georeferencing refinement, LiDAR alignment, or satellite-specific projection [1,2,3,47]. Sat-NeRF, EOGS, EOGS++, and SkySplat span RPC-aware rendering, local affine approximation, internal refinement, and RPC-compatible generalization [6,9,16,17]. Comparisons must disclose projection interface, tile and height domain, terrain relief, refined variables, and residual checks because RPC/affine validity differs between compact low-relief tiles and wide mountainous areas.

4.3. Scalability Axis: Per-Scene Optimization, Partitioning, LoD, and Generalization

Scalability strategies include per-scene optimization, partitioned/parallel training, LoD or hierarchy, pruning/compression, and feed-forward generalization. VastGaussian, CityGaussian, CityGaussianV2, hierarchical 3DGS, Momentum-GS, LightGaussian, Compressed 3DGS, and generalizable pipelines illustrate these choices [11,12,13,14,48,49,50,51,52,53,54]. Their gains must be interpreted against seams, storage, training/pretraining costs, geometry retention, and adaptation requirements.

4.4. Geometric-Supervision Axis: From Photometric Consistency to Mapping-Ready Constraints

Supervision ranges from image-only photometric consistency and internal camera refinement to sparse georeferencing, dense LiDAR/DSM/depth support, semantic or structural priors, and amortized pretraining. Surface-aware methods such as 2DGS, Pixel-GS, SuGaR, Gaussian Surfels, and GaussianPro improve geometric regularity, while ARSGaussian, GeoRefGS, GS4Buildings, EOGS++, GU-GS, and product-oriented methods tie reconstruction to remote-sensing geometry or outputs [2,3,5,17,21,44,45,55,56,57,58]. Supervision labels are therefore required for fair comparison.

4.5. Mapping Representative Methods to the Taxonomy

Table 1 maps representative methods to the four axes. The table is not intended as an exhaustive leaderboard or a set of mutually exclusive classes. It is a structured reading guide for a faceted taxonomy. Our purpose is to show how methods that share the label “Gaussian splatting” differ in platform assumptions, sensor handling, scalability mechanisms, and geometric commitments.
Table 1. Representative methods mapped to the proposed taxonomy. The entries summarize the primary role of each method rather than all implementation details.
The mapping reveals a persistent imbalance: generic large-scene methods are mature in efficiency, whereas remote-sensing methods remain dominated by per-scene optimization and platform-specific priors. UAV methods provide the strongest external geometry, and satellite methods emphasize RPC/affine cameras, temporal robustness, and height recovery. Separating scalability from supervision therefore prevents rendering gains from being mistaken for metric reliability [2,6,11,12,13,15,16,17,18].

5. Scalability and Rendering Efficiency in Large-Scale Remote Sensing

This section treats scalability as an end-to-end property rather than a frame-rate number. For large-scale remote sensing, efficiency includes preprocessing, partitioning, optimization, storage, rendering, product extraction, and the ability to keep geometry reliable as scene extent, image count, and Gaussian count grow [1,6,11,12,13,16,29]. Figure 6 summarizes the main bottlenecks and representative optimization strategies.
Figure 6. Vanilla 3DGS’s bottlenecks and subsequent optimization methods.

5.1. Scaling Bottlenecks

Vanilla 3DGS remains a per-scene optimizer. This is effective for bounded scenes, but large UAV blocks and multi-temporal satellite collections increase Gaussian count, optimizer state, visibility buffers, memory use, and gradient imbalance. A single global Gaussian pool can overfit well-observed regions while leaving weakly constrained roofs, terrain, vegetation, or low-parallax satellite areas unstable [1,11,12]. Remote-sensing products also impose a stronger requirement than view synthesis: a fast renderer is not operationally useful if block seams, weak georeferencing, or unstable height surfaces prevent DSM, orthophoto, mesh, or georeferenced-scene generation [3,5,16,17].

