Update README.md
Browse files
README.md
CHANGED
|
@@ -1,3 +1,195 @@
|
|
| 1 |
---
|
| 2 |
license: apache-2.0
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
| 3 |
---
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
| 1 |
---
|
| 2 |
license: apache-2.0
|
| 3 |
+
tags:
|
| 4 |
+
- '- spacecraft'
|
| 5 |
+
- '- obstacle-avoidance'
|
| 6 |
+
- '- world-models'
|
| 7 |
+
- '- isaac-sim'
|
| 8 |
+
- '- trajectory-prediction'
|
| 9 |
+
pretty_name: Orbit-Planner Orbital Evasion Dataset
|
| 10 |
---
|
| 11 |
+
---
|
| 12 |
+
pretty_name: Orbit-Planner Orbital Evasion Dataset
|
| 13 |
+
task_categories:
|
| 14 |
+
- robotics
|
| 15 |
+
- reinforcement-learning
|
| 16 |
+
tags:
|
| 17 |
+
- spacecraft
|
| 18 |
+
- obstacle-avoidance
|
| 19 |
+
- world-models
|
| 20 |
+
- multimodal
|
| 21 |
+
- trajectory-prediction
|
| 22 |
+
- isaac-sim
|
| 23 |
+
- hdf5
|
| 24 |
+
---
|
| 25 |
+
|
| 26 |
+
# Orbit-Planner Orbital Evasion Dataset
|
| 27 |
+
|
| 28 |
+
<p align="center">
|
| 29 |
+
<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>
|
| 30 |
+
<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>
|
| 31 |
+
<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>
|
| 32 |
+
</p>
|
| 33 |
+
|
| 34 |
+
Orbit-Planner is a simulated multimodal trajectory dataset for vision-based
|
| 35 |
+
spacecraft navigation and obstacle avoidance. It contains synchronized
|
| 36 |
+
first-person RGB images, depth maps, spacecraft states, thruster commands, and
|
| 37 |
+
event labels collected in the Orbital Evasion task from Space Robotics Bench
|
| 38 |
+
and NVIDIA Isaac Sim.
|
| 39 |
+
|
| 40 |
+
The dataset is intended for learning latent world models, spacecraft dynamics,
|
| 41 |
+
visual representations, imitation policies, and collision-aware planning. Its
|
| 42 |
+
trajectories cover successful obstacle avoidance, direct high-risk flight, and
|
| 43 |
+
open-loop exploration, providing both task-oriented behavior and diverse
|
| 44 |
+
spacecraft dynamics.
|
| 45 |
+
|
| 46 |
+
## Dataset at a Glance
|
| 47 |
+
|
| 48 |
+
| Property | Value |
|
| 49 |
+
| --- | ---: |
|
| 50 |
+
| Number of trajectories | 8,000 |
|
| 51 |
+
| Total time steps | 2,114,895 |
|
| 52 |
+
| Time between consecutive frames | 0.04 s (25 Hz) |
|
| 53 |
+
| Average steps per trajectory | 264.36 |
|
| 54 |
+
| Trajectories with success events | 3,437 |
|
| 55 |
+
| Trajectories with collision events | 1,530 |
|
| 56 |
+
| State dimension | 16 |
|
| 57 |
+
| Action dimension | 8 |
|
| 58 |
+
| Event dimension | 2 |
|
| 59 |
+
| RGB resolution | 224 x 224 x 3 |
|
| 60 |
+
| Depth resolution | 224 x 224 |
|
| 61 |
+
|
| 62 |
+
The dataset contains the following collection strategies:
|
| 63 |
+
|
| 64 |
+
| Strategy | Trajectories | Description |
|
| 65 |
+
| --- | ---: | --- |
|
| 66 |
+
| `expert` | 5,601 | RRT* obstacle-avoiding path planning followed by path smoothing and PD tracking. |
|
| 67 |
+
| `risky` | 1,578 | Direct flight toward the target without obstacle-avoiding path planning. |
|
| 68 |
+
| `explore` | 821 | Segmented near-open-loop force, torque, combined-control, and coasting behavior. |
|
| 69 |
+
|
| 70 |
+
## Data Generation
|
| 71 |
+
|
| 72 |
+
Each episode starts with the spacecraft at the local origin with identity
|
| 73 |
+
orientation and zero velocity. The target and 14 obstacles are randomized for
|
| 74 |
+
each trajectory. In the released configuration, obstacles are placed around
|
| 75 |
+
the start-to-target corridor and may drift during an episode. The onboard
|
| 76 |
+
camera follows the spacecraft attitude and looks along the body-frame `-Z`
|
| 77 |
+
axis.
