1 Introduction
In this work we focus on surface reconstruction from multiscale multiview stereo (MVS) point clouds. These point clouds receive increasing attention as their computation only requires simple 2D images as input. Thus the same reconstruction techniques can be used for all kinds of 2D images independent of the acquisition platform, including satellites, airplanes, unmanned aerial vehicles (UAVs) and terrestrial mounts. These platforms allow to capture a scene in a large variety of resolutions (aka scale levels or levels of details). A multicopter UAV alone can vary the level of detail by roughly two orders of magnitude. If the point clouds from different acquisition platforms are combined, there is no limit to the possible variety of point density and 3D uncertainty. Further, the size of these point clouds can be immense. Stateoftheart MVS approaches [10, 11, 12, 28] compute 3D points in the order of the total number of acquired pixels. This means that they generate 3D points in the order of per taken image with a modern camera. In a few hours of time, it is thus possible to acquire images that result in several billions of points.
Extracting a consistent surface mesh from this immense amount of data is a nontrivial task, however, if such a mesh could be extracted it would be a great benefit for virtual 3D tourism. Instead of only being able to experience a city from far away, it would then be possible to completely immerge into the scene and experience cultural heritage in full detail.
However, current research in multiscale surface reconstruction focuses on one of two distinct goals (aside from accuracy). One group (e.g. [8, 21]) focuses on scalability through local formulations. The drawback of these approaches is that the completeness often suffers; i.e. many holes can be seen in the reconstruction due to occlusions in the scene, which reduces the usefulness for virtual reality. The second group (e.g. [31, 33]) thus focuses on obtaining a closed mesh through applying global methods. For obtaining the global solution, these methods require all data at once, which sadly precludes them from being scalable. Achieving both goals at once, scalability and a closed solution, might be impossible for arbitrary jumps in point density. The reason for this is that any symmetric neighborhood on the density jump boundary can have more points in the denser part than fit into memory, while having only a few or even no points in the sparse part. However, scalability requires independent subproblems of limited size, while a closed solution requires sufficient overlap for joining them back together. To mitigate this problem, we formulate our approach as a hybrid between global and local methods.
First, we separate the input data with a coarse octree, where a leaf node typically contains thousands of points. The exact amount of points is an adjustable parameter that represents the tradeoff between completeness and memory usage. Within neighboring leaf nodes, we perform a local Delaunay tetrahedralization and maxflow mincut optimization to extract local surface hypotheses. This leads to many surface hypotheses that partially share the same base tetrahedralization, but also intersect each other in many places. To resolve these conflicts between the hypotheses in a nonvolumetric manner, we propose a novel graph cut formulation based on the individual surface hypotheses. This formulation allows us to optimally fill holes which result from local ambiguities and thus maximize the completeness of the final surface. This allows us to handle point clouds of any size with a constant memory footprint, where the capability to close holes can be traded off with the memory usage. Thus we were able to generate a consistent mesh from a point cloud with 2 billion points with a ground sampling variation from 1m to 50m using less than 9GB of RAM per process (see Fig. 1 and video [24]).
2 Related Work
Surface reconstruction from point clouds is an extensively studied topic and a general review can be found in [5]. In the following, we focus on the most relevant works with respect to multiscale point clouds and scalability.