5.2. Efficiency Strategies

Current scaling strategies fall into four groups. Per-scene optimization, used by vanilla 3DGS and many early remote-sensing adaptations, is flexible but costly for repeated scenes [1,16,18]. Partitioned and parallel methods such as VastGaussian, CityGaussian, CityGaussianV2, ULSR-GS, and UAV-specific partitioning approaches reduce memory and training burden but must control seams, cross-block consistency, and partition-dependent density drift [11,12,13,15,32,33]. LoD, compression, pruning, and storage-aware representations reduce deployment cost but can remove fine structures needed for roofs, façades, terrain discontinuities, or product boundaries [12,13,25,34,50,51]. Feed-forward or generalizable pipelines such as pixelSplat, TranSplat, DepthSplat, AnySplat, SkySplat, and SatSurfGS reduce per-scene optimization, but their geometric reliability under sensor heterogeneity, seasonal change, and large geographic extent remains an open evaluation issue [6,14,22,52,53,54].

5.3. Operational Definition

For benchmark use, scalability should be reported as a vector rather than a single score: preprocessing time, training or adaptation time, rendering speed, product-generation time, peak memory, model size, Gaussian count, storage, partition overhead, and geometry retained after scaling or compression. A method that renders quickly but requires heavy manual preprocessing or loses height fidelity is not necessarily more scalable for remote-sensing use. This motivates the next section, which treats metric reliability as a co-equal requirement.

6. Geometric Constraints and Metric Reliability

Remote sensing requires 3DGS to retain metrically stable structure for DSMs, orthophotos, buildings, vegetation, and georeferenced scenes, not merely fast rendering [1].

6.1. Failure Modes Without Explicit Geometry

Weakly constrained 3DGS can improve photometric fit while producing floaters, elongated splats, doubled surfaces, blurred boundaries, unstable thin structures, or depth bleeding. In remote sensing these artifacts are not cosmetic: they can become height errors, roof-edge distortion, orthophoto artifacts, or invalid DSM products. The problem is amplified by sparse or anisotropic views, weak satellite parallax, shadows, multi-date appearance changes, and imperfect camera or RPC models [6,8,9,10,16]. Figure 7 and Figure 8 are qualitative illustrations only; they motivate why photometric-only optimization can fail under temporal change, contamination, occlusion, and missing façade evidence.
Figure 7. An illustrative example of significant temporal variation in multi-date remote-sensing imagery over Shanghai Binjiang Forest Park, Shanghai, China: (a) observation in April 2025, showing comparatively sparse vegetation and more exposed ground surfaces; (b) observation in July 2024, showing denser vegetation cover over the same area. Imagery © 2025 Airbus, accessed via Google Earth Pro on 26 May 2026, and shown here for qualitative illustration only [59].
Figure 8. Illustrative causes of information loss in satellite reconstruction. (a) Cloud or mist contamination. (b) Flyover obstruction. (c) Missing facade evidence under limited viewing geometry. Imagery © 2025 Airbus and Maxar Technologies, accessed via Google Earth Pro on 26 May 2026, and shown here for qualitative illustration only [59].
A methodological consequence is that photometric supervision alone is underdetermined: many 3D configurations can yield similar image-space fidelity under sparse or biased viewing. The most relevant innovations for remote sensing are therefore not just those that improve PSNR, but those that inject, preserve, or evaluate geometry while remaining compatible with efficient Gaussian rendering [2,17,44,45].

6.2. Control-Point-Free and Weakly Supervised Metric Reliability

LiDAR, GCPs, and dense reference DSMs are not always available. In control-point-free satellite or wide-area settings, absolute metric accuracy cannot be certified as an externally validated product, but reliability can still be improved and partially audited through sensor-consistent projection, image-only camera/RPC refinement, multi-view reprojection consistency, epipolar or height-range constraints, surface or normal-depth regularity, temporal/shadow masking, uncertainty estimation, and held-out-view or held-out-date validation. These internal checks should be reported as consistency evidence, not as independent DSM or geo-alignment accuracy; the benchmark framework therefore separates supervision class, reference-data availability, internal consistency, and externally validated product metrics.