|
| 78 |
+
|
| 79 |
+
Expert trajectories use RRT* with a 1.2 m planning clearance, shortcut-based
|
| 80 |
+
path smoothing, waypoint resampling, and closed-loop PD path tracking. Risky
|
| 81 |
+
trajectories fly directly toward the target. Exploration trajectories use
|
| 82 |
+
near-open-loop control segments to increase translational and rotational
|
| 83 |
+
dynamics diversity.
|
| 84 |
+
|
| 85 |
+
The maximum episode length is 300 steps. A successful episode passes the
|
| 86 |
+
target's z-plane while remaining within the configured lateral tolerance.
|
| 87 |
+
Collision detection uses an impulse-based proxy: a collision is marked when
|
| 88 |
+
the magnitude of the step-to-step change in world-frame linear velocity,
|
| 89 |
+
`||v_t - v_{t-1}||`, exceeds 0.5 m/s. After the first detected collision,
|
| 90 |
+
collection continues for 30 additional closed-loop steps so that post-impact
|
| 91 |
+
dynamics are retained.
|
| 92 |
+
|
| 93 |
+
## Data Structure
|
| 94 |
+
|
| 95 |
+
The HDF5 data are organized as one group per trajectory:
|
| 96 |
+
|
| 97 |
+
```text
|
| 98 |
+
dataset.h5
|
| 99 |
+
+-- traj_0000/
|
| 100 |
+
| +-- states [T, 16] float64
|
| 101 |
+
| +-- actions [T, 8] float32
|
| 102 |
+
| +-- events [T, 2] float32
|
| 103 |
+
| +-- rgb [T, 224, 224, 3] uint8
|
| 104 |
+
| +-- depth [T, 224, 224] uint8
|
| 105 |
+
+-- traj_0001/
|
| 106 |
+
| +-- ...
|
| 107 |
+
+-- ...
|
| 108 |
+
```
|
| 109 |
+
|
| 110 |
+
All arrays are gzip-compressed in the HDF5 file. The accompanying
|
| 111 |
+
[`meta.json`](./meta.json) contains the full dataset configuration, feature
|
| 112 |
+
definitions, aggregate statistics, and a trajectory-level index.