Many surface reconstruction approaches rely on an octreestructure for data handling. While it has been shown by Kazhdan et al. [20] that consistent isosurfaces can be extracted from arbitrary octree structures, the vast scale differences imposed by multiview stereo lead to new challenges for octreebased approaches. Consequently, fixed depth approaches (e.g. [16, 19, 6]) are not wellsuited for this kind of input data. Thus, Muecke et al. [27] handle scale transitions in computing meshes on multiple octree levels within a crust of voxels around the data points and stitching the partial solutions back together. However, this approach is not scalable due to its global formulation. Fuhrmann and Goesele [8] therefore propose a completely local surface reconstruction approach, where they construct an implicit function as the sum of basis functions. While this approach is scalable from a theoretical stand point, the interpolation capabilities are very limited due to a very small support region. Furthermore, the pure local nature of the approach is unable to cope with mutually supporting outliers (e.g. if one depthmap is misaligned with respect to the other depthmaps), which occur quite often in practice (see experiments). Kuhn et al. [21] reduce this problem by checking for visibility conflicts in close proximity (10 voxels) of a measurement. Nevertheless, this approach still has very limited interpolation capabilities compared to global approaches. Recently, Ummenhofer and Brox [31] proposed a global variational approach for surface reconstruction of large multiscale point clouds. While they report that they can process a billion points, the required memory foot print for this problem size is already considerable (152 GB). Aside from not being scalable due to the global formulation, this approach also needs to balance the octree. As our experiments demonstrate, this leads to severe problems if the scale difference is too large.
Aside from octreebased approaches, there is also a considerable amount of work that is based on the Delaunay tetrahedralization of the 3D points [13, 15, 18, 22, 23, 33]. Opposed to octreebased approaches, the Delaunay tetrahedralization splits the space into uneven tetrahedra and thus grants these approaches the unique capability to close holes of arbitrary size for any point density. The key property of these approaches is that they build a directed graph based on the neighborhood of adjacent tetrahedra in the Delaunay tetrahedralization. The energy terms within the graph are then set according to rays between the cameras and their corresponding 3D measurements. These visibility terms make this type of approaches very accurate and robust to outliers. The main differences between the approaches mentioned above are how the smoothness terms are set and what kind of postprocessing is applied. One property that all of these approaches share is that they are all based on global graph cut optimization, which precludes them from scalability. However, the complete resilience to changes in point density makes these approaches ideal for multiview stereo surface reconstruction, which motivated us to scale up this type of approaches.
3 Global Meshing by Labatut et al.
Our base method is a global meshing approach by Labatut et al. [22], which requires a point cloud with visibility information as input (i.e. which point was reconstructed using which cameras/images). With this data, they first compute the Delaunay tetrahedralization of the point cloud. This leads to a set of tetrahedra which are connected to their neighbors through their facets. If the sampling is dense enough, it has been shown that this tetrahedralization contains a good approximation of the real surface [3]. Now the main idea of [22] was to construct a dual graph representation of the Delaunay tetrahedralization and perform graph cut optimization on this dual graph to extract a surface (a visual representation of the dual graph is plotted in Fig. 2). They formulated the problem such that after the optimization each tetrahedron is either labeled as inside or outside. This results in a watertight surface, which is the minimum cut of the graph cut optimization and represents the transition between tetrahedra labeled as inside and outside.
The following optimization problem is solved by the graph cut optimization to find the surface :
(1) 
where is the data term and represents the penalties for the visibility constraint violations (i.e. ray conflicts, see Fig. 2.c). is the regularization term and is the sum of all smoothness penalties across the surface. is a factor that balances the data and the regularization term and thus it controls the degree of smoothness.
Many ways have been proposed to set these energy terms [13, 15, 18, 22, 23, 33]. In an evaluation [25] on the Strecha dataset [30], we found that a constant visibility cost (Fig. 2.c) and a small constant regularization cost (per edge/facets) lead to very accurate results. Thus we used this energy formulation with in all our experiments. Note that this base energy formulation is not crucial for our approach and can be replaced by other methods.
4 Making It Scale
To scale up the base method, it is necessary to first divide the data into manageable pieces, which we achieve with an unrestricted octree. On overlapping data subsets, we then solve the surface extraction problem optimally and obtain overlapping hypotheses. This brings us to the main contribution of our work, the fusion of these hypotheses. The main problem is that the property which gives the base approach its unique interpolation properties (i.e. the irregular space division via Delaunay tetrahedralization) also makes the fusion of the surface hypotheses a nontrivial problem. We solve this problem by first collecting consistencies between the mesh hypotheses and then filling the remaining holes via a second graph cut optimization on surface candidates. In the following we explain all important steps.
Dividing and conquering the data.