6.3. UAV and Airborne Branch: LiDAR Fusion, Alignment, and Regularization

UAV methods provide the clearest geometry-aware examples. ARSGaussian combines LiDAR-guided densification, alignment, geometric consistency, and bundle adjustment; GeoRefGS learns a georeferenced transformation; ULSR-GS, GS4Buildings, and Tortho-Gaussian target surface consistency, structural priors, and true orthophotos [2,3,5,15,45]. Benchmarks must state whether LiDAR, GCPs, georeferencing, priors, or product references are used for training, alignment, post-processing, or evaluation.

6.4. Satellite Branch: RPC Cameras, Bundle Adjustment, and Temporal Robustness

Satellite 3DGS is geometrically demanding because long stand-off distance weakens convergence, push-broom geometry is line-dependent, RPC or affine approximations replace simple perspective cameras, and multi-date collections introduce shadows, seasonal change, and radiometric inconsistency. Sat-NeRF and EO-NeRF already showed that RPC modeling, shadow handling, transient-object treatment, bundle adjustment, and DSM recovery are central in satellite neural reconstruction [9,10]. Gaussian-based satellite methods inherit these constraints: EOGS uses local affine satellite projection, EOGS++ adds camera refinement and TSDF processing, and SatGS, SkySplat, ShadowGS, and SatSurfGS address temporal appearance, RPC-compatible generalization, shadow-aware supervision, and confidence-aware surface recovery [6,16,17,18,19,22].
The remaining limitation is that RPC and affine handling can themselves become a source of geometric error. RPC metadata may be biased or insufficiently refined, and local affine approximations are valid only over limited image tiles and height intervals. The risk is especially high in large mountainous or high-relief regions, where elevation varies rapidly within one tile and the first-order linearization no longer represents the true push-broom/RPC projection. In such cases, the optimizer may compensate for projection error by deforming Gaussian geometry, creating DSM bias, block seams, or geo-alignment distortion. Satellite 3DGS results should therefore report the approximation domain, terrain-relief range, height interval, camera/RPC refinement residuals, tile-size policy, and whether high-relief areas use smaller tiles, direct RPC evaluation, or a more rigorous sensor model.

6.5. Surface-Oriented and Prior-Guided Gaussian Variants

2DGS, SuGaR, and Gaussian Surfels bias Gaussians toward surfaces through flattened primitives, mesh binding, or depth/normal consistency [44,56,57]. CityGaussianV2, GS4Buildings, and Tortho-Gaussian connect these ideas to large scenes, structural priors, and map products [5,13,45]. Because vegetation and clutter are not clean surfaces, future systems may need adaptive mixtures of surface-biased and volumetric primitives.
Figure 9 shows a supervision hierarchy from photometric realism to metric remote-sensing reliability.
Figure 9. A supervision hierarchy from photometric realism to metric remote-sensing reliability.

6.6. From Visual Realism to Measurable Geometry

Remote-sensing 3DGS should be evaluated at three levels: rendering fidelity (PSNR, SSIM, learned perceptual image patch similarity (LPIPS), and visual consistency), geometric reliability (DSM MAE/RMSE, point-to-surface distance, completeness, boundary precision, and height residuals), and geospatial utility (orthophoto production, building reconstruction, geo-registration, or mapping at the intended scale). EOGS/EOGS++, GeoRefGS, GS4Buildings, and Tortho-Gaussian are important because they foreground elevation recovery, geographic alignment, and product-oriented structural quality [3,5,16,17,45]. This reinforces the main thesis: the field must move from visually plausible reconstruction to sensor-aware, scalable, and metrically constrained scene representation.

7. Cross-Platform Synthesis and Benchmark Implications

UAV and satellite 3DGS share three requirements: scalable scene representation, sensor-consistent optimization, and product-level validity. Large-scene methods address Gaussian growth through partitioning, LoD, hierarchy, or compression [11,12,13,48]; remote-sensing methods additionally tie optimization to georeferencing, LiDAR, structural priors, orthophotos, or satellite cameras and height products [2,3,5,6,15,16,17,24,45].
The platforms nevertheless require separate tracks. UAV/aerial imagery usually provides stronger parallax and more external control, supporting LiDAR- or prior-assisted surface and product reconstruction [2,26,27]. Satellite imagery combines push-broom/RPC geometry, weaker baselines, temporal gaps, shadows, and atmospheric variation; SatGS, SkySplat, ShadowGS, SA-GS, GU-GS, SatSurfGS, and semantic-feature methods address appearance, generalization, uncertainty, and DSM recovery [6,18,19,20,21,22,23]. A common reporting core should therefore be paired with platform-specific evaluation.

