--- license: cc-by-nc-sa-4.0 pretty_name: SPARK-2021 (SPAcecraft Recognition leveraging Knowledge of space environment) language: - en size_categories: - 100K.rgb.jpg # RGB image .depth.png # 16-bit depth map, same geometry as the RGB frame .json # {"label": 3, "class": "Calipso", "bbox": [R_min, C_min, R_max, C_max]} ``` ### Splits | Split | Samples | Notes | |---|---|---| | `train` | _TODO_ | Public training split of the SPARK 2021 challenge | | `validation` | _TODO_ | Public validation split (labels released) | | `test` | not included | Challenge test labels were kept private | Class composition of the full release: **12,500 images per satellite class** (10 classes) and **5,000 images per debris object** across 5 debris models, all merged into a single `Debris` class (25,000 images) — 150,000 images in total per modality. ### Classes | Index | Class | Type | |---|---|---| | 0 | AcrimSat | Satellite | | 1 | Aquarius | Satellite | | 2 | Aura | Satellite | | 3 | Calipso | Satellite | | 4 | Cloudsat | Satellite | | 5 | CubeSat | Satellite (1RU generic CubeSat) | | 6 | Debris | Debris (5 models merged) | | 7 | Jason | Satellite | | 8 | Sentinel-6 | Satellite | | 9 | Terra | Satellite | | 10 | TRMM | Satellite | Satellite models come from [NASA 3D Resources](https://nasa3d.arc.nasa.gov/). Debris objects are corrupted-texture parts of satellites and rockets: space shuttle external tank, orbital docking system, damaged communication dish, thermal protection tiles, and connector ring. ### ⚠️ Bounding-box convention Boxes follow the **original SPARK convention**, which is *row/column ordered*, not the usual `x, y` ordering: ``` bbox = [R_min, C_min, R_max, C_max] # == [y_min, x_min, y_max, x_max] ``` Conversions: ```python r_min, c_min, r_max, c_max = bbox # Pascal VOC / torchvision (x1, y1, x2, y2) voc = [c_min, r_min, c_max, r_max] # COCO (x, y, w, h) coco = [c_min, r_min, c_max - c_min, r_max - r_min] # YOLO (normalised cx, cy, w, h) for an image of size (H, W) yolo = [((c_min + c_max) / 2) / W, ((r_min + r_max) / 2) / H, (c_max - c_min) / W, (r_max - r_min) / H] ``` --- ## Usage ```python from datasets import load_dataset ds = load_dataset("/spark-2021", split="train") sample = ds[0] sample["rgb"] # PIL.Image, RGB sample["depth"] # PIL.Image, 16-bit single channel sample["label"] # int in [0, 10] sample["bbox"] # [R_min, C_min, R_max, C_max] ``` ### Streaming (recommended — the full dataset is large) ```python ds = load_dataset("/spark-2021", split="train", streaming=True) for sample in ds.take(8): print(sample["label"], sample["bbox"], sample["rgb"].size) ``` ### RGB-only classification ```python ds = load_dataset("/spark-2021", split="train").remove_columns("depth") ``` ### Depth handling Depth maps are stored as 16-bit PNGs. Convert to a float array before use: ```python import numpy as np depth = np.asarray(sample["depth"], dtype=np.float32) # raw sensor units ``` Note that the released depth maps are known to be noisy and to contain holes; several challenge entries applied morphological opening / hole filling before using them. --- ## Dataset creation SPARK was rendered in **Unity3D**, with: - **Earth model** — high-resolution textured 16k-polygon model based on the NASA Blue Marble collection, including clouds, cloud shadows, and atmospheric outer scattering. - **Background** — high-resolution ESO panorama of the Milky Way. - **Target** — one of the 10 satellite models or 5 debris models, randomly placed inside the camera field of view, in LEO. - **Chaser** — observer platform carrying a pinhole RGB camera with known intrinsics plus a depth camera. The Sun and the Earth are randomly rotated about their axes in every frame. The dataset is deliberately spanned along four axes of variation: 1. **Scene illumination** — including extreme cases where sunlight directly faces the sensor or reflects off the target/Earth, producing lens flare and sensor blooming. 2. **Scene background** — Earth-in-background (rich texture, ocean/cloud specularity) vs. deep space (featureless, sparse stars). 3. **Range** — varying camera-to-target distance, i.e. varying target occupation of the frame. 4. **Sensor noise** — zero-mean white Gaussian noise at varying levels, emulating the high dynamic range and small-sensor noise of spaceborne imagers. The baseline study in the SPARK paper found accuracy degrading systematically with lower illumination, longer range, and increasing noise, with the **far-range + low-illumination** subset being the hardest regime. Fine-tuning ImageNet-pretrained backbones outperformed both random initialisation and frozen feature extraction, and RGB-D fusion reached 90.05% validation accuracy versus 75% (RGB only) and 88.01% (depth only) at 64×64 input resolution. --- ## Original challenge protocol The ICIP 2021 competition defined two tasks and two dedicated metrics. **Task 1 — Classification.** Errors were weighted by severity: misclassifying a satellite as another satellite (level 1/4), a satellite as debris (level 2/4), and — most severely — debris as a satellite (level 4/4). Ranking used an F2-score-based metric combined with the proportion of correctly classified non-debris samples. **Task 2 — Detection.** Inspired by the COCO protocol: the proportion of images with both a correct class prediction and an IoU above threshold, averaged over several IoU thresholds. These metrics are documented here for reproducibility; this repository does not host an evaluation server. --- ## Intended uses - Spacecraft and debris **classification** and **detection** under space imaging conditions - **Multi-modal RGB-D** fusion research - **Robustness studies** with respect to illumination, range, and sensor noise - Pretraining / representation learning for downstream proximity-operations perception ### Out of scope and limitations - **Fully synthetic.** Models trained on SPARK alone will exhibit a substantial sim-to-real domain gap and should not be treated as flight-qualified without hardware-in-the-loop or on-orbit validation. - **Renderer artefacts.** Illumination, flare, and noise are approximations of the true space radiometric environment; depth maps are simulated, not from a flight-representative sensor. - **Class imbalance.** The single `Debris` class aggregates five geometrically distinct objects. - **No pose labels.** SPARK provides class and bounding box only. For 6-DoF pose, see SPEED / SPEED+ or URSO. --- ## Citation If you use SPARK, please cite both the dataset paper and the challenge paper: ```bibtex @inproceedings{musallam2021sparkchallenge, title = {Spacecraft Recognition Leveraging Knowledge of Space Environment: Simulator, Dataset, Competition Design and Analysis}, author = {Musallam, Mohamed Adel and Gaudilli{\`e}re, Vincent and Ghorbel, Enjie and Al Ismaeil, Kassem and Perez, Marcos Damian and Poucet, Michel and Aouada, Djamila}, booktitle = {IEEE International Conference on Image Processing Challenges (ICIPC)}, pages = {11--15}, year = {2021}, doi = {10.1109/ICIPC53495.2021.9620184} } ``` ## Acknowledgements Dataset produced by the Computer Vision, Imaging & Machine Intelligence (CVI²) research group, Interdisciplinary Centre for Security, Reliability and Trust (SnT), University of Luxembourg, in collaboration with LMO. ## Contact Project page: Issues with this Hugging Face mirror: open a discussion on this repository.