For dividing the data, we use an octree, similar to other works in this field [8, 20, 21, 27]. In contrast to these works, we treat leaf nodes (aka voxels) of the tree differently. Instead of treating a voxel as smallest unit, we only use it to reduce the number points to a manageable size. We achieve this by subdividing the octree nodes until the number of points within each node is below a fixed threshold. As we want to handle density jumps of arbitrary size, we do not restrict the transition between neighboring voxels. This means that the traditional local neighborhood is not well suited for combining the local solutions, as this neighborhood can be very large at the transition between scale levels. Instead, we collect all unique voxel subsets, where each voxel in the set touches the same voxel corner point (corner point, edge and plane connections are respected). This limits the maximum subset size to 8 voxels. For each voxel subset, we then compute a local Delaunay tetrahedralization and execute the base method (Sec. 3) to extract a surface hypothesis. The resulting hypotheses strongly overlap each other in most parts, but inconsistencies arise at the voxel boundaries. In these regions, the tetrahedra topology strongly differs, which results in a significant amount of artifacts and ambiguity. For this reason, standard mesh repair approaches such as [17, 4] are not applicable.
Building up a consistent mesh.
In a first step, we collect all triangles (within each voxel) which are shared among all local solutions and add them to the combined solution. In the following ”combined solution” will always refer to the current state of the combined surface hypothesis. Note that the initial combined solution is already a valid surface hypothesis with many holes. Triangles which are part of the combined solution are not revised by any subsequent steps. Then we look for all triangles that span between two voxels and are in the local solution of all voxel subsets that contain these two voxels. If these triangles separate two final tetrahedra, we add them to the combined solution. In our case, a final tetrahedron is a tetrahedron where the circumscribing sphere does not reach outside the voxel subset. After this step, the combined solution typically contains a large amount of holes at the voxel borders.
In the next step, we want to find edgeconnected sets of triangles (we will further refer to these sets as ”patches”) with which we can close the holes in the combined solution. To create patch candidates, we search through the local solutions. First, we remove triangles that would violate the twomanifoldness of the combined solution (i.e. connecting a facet to an edge that already has two facets) or would intersect the combined solution. Then we cluster all remaining triangles in linear time to patches via their edge connections. On a voxel basis, we now end up with many patch candidates. While many candidates might be used to close a hole, it happens that some of them are more suitable than others. As the base approach produces a closed surface for each voxel subset, this also means that it closes the surface behind the scene. To avoid that such a patch is used rather than one in the foreground, we rank the quality of a patch by its centricity in the voxel subset. In other words, we prefer patches which are far away from the outer border of the voxel subset, as the Delaunay tetrahedralization is more stable in these regions. We compute the centricity of a patch as:
(2) 
where is the centroid of the patch , is the set of inner points (Fig. 3) of the voxel subset of . is the distance from the inner point to the farthest corner of the voxel in which lies, which normalizes the centricity to [0,1].
For each voxel, we now try to fit the candidate patches in descending order, while ensuring that the outer boundary completely connects to the combined solution without violating the twomanifoldness or intersecting the combined solution. If such a patch is found it is added to the combined solution. Thus this step closes holes which can be completely patched with a single local solution.
Hole filling via graph cut
To deal with parts of the scene where the local Delaunay tetrahedralizations are very inconsistent, we propose a graph cut formulation on the triangles of a patch candidate. For efficiency, this graph cut operates only on surface patches for which the visibility terms have already been evaluated by the first graph cut. The idea behind the formulation is to minimize the total length of the outer mesh boundary.
First, we rank all candidate patches by centricity. For the best patch candidate, we extract all triangles in the combined solution which share an edge connection with the patch. The edges connecting the combined solution with the patch define the ”hole” which we aim to close or minimize (we refer to this set of edges as and the corresponding set of triangles as ). Within the set of patch triangles (), we now want to extract the optimal subset of triangles () such that the overall outer edge length is minimized:
(3) 
where is the set of outer edges (i.e. edges only shared by one triangle) defined through the triangle subset and .