7.1. Efficiency–Geometry Trade-Offs Across Method Families

Across method families, the core trade-off is scalability versus geometry retention under platform-specific sensing constraints. Partitioning, hierarchy, compression, surface-biased primitives, prior-guided supervision, and generalizable inference each improve one part of the pipeline while changing seam consistency, model size, supervision assumptions, height fidelity, or cost accounting [2,6,11,12,13,15,17,44,45,48,50,51,56,60]. A scientifically useful benchmark should therefore use a Pareto-style scorecard rather than a single aggregate score.
A full same-dataset leaderboard across UAV/aerial and satellite 3DGS is not currently defensible because the reviewed studies differ in scenes, sensor models, supervision regimes, outputs, and metric definitions. Table 2 therefore summarizes reported metric families and comparability limits rather than pooled performance. The shorthand S0–S5, defined formally in Section 8.3, denotes fixed-camera image-only, internally refined image-only, sparse-control/georeferenced, dense-geometry-assisted, semantic/structural-prior-guided, and amortized/generalizable supervision, respectively.
Table 2. Representative reported metrics and comparability limits across large-scale and remote-sensing 3DGS methods. Metric names are summarized at the review level; numerical values should be compared only within the same dataset, split, sensor model, and supervision class.
Table 3 gives a small worked example of how the proposed scorecard can be populated from values reported by original UAV and satellite studies. The table is not a new experiment and does not claim statistical pooling. Its purpose is to demonstrate the benchmark logic: visual quality, DSM/height error, cost, supervision class, and sensor-model assumptions must be read together. For example, a method may report strong image quality in one area of interest while another method reports lower height error or much lower deployment time; the benchmark should expose such trade-offs instead of hiding them behind one aggregate rank.
Table 3. Worked scorecard example using reported UAV and satellite results from the original papers. Values are copied or summarized from the cited studies and should be interpreted only within their reported datasets, splits, masks, and evaluation protocols.

7.2. Implications for Benchmark Design

A credible benchmark must be platform-aware, report efficiency with geometry and product utility, and expose supervision and sensor assumptions. It should therefore use separate tracks, declared supervision classes, decomposed costs, multi-family metrics, and explicit failure reporting rather than a single pooled ranking.

8. Toward a Reproducible Benchmarking Framework

The synthesis above leads to one benchmark principle: large-scale remote-sensing 3DGS should be evaluated through a structured scorecard, not a generic NVS leaderboard. Performance must be interpreted jointly by platform track, sensor model, scalability strategy, supervision class, cost model, visual fidelity, metric geometry, product utility, and failure behavior [2,11,13]. Figure 10 summarizes the proposed framework.
Figure 10. Operational structure of the proposed reproducible benchmark framework for large-scale remote-sensing 3DGS.

8.1. Benchmark Objectives and Design Principles

A useful benchmark should make cross-paper comparison more defensible, expose efficiency–geometry trade-offs, and remain extensible. We therefore define it as dataset-agnostic but metadata-strict and track-based rather than method-centered: each scene must carry standard metadata, and methods should be compared first within declared task settings before any cross-track interpretation.

