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  license: apache-2.0
 
 
 
 
 
 
 
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  ---
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
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  ---
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  license: apache-2.0
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+ tags:
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+ - '- spacecraft'
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+ - '- obstacle-avoidance'
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+ - '- world-models'
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+ - '- isaac-sim'
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+ - '- trajectory-prediction'
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+ pretty_name: Orbit-Planner Orbital Evasion Dataset
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  ---
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+ ---
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+ pretty_name: Orbit-Planner Orbital Evasion Dataset
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+ task_categories:
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+ - robotics
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+ - reinforcement-learning
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+ tags:
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+ - spacecraft
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+ - obstacle-avoidance
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+ - world-models
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+ - multimodal
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+ - trajectory-prediction
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+ - isaac-sim
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+ - hdf5
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+ ---
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+
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+ # Orbit-Planner Orbital Evasion Dataset
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+
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+ <p align="center">
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+ <a href="https://arxiv.org/abs/0000.00000"><img src="https://img.shields.io/badge/arXiv-Paper-B31B1B?logo=arxiv&logoColor=white" alt="ArXiv Paper"></a>
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+ <a href="https://github.com/ZhijianLi2003/Orbit_Planner"><img src="https://img.shields.io/badge/GitHub-Code-181717?logo=github&logoColor=white" alt="GitHub Code"></a>
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+ <a href="https://zhijianli2003.github.io/Orbit_Planner/"><img src="https://img.shields.io/badge/Project-Page-0A7EA4?logo=googlechrome&logoColor=white" alt="Project Page"></a>
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+ </p>
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+
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+ Orbit-Planner is a simulated multimodal trajectory dataset for vision-based
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+ spacecraft navigation and obstacle avoidance. It contains synchronized
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+ first-person RGB images, depth maps, spacecraft states, thruster commands, and
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+ event labels collected in the Orbital Evasion task from Space Robotics Bench
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+ and NVIDIA Isaac Sim.
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+
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+ The dataset is intended for learning latent world models, spacecraft dynamics,
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+ visual representations, imitation policies, and collision-aware planning. Its
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+ trajectories cover successful obstacle avoidance, direct high-risk flight, and
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+ open-loop exploration, providing both task-oriented behavior and diverse
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+ spacecraft dynamics.
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+
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+ ## Dataset at a Glance
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+
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+ | Property | Value |
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+ | --- | ---: |
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+ | Number of trajectories | 8,000 |
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+ | Total time steps | 2,114,895 |
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+ | Time between consecutive frames | 0.04 s (25 Hz) |
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+ | Average steps per trajectory | 264.36 |
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+ | Trajectories with success events | 3,437 |
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+ | Trajectories with collision events | 1,530 |
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+ | State dimension | 16 |
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+ | Action dimension | 8 |
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+ | Event dimension | 2 |
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+ | RGB resolution | 224 x 224 x 3 |
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+ | Depth resolution | 224 x 224 |
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+
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+ The dataset contains the following collection strategies:
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+
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+ | Strategy | Trajectories | Description |
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+ | --- | ---: | --- |
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+ | `expert` | 5,601 | RRT* obstacle-avoiding path planning followed by path smoothing and PD tracking. |
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+ | `risky` | 1,578 | Direct flight toward the target without obstacle-avoiding path planning. |
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+ | `explore` | 821 | Segmented near-open-loop force, torque, combined-control, and coasting behavior. |
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+
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+ ## Data Generation
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+
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+ Each episode starts with the spacecraft at the local origin with identity
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+ orientation and zero velocity. The target and 14 obstacles are randomized for
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+ each trajectory. In the released configuration, obstacles are placed around
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+ the start-to-target corridor and may drift during an episode. The onboard
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+ camera follows the spacecraft attitude and looks along the body-frame `-Z`
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+ axis.
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+
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+ Expert trajectories use RRT* with a 1.2 m planning clearance, shortcut-based
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+ path smoothing, waypoint resampling, and closed-loop PD path tracking. Risky
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+ trajectories fly directly toward the target. Exploration trajectories use
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+ near-open-loop control segments to increase translational and rotational
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+ dynamics diversity.
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+
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+ The maximum episode length is 300 steps. A successful episode passes the
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+ target's z-plane while remaining within the configured lateral tolerance.
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+ Collision detection uses an impulse-based proxy: a collision is marked when
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+ the magnitude of the step-to-step change in world-frame linear velocity,
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+ `||v_t - v_{t-1}||`, exceeds 0.5 m/s. After the first detected collision,
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+ collection continues for 30 additional closed-loop steps so that post-impact
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+ dynamics are retained.
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+