We achieve this minimization with the following graph formulation (see also Fig. 4). For each triangle in the hole set and the patch we insert a node in the graph. Then we insert edges with infinite capacity from the source to all triangles/nodes in (to force this set of triangles to be part of the solution). All triangles in are then connected to their neighbors in with directed edges, where the capacity of the edge in the graph corresponds to the edge length in 3D. Similarly, we insert two graph edges for each pair of neighboring triangles in , where the capacity is also equal to the edge length. Finally, we insert a graph edge for each outer triangle (i.e. all triangles with less than three neighbors). These edges are connected to the sink and their capacity is the sum of all outer edges of the triangle. Through this formulation, the graph cut optimization minimizes the total length of the remaining boundary. After the optimization, all triangles which are needed for the optimal boundary reduction are contained in the source set of the graph. These triangles are added to the combined solution and the process is repeated with the next patch candidate.
5 Experiments
We split our experiments into three parts. First, we present qualitative results on a publicly available multiscale dataset [9] and a new cultural heritage dataset with an extreme density diversity (from 1m to 50m). Second, we evaluate our approach quantitatively on the Middlebury dataset [29] and the DTU dataset [1]. Third, we assess the breakdown behavior of our approach in a synthetic experiment, where we iteratively increase the point density ratio between neighboring voxels up to a factor of 4096.
For all our experiments, we use the same set of parameters. The most interesting parameter is the maximum number of points per voxel (further referred to as ”leaf size”), which represents the tradeoff between completeness and memory usage. We set this parameter to 128k points, which keeps the memory consumption per process below 9GB. Only in our first experiment (Citywall), we vary this parameter to assess its sensitivity (which turns out to be very low). As detailed in our technical report [25], the base method per se is not able to handle Gaussian noise without a loss of accuracy. Thus, we apply simple pre and postprocessing steps for the reduction of Gaussian noise. As preprocessing step, we apply scale sensitive point fusion. Points are iteratively and randomly drawn from the set of all points within a voxel. For each drawn point, we fuse the knearest neighbors within a radius of 3 times the point scale (points cannot be fused twice). This step can be seen as the nonvolumetric equivalent to the fusion of points on a fixed voxel grid. The knn criterion only prohibits that uncertain points delete too many more accurate points. We select k such that all points of similar scale within the radius are fused if no significantly finer scale is present (leading to ). As postprocessing, we apply two iterations of HCLaplacian smoothing [32]. Both, post and preprocessing, are computationally negligible compared to the meshing itself (less than 1% of the runtime). All experiments reporting timings were run on a server with 210GB accessible RAM and 2 Intel(R) Xeon(R) CPU E52680 v2 @ 2.80GHz, which totals in 40 virtual cores. For merging the local solutions back together, we process the local solutions on a voxel basis. If patch candidates extend in other voxels, these voxels are locked to avoid race conditions. To minimize resource conflicts, we randomly choose voxels which are delegated to worker processes. The number of worker processes is adjusted to fit the memory of the host machine.
5.1 Qualitative Evaluation
For multiscale 3D reconstruction there currently does not exist any benchmark with ground truth. Thus, qualitative results are the most important indicator for comparing 3D multiscale meshing approaches. On two datasets, we compare our approach to two stateoftheart multiscale meshing approaches. The first approach (FSSR [8]) is a completely local approach, whereas the second approach (GDMR [31]) contains a global optimization. For our approach, we only use a single ray per 3D point (from the camera of the depthmap).
Citywall dataset.