8.2. Dataset Tracks, Scene Units, and Minimum Metadata

The benchmark defines a scene unit by footprint, images, sensor model, coordinate reference, split, masks, and reference products; tiled areas additionally require boundaries, overlap, and aggregation rules. Four primary tracks are recommended: UAV image/NVS; UAV geometry-product; satellite RPC/multi-view; and satellite multi-temporal robustness, with hybrid UAV–satellite or aerial–ground data treated as exploratory. Direct comparison is restricted to the same track, split, sensor setting, and compatible supervision.
Each release should separate development and locked test scenes and publish, where licensing permits, scene identifiers, checksums, splits, masks, and versioned evaluation scripts. Minimum metadata include footprint, GSD, CRS and vertical datum, acquisition geometry, sensor/camera model, temporal record, preprocessing, reference data, priors, target products, and access restrictions. Satellite records additionally require an RPC source, an affine/refinement strategy, an approximation domain, a height interval, a terrain-relief range, and residual checks. Supplementary File S3 provides the machine-readable YAML schema.

8.3. Supervision Classes and Baseline Method Groups

Baseline grouping should distinguish method family from supervision class. Families describe algorithmic roles; supervision classes describe what information a method is allowed to use. Each experiment should report one or more classes from Table 4—for example, S2 + S3 for GCP + LiDAR supervision or S1 + S5 for pretrained prediction with per-scene RPC refinement. These are comparability labels, not quality levels.
Table 4. Supervision classes for fair comparison of remote-sensing 3DGS methods.
Table 5 groups baseline families by benchmark role: vanilla/direct adaptations, scalable scene management, compression, geometry/surface variants, remote-sensing sensor/prior/product methods, and generalizable feed-forward pipelines. These families are not disjoint—for example, CityGaussianV2, EOGS++, and SkySplat combine multiple roles—but the grouping clarifies which capability is being tested, while supervision classes clarify whether the comparison is fair [6,13,17].
Table 5. Baseline method families and required supervision declaration. Methods are grouped by benchmark role rather than by citation frequency.

8.4. Cost Accounting and Fair Comparison Rules

Fair comparison requires decomposed cost reporting. Let T pre , T train , T pretrain , T adapt , T render , T prod , and T post denote preprocessing, per-scene training, cross-scene pretraining, adaptation, rendering/inference, product generation, and post-processing. For per-scene optimization,
T scene = T pre + T train + T render + T prod + T post ,
whereas generalizable methods report
T deploy = T pre + T adapt + T render + T prod + T post .
They should disclose T pretrain separately. If an amortized total is reported over N eff effective deployment scenes, it should be defined as T amort = T deploy + T pretrain / N eff . Reports must also provide hardware, wall time or GPU-hours, peak memory, stopping rule, output resolution, Gaussian count, model size, and pre/post-compression storage. Required SfM, bundle adjustment, RPC correction, registration, masking, product extraction, and post-processing must not be omitted. Geometry comparisons must use identical coordinate frames, masks, alignment, and references.

8.5. Evaluation Metrics and Geometry Definitions

Four metric families are required: visual fidelity, computational efficiency, metric geometry, and product utility. A minimum report includes PSNR/SSIM/LPIPS; preprocessing, training/adaptation, inference, and product-generation time; peak memory, Gaussian count, and storage; DSM or surface errors when reference data exist; and task-specific orthophoto, building, canopy, or geo-registration measures. CRS, vertical datum, product resolution, masks, alignment, and reference quality must be declared [61,62]. Without independent reference data, reprojection, held-out-view/date, relative-height, normal-depth, temporal, or uncertainty measures must be labeled internal consistency rather than absolute accuracy.
Let Ω eval denote the set of reference-valid evaluation pixels, and let Ω valid ⊆ Ω eval be the subset for which the method returns a valid estimate. For i ∈ Ω valid , define e i z = z ^ i − z i . We also write N valid = | Ω valid | , N eval = | Ω eval | , and
m z = median j ∈ Ω valid e j z .
Default elevation statistics are
MAE z   = 1 N valid ∑ i ∈ Ω valid e i z , RMSE z   = 1 N valid ∑ i ∈ Ω valid e i z 2 1 / 2 , Bias z   = 1 N valid ∑ i ∈ Ω valid e i z .
The normalized median absolute deviation is
NMAD z = 1.4826   median i ∈ Ω valid e i z − m z .
For a tolerance τ , define the valid inlier set Ω τ = { i ∈ Ω valid : e i z ≤ τ } . The valid-pixel inlier rate, coverage, and tolerance-aware completeness are then
Inlier τ   = | Ω τ | N valid , Cov   = N valid N eval , Comp τ   = | Ω τ | N eval .
Surface products should additionally report symmetric point-to-surface distance and normal consistency; orthophotos and georeferenced scenes should report displacement or checkpoint residuals; tiled methods should quantify seam discontinuity. Results should be interpreted as Pareto trade-offs rather than collapsed into one score.