|
| 113 |
+
|
| 114 |
+
### State
|
| 115 |
+
|
| 116 |
+
The state vector is
|
| 117 |
+
|
| 118 |
+
```text
|
| 119 |
+
s_t = [p_t, v_t, rot6d_t, omega_t, phi_t]
|
| 120 |
+
```
|
| 121 |
+
|
| 122 |
+
| Slice | Size | Description |
|
| 123 |
+
| --- | ---: | --- |
|
| 124 |
+
| `p_t` (`0:3`) | 3 | Spacecraft displacement from its initial position in the world frame. |
|
| 125 |
+
| `v_t` (`3:6`) | 3 | Linear velocity in the body frame. |
|
| 126 |
+
| `rot6d_t` (`6:12`) | 6 | First two columns of the rotation matrix. |
|
| 127 |
+
| `omega_t` (`12:15`) | 3 | Angular velocity in the body frame. |
|
| 128 |
+
| `phi_t` (`15:16`) | 1 | Remaining fuel fraction in `[0, 1]`. |
|
| 129 |
+
|
| 130 |
+
### Action
|
| 131 |
+
|
| 132 |
+
The action vector contains normalized commands for eight spacecraft thrusters:
|
| 133 |
+
|
| 134 |
+
```text
|
| 135 |
+
a_t = [F1, F2, ..., F8], a_t in [0, 1]^8
|
| 136 |
+
```
|
| 137 |
+
|
| 138 |
+
### Events
|
| 139 |
+
|
| 140 |
+
The event vector is
|
| 141 |
+
|
| 142 |
+
```text
|
| 143 |
+
e_t = [collision, success]
|
| 144 |
+
```
|
| 145 |
+
|
| 146 |
+
`collision` is the event label intended for downstream use and marks steps
|
| 147 |
+
where the velocity-based impulse proxy exceeds its configured threshold.
|
| 148 |
+
`success` is retained only as a collection-time bookkeeping field and is not
|
| 149 |
+
used by the current training or evaluation pipeline, so it can be ignored.
|
| 150 |
+
Event values are binary and stored as `float32`.
|
| 151 |
+
|
| 152 |
+
### Visual Observations
|
| 153 |
+
|
| 154 |
+
Each step includes a first-person `uint8` RGB frame and a grayscale `uint8`
|
| 155 |
+
depth frame. Depth values use an inverted encoding in which larger values are
|
| 156 |
+
nearer. Convert a stored depth value `d` to meters with:
|
| 157 |
+
|
| 158 |
+
```text
|
| 159 |
+
depth_m = ((255 - d) / 255.0) * 50.0 + 0.1
|
| 160 |
+
```
|
| 161 |
+
|
| 162 |
+
The valid clipping range is 0.1 m to 50.1 m, and background space is encoded as
|
| 163 |
+
zero.
|
| 164 |
+
|
| 165 |
+
### Trajectory Metadata
|
| 166 |
+
|
| 167 |
+
Each trajectory has an identifier and summary attributes including
|
| 168 |
+
`total_steps`, `has_collision`, `has_success`, `terminated`, `truncated`,
|
| 169 |
+
`target_pos`, `strategy`, and `collision_step`. A `collision_step` value of
|
| 170 |
+
`-1` means that no collision was detected; otherwise, it identifies the first
|
| 171 |
+
collision frame.
|
| 172 |
+
|
| 173 |
+
## Intended Uses
|
| 174 |
+
|
| 175 |
+
This dataset is suitable for:
|
| 176 |
+
|
| 177 |
+
- multimodal and latent spacecraft world models;
|
| 178 |
+
- visual dynamics and future-state prediction;
|
| 179 |
+
- imitation learning and offline reinforcement learning;
|
| 180 |
+
- obstacle-avoidance planning and control;
|
| 181 |
+
- collision prediction and post-impact dynamics modeling;
|
| 182 |
+
- benchmarking state, depth, and action representation learning.
|
| 183 |
+
|
| 184 |
+
Trajectory-level splits should be used to prevent adjacent frames from the same
|
| 185 |
+
episode from appearing in both training and evaluation sets.
|
| 186 |
+
|
| 187 |
+
## Limitations
|
| 188 |
+
|
| 189 |
+
The data are generated entirely in simulation and do not capture every source
|
| 190 |
+
of real spacecraft sensor noise, actuator uncertainty, illumination variation,
|
| 191 |
+
or contact dynamics. Behavior comes from scripted expert, risky, and exploration
|
| 192 |
+
controllers rather than human demonstrations. Collision labels are based on a
|
| 193 |
+
velocity-change threshold, so they should not be treated as direct contact
|
| 194 |
+
sensor measurements. The strategy and outcome distributions are also
|
| 195 |
+
imbalanced and should be considered when constructing evaluation splits.
|