The Citywall dataset [9] is publicly available and consists of 564 images, which were taken in a handheld manner and contain a large variation of camera to scene distance. As input we use a point cloud computed with the MVE [9] pipeline on scale level 1, which resulted in 295M points. For this experiment, we used the same parameters as used in [31] for FSSR and GDMR. For FSSR, the ”meshclean” routine was used as suggested in the MVE users guide with ”t10”. Aside from the visual comparisons (Fig. 5), we use this dataset also to evaluate the impact of choosing different leaf sizes (maximum numbers of points per voxel) on the quality and completeness of the reconstruction (Fig. 5) and the memory consumption (Tab. 1).
leaf size  512k  128k  32k  8k 

Peak Mem [GB]  25.3  8.9  3.1  2.2 
In matters of completeness, we can see in Fig. 5 that our approach lies in between FSSR (a local approach) and GDMR (a global approach). The degree of completeness can be adjusted with the leaf size. A large leaf size leads to a very complete result, but the memory consumption is also significantly higher (see Tab. 1). However, even with very small leaf sizes (8k points), the mesh is completely closed in densely sampled parts of the scene.
If we compare the quality of the resulting mesh to FSSR and GDMR, we see that our approach preserves much more fine details and has significantly higher resilience against mutually supporting outliers (red circles). The degree of resilience declines gracefully when the leaf size becomes lower, and even for 8k points the output is, in this respect, at least as good as FSSR and GDMR. The drawback of our method is that the Gaussian noise level is somewhat higher compared to the other approaches, which could be reduced with more smoothing iterations.
Valley dataset.
The Valley dataset is a cultural heritage dataset, where the images were taken on significantly different scale levels. The most coarse scale was recorded with a manned and motorized hang glider, the second scale level with a fixed wing UAV (unmanned aerial vehicle), the third with an autonomous octocopter UAV [26] and the finest scale with a terrestrial stereo setup [14]. Each scale was reconstructed individually and then georeferenced using offline differential GPS measurements of ground control points (GCPs), total station measurements of further GCPs and a prism on the stereo setup [2]. The relative alignment was then finetuned with ICP (iterative closest point). On each scale level we densified the point cloud using SURE [28], which was mainly developed for aerial reconstruction and is therefore ideally suited for this data. We compute the point scale for SURE analog to MVE as the average 3D distance from a depthmap value to its neighbors (4neighborhood). The resulting point clouds have the following size and ground sampling distance: Stereo setup (1127M points @ 4347m), octocopter UAV (46M points @ 3.515mm), fixed wing UAV (162M points @ 35cm) and hang glider (572M points @ 10100cm), which sums up to 1.9 billion points in total. This dataset is available [24].
On this dataset, FSSR and GDMR were executed with the standard parameters, which also obtained the ”best” results for SURE input on the DTU dataset (see Sec. 5.2). However, both approaches ran out of memory with these parameters on the evaluation machine with 210 GB RAM. To obtain any results for comparison we increased the scale parameter (in multiples of two) until the approaches could be successfully executed, which resulted in a scaling factor of 4 for FSSR and GDMR. The second problem of the reference implementations is that they use a maximum octree depth of 21 levels for efficient voxel indexing, but this dataset requires a greater depth. Thus both implementations ignore the finest scale level. To still evaluate the transition capabilities between octocopter and stereo scale, we also executed both approaches on only these two scale levels (marked as ”only subset”). The overall runtimes were 1.5 days for GDMR, 0.5 days for FSSR and 9 days for our approach. One has to be keep in mind that FSSR and GDMR had two octree levels less (data reduction between 16 and 64), additionally to throwing away the lowest scale (half of the points). Furthermore, our approach only required 119GB of memory with 16 processes, whereas GDMR required 150GB and FSSR 170GB, despite the large data reduction. Per process our approach once again required less than 9GB. In Fig. 6 we show the results of this experiment. Note that even without the 2 coarser scale levels, both reference approaches are unable to consistently connect the lowest scale level. In contrast, our approach produces a single mesh that consistently connects all scale levels from 6 down to submillimeter density (see video [24]).
5.2 Quantitative Evaluation
For the quantitative evaluation, we use the Middlebury [29] and the DTU dataset [1]. Both datasets are single scale and have relatively small data sizes (Middlebury 96Mpix, DTU 94Mpix). However, they provide ground truth and allow us to show that our approach is highly competitive in matters of accuracy and completeness.