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+ ## Data Structure
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+
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+ The HDF5 data are organized as one group per trajectory:
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+
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+ ```text
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+ dataset.h5
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+ +-- traj_0000/
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+ | +-- states [T, 16] float64
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+ | +-- actions [T, 8] float32
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+ | +-- events [T, 2] float32
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+ | +-- rgb [T, 224, 224, 3] uint8
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+ | +-- depth [T, 224, 224] uint8
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+ +-- traj_0001/
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+ | +-- ...
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+ +-- ...
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+ ```
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+
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+ All arrays are gzip-compressed in the HDF5 file. The accompanying
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+ [`meta.json`](./meta.json) contains the full dataset configuration, feature
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+ definitions, aggregate statistics, and a trajectory-level index.
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+
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+ ### State
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+
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+ The state vector is
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+
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+ ```text
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+ s_t = [p_t, v_t, rot6d_t, omega_t, phi_t]
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+ ```
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+
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+ | Slice | Size | Description |
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+ | --- | ---: | --- |
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+ | `p_t` (`0:3`) | 3 | Spacecraft displacement from its initial position in the world frame. |
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+ | `v_t` (`3:6`) | 3 | Linear velocity in the body frame. |
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+ | `rot6d_t` (`6:12`) | 6 | First two columns of the rotation matrix. |
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+ | `omega_t` (`12:15`) | 3 | Angular velocity in the body frame. |
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+ | `phi_t` (`15:16`) | 1 | Remaining fuel fraction in `[0, 1]`. |
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+
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+ ### Action
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+
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+ The action vector contains normalized commands for eight spacecraft thrusters:
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+
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+ ```text
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+ a_t = [F1, F2, ..., F8], a_t in [0, 1]^8
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+ ```
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+
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+ ### Events
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+
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+ The event vector is
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+
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+ ```text
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+ e_t = [collision, success]
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+ ```
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+
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+ `collision` is the event label intended for downstream use and marks steps
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+ where the velocity-based impulse proxy exceeds its configured threshold.
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+ `success` is retained only as a collection-time bookkeeping field and is not
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+ used by the current training or evaluation pipeline, so it can be ignored.
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+ Event values are binary and stored as `float32`.
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+
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+ ### Visual Observations
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+
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+ Each step includes a first-person `uint8` RGB frame and a grayscale `uint8`
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+ depth frame. Depth values use an inverted encoding in which larger values are
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+ nearer. Convert a stored depth value `d` to meters with:
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+
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+ ```text
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+ depth_m = ((255 - d) / 255.0) * 50.0 + 0.1
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+ ```
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+
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+ The valid clipping range is 0.1 m to 50.1 m, and background space is encoded as
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+ zero.
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+
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+ ### Trajectory Metadata
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+
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+ Each trajectory has an identifier and summary attributes including
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+ `total_steps`, `has_collision`, `has_success`, `terminated`, `truncated`,
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+ `target_pos`, `strategy`, and `collision_step`. A `collision_step` value of
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+ `-1` means that no collision was detected; otherwise, it identifies the first
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+ collision frame.
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+
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+ ## Intended Uses
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+
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+ This dataset is suitable for:
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+
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+ - multimodal and latent spacecraft world models;
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+ - visual dynamics and future-state prediction;
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+ - imitation learning and offline reinforcement learning;
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+ - obstacle-avoidance planning and control;
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+ - collision prediction and post-impact dynamics modeling;
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+ - benchmarking state, depth, and action representation learning.
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+
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+ Trajectory-level splits should be used to prevent adjacent frames from the same
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+ episode from appearing in both training and evaluation sets.
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+
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+ ## Limitations
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+
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+ The data are generated entirely in simulation and do not capture every source
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+ of real spacecraft sensor noise, actuator uncertainty, illumination variation,
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+ or contact dynamics. Behavior comes from scripted expert, risky, and exploration
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+ controllers rather than human demonstrations. Collision labels are based on a
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+ velocity-change threshold, so they should not be treated as direct contact
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+ sensor measurements. The strategy and outcome distributions are also
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+ imbalanced and should be considered when constructing evaluation splits.