8.6. Failure-Case Reporting and Benchmark Validity

Failure reporting is part of the benchmark, not a supplementary note. In large-scale remote sensing, the most practically important differences between methods often appear in difficult scenes: weak texture, repetitive roofs, water, vegetation, steep relief, low overlap, clouds, shadows, strong seasonal change, poor RPC accuracy, or memory pressure. If failed scenes are silently removed, the benchmark will overestimate both accuracy and robustness.
Every benchmark result should therefore include an attempted-scene count, completed-scene count, valid-product count, and failure-code distribution. A scene should be counted as attempted once the method is launched under the declared protocol. A scene should be counted as completed only if training or inference finishes within the stated resource budget. A scene should be counted as a valid product only if the required output can be evaluated under the benchmark metric script. The success rate should be reported as
R succ = N completed N attempted ,   R valid = N valid   product N attempted .
Non-computable metrics should be reported as missing values with a failure code, not as zero and not as omitted rows. Table 6 illustrates failure-case reporting rules for remote-sensing 3DGS benchmarks.
Table 6. Failure-case reporting rules for remote-sensing 3DGS benchmarks.
Failed scenes should be listed alongside successful ones. Aggregate metrics should use completed and valid scenes, while R succ and R valid are computed over all attempted scenes.

8.7. Reproducibility and Reporting Checklist

Reproducibility should be treated as a benchmark deliverable because alignment choices, camera/RPC refinement, and failed-scene handling can change the interpretation of results [63,64,65]. Each comparison should disclose, where licensing permits, scene IDs, dataset versions, splits, masks, metadata, sensor/prior descriptions, supervision class, training configuration, hardware/software environment, cost accounting, metric scripts, failure logs, released artifacts, and code commits. If raw data cannot be redistributed, scene identifiers, access restrictions, metadata, split files, and evaluation scripts should still be provided. The machine-readable template in Supplementary File S3 is intended to standardize this disclosure.

8.8. Scope and Limitations of the Proposed Framework

The framework is modular rather than closed. Public scenes remain uneven across UAV and satellite settings, geometric references are not always available, priors can be difficult to standardize, and generalizable pipelines have cost models unlike per-scene optimization. Satellite tracks also require explicit terrain stratification: RPC or affine approximations that are adequate for compact low-relief urban tiles may be unsafe for wide mountainous regions unless tile size, height range, residuals, and sensor-model validity are documented. The framework therefore functions as an extensible reporting template that makes track, metadata, sensor model, supervision, cost, geometry definition, product target, and failure behavior explicit rather than hidden in experimental setup.

9. Conclusions

This review argues that large-scale remote-sensing 3DGS should not be interpreted simply as a faster substitute for generic novel-view synthesis. The current evidence suggests that its practical value depends on whether efficient Gaussian representations can remain sensor-consistent, geometrically reliable, and usable for downstream geospatial products. The four-axis taxonomy developed here helps explain why the literature diverges across platform, projection model, scalability strategy, and supervision regime.
From this perspective, progress in remote-sensing 3DGS is likely to depend less on rendering speed alone than on the joint improvement of metric geometry, georeferencing fidelity, cost transparency, and reproducible evaluation. The benchmark framework proposed in this review is therefore deliberately modular. It supports platform-aware tracks, declared supervision classes, explicit cost accounting, and joint reporting of visual, geometric, and product-level metrics. Future advances will be most useful when they connect scalable Gaussian representations with sensor-aware optimization and mapping-ready outputs under clearly documented evaluation protocols.