Thr.  PSR [19]  SSD [7]  FSSR  GDMR  OURS 

90%  0.36  0.38  0.40  0.42  0.35 
97%  0.56  0.56  0.63  0.61  0.54 
99%  0.84  0.75  0.84  0.78  0.71 
Middlebury dataset.
Following the foot steps of [8, 27, 31], we evaluate our approach on the Middlebury Temple Full dataset [29]. This established benchmark consists of 312 images and a nonpublic ground truth. For fairness, we use the same evaluation approach as [31] and report our results for a point cloud computed with MVE [9] in Tab. 2. In this setup, our approach reaches the best accuracy on all accuracy thresholds with a very high completeness (for 1.25mm: OURS: 99.7%, FSSR: 99.4%, GDMR: 99.3%). A visual comparison can be found in the supplementary [24]. Among all evaluated MVS approaches we are ranked second [29] (on March/10/2017). Only [34] obtained a better accuracy in the evaluation, and they actually focus on generating better depthmaps and not surface reconstruction.
DTU dataset.
The DTU Dataset [1] consists of 124 miniature scenes with 49/64 RGB images and structuredlight ground truth for each scene. However, the ground truth contains a significant amount of outliers, which in our opinion requires manual cleaning for delivering expressive results. Thus, we hand picked one of the scenes (No. 25) and manually removed obvious outliers (see supplementary [24]). We chose this scene as it contains many challenging structures (fences, umbrellas, tables, an arc and a detached signplate) additional to a quite realistic facade model. On this data, we evaluate three different meshing approaches (FSSR [8],GDMR [31] and OURS) on the point clouds of three stateoftheart MVS algorithms (MVE [9],SURE [28] and PMVS [10]).
For our approach, we used a maximum leaf size of 128k points which results peak memory usage per process of below 9GB. For FSSR we swept the scale multiplication factor and for GDMR and in multiples of two. In Tab. 3, we compare our approach to the ”best” values of FSSR and GDMR. With ”best” we mean that the sum of the median accuracy and completeness is minimal over all evaluated parameters. A table with all evaluated parameters can be found in the supplementary [24].
If we take a look at the results, we can see that the relative performance of each approach is strongly influenced by the input point cloud. For PMVS input, our approach is ranked second in all factors, while FSSR obtains a higher accuracy at the cost of lower completeness and GDMR higher completeness at the cost of lower accuracy. On SURE input, our approach performs worse than the other two. Note that in this scene, SURE produces a great amount of mutually consistent outliers through extrapolation in textureless regions. These outliers cannot be resolved with the visibility term as all cameras observe the scene from the same side. For MVE input, our approach achieves the best rank in nearly all evaluated factors.
MVE  MeanAcc  MedAcc  MeanCom  MedCom 

FSSR  0.673 (2)  0.396 (3)  0.430 (3)  0.239 (1) 
GDMR  1.013 (3)  0.275 (2)  0.423 (2)  0.284 (3) 
OURS  0.671 (1)  0.262 (1)  0.423 (1)  0.279 (2) 
SURE  MeanAcc  MedAcc  MeanCom  MedCom 
FSSR  1.044 (1)  0.490 (3)  0.431 (1)  0.257 (1) 
GDMR  1.099 (2)  0.301 (1)  0.519 (3)  0.357 (2) 
OURS  1.247 (3)  0.365 (2)  0.509 (2)  0.368 (3) 
PMVS  MeanAcc  MedAcc  MeanCom  MedCom 
FSSR  0.491 (1)  0.318 (1)  0.624 (3)  0.395 (3) 
GDMR  0.996 (3)  0.355 (3)  0.537 (1)  0.389 (1) 
OURS  0.626 (2)  0.341 (2)  0.567 (2)  0.390 (2) 
5.3 Breakdown Analysis
In this experiment, we evaluate the limits of our approach with respect to point density jumps. Thus we construct an artificial worst case scenario, i.e. a scenario where the density change happens exactly at the voxel border. Our starting point is a square plane where we sample 2.4 million points and to which we add some Gaussian noise in the zaxis. The points are connected to 4 virtual cameras (visibility links), which are positioned fronto parallel to the plane. Then we subsequently reduce the number of points in the center of the plane by a factor 2 until we detect the first holes in the reconstruction (which happened at a reduction of 64). Then we reduce the point density by a factor 4 until a density ratio of 4096.
In Fig. 7 we show the most relevant parts of the experiment. Up to a density ratio of 32, our approach is able to produce a holefree mesh as output. If we compare this to a balanced octree (where the relative size of adjacent voxels is limited to a factor two), we can perfectly cope with 8 times higher point densities. When the ratio becomes even higher, the number of holes at the transition rises gradually. In Fig. 7, we can see that graph cut optimization is able to reduce the size of the remaining holes significantly, even for a density ratio of 4k. This means that even for extreme density ratios of over 3 orders we can still provide a result, albeit one that contains a few holes at the transition.
6 Conclusion
In this paper we presented a hybrid approach between volumetric and Delaunaybased surface reconstruction approaches. This formulation gives our approach the unique ability to handle multiscale point clouds of any size with a constant memory usage. The number of points per voxel is the only relevant parameter of our approach, which directly represents the tradeoff between completeness and memory consumption. In our experiments, we were thus able to reconstruct a consistent surface mesh on a dataset with 2 billion points and a scale variation of more than 4 orders of magnitude requiring less than 9GB of RAM per process. Our other experiments demonstrated that, despite the low memory usage, our approach is still extremely resilient to outlier fragments, vast scale changes and highly competitive in accuracy and completeness with the stateoftheart in multiscale surface reconstruction.
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Appendix A Supplementary Material
This section contains further details about the experiments conducted in the main paper.
Citywall dataset [9].
In Tab. 4, we provide a much more detailed version of Tab. 1 in the main paper. Here, the table shows which step of our approach was run with how many processes. We tried to select the number of processes such that we were sure not to exceed the memory of the server (210GB). Note that, we did not have exact knowledge of the memory consumption of each step with respect to the leaf size prior to the experiment. As the number of processes is varying per step, we normalized the runtimes to 40 virtual processes (the number of virtual cores of the server). The normalized time was computed as real runtime num processes / 40.
Middlebury dataset [29].
For the readers convenience, we downloaded and grouped the visual results from the official evaluation homepage [29]. Thus, we visual these results in Fig. 8. As detailed in the main paper (Tab. 2), we achieve better accuracy scores than all other approaches that were executed MVE [9] input. We assume that this is the case, because our approach preserves more detail than the other approaches (see bottom row).
DTU dataset [1].
For getting a fair comparison with the reference approaches, we performed a sweep of the most important parameters for FSSR [8] and GDMR [31]. For FSSR we changed the scale multiplication factor and for GDMR jointly and in multiples of two. In the main paper, we only report the scores of ”best” parameters. With ”best” we mean that the sum of the median accuracy and completeness is minimal over all evaluated parameters. The complete set of results for MVE [9],SURE [28] and PMVS [10] is in shown in Tab. 5, 6 and 7, where we marked the values reported in the main paper in bold font. Note that the standard parameters won in all cases except for PMVS (Tab. 7). We assume that the reason for this is that PMVS generates less points with standard parameters; i.e. and increase the theoretic point radius more or less by 4.
As the DTU dataset contains a significant amount of outliers in the ground truth, we cleaned the ground truth of scene 25 manually (see Fig. 9). We additionally provide the cleaned ground truth online [24]. In Fig. 9 we also show the errorcolored point clouds generated by the evaluation system of [1]. If we take a look at the results, we can see that GDMR and our approach are more robust to outliers than FSSR (see median accuracy with MVE and SURE input). If nearly no outliers are present (PMVS), FSSR reaches the best accuracy, at the cost of leaving many holes in the facade. On dense parts of the scene (mostly the facade), GDMR and our approach perform very similar, however we can see a significant difference in parts where no input points constrain the algorithms. The formulation of GDMR prefers smooth normal transitions, which can lead to unwanted bubbles (see umbrellas). Our approach instead prefers to close holes with planes. In this example, this strategy leads to a better mean accuracy. In the presence of many outliers (SURE), our approach can successfully remove outliers if they cause a ray conflict (right side of the terrace), while other outliers remain (left side of the arc).