Supplementary Materials

The following supporting information can be downloaded at: https://www.mdpi.com/article/10.3390/rs18132224/s1. Supplementary Table S1: Paper-level coding matrix for the reviewed 3DGS corpus. This spreadsheet records the 55 coded core technical studies, including corpus classification, taxonomy labels, supervision classes, benchmark-track assignments, reported metrics, efficiency or cost information, geometry or product metrics, reproducibility fields, limitations, source links, and code or project availability where reported. Supplementary Table S2: PRISMA search, deduplication, screening, and eligibility log. This spreadsheet records the source-specific search strategy, retrieval counts, deduplication process, title/abstract screening decisions, full-text eligibility decisions, exclusion reasons, and final inclusion status used to construct the 55-study core corpus. Supplementary File S1: Completed PRISMA 2020 checklist. This file provides the completed PRISMA 2020 checklist and indicates where each reporting item is addressed in the manuscript or Supplementary Materials based on the official PRISMA template. Supplementary File S2: PRISMA 2020 flow diagram. This file summarizes the identification, screening, eligibility assessment, and inclusion process for the 55-study core corpus based on the official PRISMA template. Supplementary File S3: Machine-readable benchmark metadata template. This YAML file provides a scene-level metadata template for the proposed benchmark framework.

Author Contributions

Conceptualization, W.F.; methodology, W.F., B.W. and J.Y.; investigation, W.F., J.Y. and B.W.; writing—original draft preparation, W.F.; writing—review and editing, W.F. and R.Z.; supervision, H.C. All authors have read and agreed to the published version of the manuscript.

Funding

This research and the APC were funded by the Shanghai-Africa International Joint Laboratory for Optoelectronic Remote Sensing and Early Warning in Disaster Mitigation; no grant number was assigned.

Data Availability Statement

No new experimental measurements, remote-sensing datasets, or rerun benchmark results were generated in this study. The worked scorecard example uses values reported in the cited original studies and is intended only to demonstrate the proposed reporting structure. The review-derived paper-level coding matrix for the 55 core technical studies is provided in Supplementary Table S1. The PRISMA search, deduplication, screening, and eligibility log is provided in Supplementary Table S2. The completed PRISMA 2020 checklist and PRISMA flow diagram are provided as Supplementary File S1 and Supplementary File S2, respectively. A reusable benchmark metadata template supporting the proposed benchmarking framework is provided as Supplementary File S3.

Acknowledgments

The authors thank Zhang Yuning for helpful discussions and manuscript feedback. During the preparation of this manuscript, the authors used GPT-5.5 for language polishing and organization of revision materials. The authors reviewed and edited the output and take full responsibility for the content of this publication.

Conflicts of Interest

Author H.C. was employed by the company Shanghai Etherspace Technology Co., Ltd. Apart from providing funding support for the research and APC, the funder had no role in the preparation of the manuscript or in the decision to publish the results. The remaining authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.

Abbreviations

The following abbreviations are used in this manuscript:
2DGS2D Gaussian Splatting
3DGS3D Gaussian Splatting
CRSCoordinate Reference System
DEMDigital Elevation Model
DSMDigital Surface Model
FPSFrames Per Second
GCPsGround Control Points
GNSSGlobal Navigation Satellite System
GSDGround Sampling Distance
IMUInertial Measurement Unit
LiDARLight Detection and Ranging
LoDLevel of Detail
LoD2Level of Detail 2
LPIPSLearned Perceptual Image Patch Similarity
MAEMean Absolute Error
MVSMulti-View Stereo
NeRFNeural Radiance Field
NMADNormalized Median Absolute Deviation
NVSNovel View Synthesis
PANPanchromatic
PSNRPeak Signal-to-Noise Ratio
PRISMAPreferred Reporting Items for Systematic Reviews and Meta-Analyses
RMSERoot Mean Square Error
RPCRational Polynomial Coefficients
RSMRigorous Sensor Model
SfMStructure from Motion
SSIMStructural Similarity Index Measure
TSDFTruncated Signed Distance Function
UAVUnmanned Aerial Vehicle
VRAMVideo Random Access Memory

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