leaf size  512k  128k  32k  8k 

num leaves  194  695  2675  10123 
running base approach [22]  
num processes  32  32  32  32 
real runtime [h]  38.9  30.0  18.5  12.0 
runtime/40 proc [h]  31.1  24.0  14.8  9.6 
extracting candidate patches  
num processes  16  32  32  32 
real runtime [h]  6.2  3.3  3.6  4.0 
runtime/40 proc [h]  2.5  2.6  2.9  3.2 
peak mem/proc [GB]  13.0  4.1  1.9  2.2 
closing holes with full patches  
num processes  4  4  6  6 
real runtime [h]  12.1  7.0  4.3  5.1 
runtime/40 proc [h]  1.2  0.7  0.6  0.8 
peak mem/proc [GB]  14.8  6.5  2.4  1.8 
hole filling with graph cut  
num processes  4  4  6  6 
real runtime [h]  31  18  6  5 
runtime/40 proc [h]  0.8  0.5  0.2  0.1 
peak mem/proc [GB]  25.3  8.9  3.1  1.8 
overall  
runtime/40 proc [h]  35.6  27.8  18.5  13.7 
peak mem/proc [GB]  25.3  8.9  3.1  2.2 
Approach  Param.  Accuracy  Completeness  

Factor  Mean  Median  Variance  Mean  Median  Variance  
FSSR  1  0.673  0.396  0.685  0.430  0.239  1.638 
2  0.833  0.403  1.213  0.474  0.285  1.630  
4  0.878  0.338  1.698  0.490  0.289  1.625  
GDMR  0.5  1.048  0.269  4.846  0.460  0.290  0.716 
1  1.013  0.275  4.262  0.423  0.284  0.587  
2  1.021  0.287  4.015  0.410  0.278  0.496  
4  1.008  0.304  3.539  0.407  0.270  0.524  
8  0.971  0.332  2.772  0.399  0.260  0.564  
OURS    0.671  0.262  1.330  0.423  0.279  0.575 
Approach  Param.  Accuracy  Completeness  

Factor  Mean  Median  Variance  Mean  Median  Variance  
FSSR  1  1.044  0.490  2.487  0.431  0.257  1.218 
2  1.594  0.523  5.935  0.501  0.353  0.985  
4  1.975  0.496  9.503  0.485  0.370  0.450  
8  2.395  0.520  14.259  0.520  0.387  0.462  
GDMR  0.5  1.101  0.295  4.931  0.565  0.373  0.917 
1  1.099  0.301  4.693  0.519  0.357  0.744  
2  1.163  0.322  4.813  0.494  0.339  0.753  
4  1.358  0.373  5.687  0.465  0.317  0.703  
OURS    1.247  0.365  5.013  0.509  0.368  0.512 
Approach  Param.  Accuracy  Completeness  

Factor  Mean  Median  Variance  Mean  Median  Variance  
FSSR  2  0.332  0.245  0.079  1.110  0.476  4.867 
4  0.491  0.318  0.273  0.624  0.395  1.772  
8  0.593  0.327  0.551  0.764  0.413  3.126  
GDMR  1  1.651  0.456  9.159  1.280  0.621  3.785 
2  1.372  0.373  6.855  0.789  0.468  1.510  
4  1.149  0.343  4.991  0.581  0.404  0.735  
8  0.996  0.355  3.024  0.537  0.389  0.613  
16  0.988  0.377  2.697  0.529  0.381  0.615  
32  1.003  0.402  2.586  0.518  0.368  0.633  
OURS    0.626  0.341  0.755  0.567  0.390  0.743 
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