Qvelard commited on
Commit
6aaeebd
·
verified ·
1 Parent(s): fada988

Update README.md

Browse files
Files changed (1) hide show
  1. README.md +6 -6
README.md CHANGED
@@ -43,7 +43,7 @@ of the [ledrone](https://github.com/ahive-org/ledrone) project.
43
 
44
  | | |
45
  |---|---|
46
- | Task | `takeoff` climb from the ground and hold a target altitude |
47
  | Type | Goal-conditioned, **state-based** (FPV image is an optional auxiliary) |
48
  | Episodes | 300 |
49
  | Frames | 60,000 (200/episode, 6.7s at 30 Hz) |
@@ -61,7 +61,7 @@ flies the `takeoff` reference in the `LeDrone` env on the **PyBullet** backend.
61
 
62
  - **DART-style coverage** ([Laskey et al. 2017](https://arxiv.org/abs/1703.09327)): the
63
  drone is driven by a *noised* command (σ = 0.15 m/s on the velocity channels) but each
64
- frame is **labelled with the clean expert command** so the policy sees
65
  off-distribution states *and* the optimal correction for them, mitigating
66
  behavior-cloning covariate shift.
67
  - **Slew-rate-limited setpoint** ramps the command from rest, taming the low-level
@@ -89,7 +89,7 @@ python tools/generate_expert_dataset.py --task takeoff --backend pybullet \
89
 
90
  State is the SOTA quadrotor policy observation (relative goal + velocity + orientation +
91
  body rates); **battery is intentionally excluded** (handled by domain randomization, not
92
- observed Hwangbo 2017, Molchanov 2019, Kaufmann ICRA 2022 / Nature 2023). Attitude is
93
  a unit quaternion; map to a continuous 6D rep
94
  ([Zhou et al., CVPR 2019](https://arxiv.org/abs/1812.07035)) if desired. `action` is a
95
  NED velocity + yaw rate clipped to the envelope (≤ 2 m/s horizontal, ≤ 1 m/s climb,
@@ -121,15 +121,15 @@ frame = ds[0] # observation.state (13,), observation.environment_state (3,), ac
121
 
122
  Analysis across all three `ledrone` tasks, computed from this DART-regenerated data.
123
 
124
- **Signature trajectories** takeoff climbs from the ground, hover converges & station-keeps, circle flies full loops (>= 360 deg).
125
 
126
  ![Trajectories](figures/trajectories.png)
127
 
128
- **Convergence & attitude** every task drives the goal error to near-zero (circle keeps a small steady tracking lag from following a moving target); body tilt stays gentle (median ~10 deg, 95% <= 35 deg).
129
 
130
  ![Convergence and attitude](figures/convergence_attitude.png)
131
 
132
- **Command / action space** takeoff & hover station-keep at ~0.1 m/s while circle orbits at ~1.3 m/s; the climb command is bimodal for takeoff; yaw-rate is centered on the goal bearing.
133
 
134
  ![Action space](figures/action_space.png)
135
 
 
43
 
44
  | | |
45
  |---|---|
46
+ | Task | `takeoff` : climb from the ground and hold a target altitude |
47
  | Type | Goal-conditioned, **state-based** (FPV image is an optional auxiliary) |
48
  | Episodes | 300 |
49
  | Frames | 60,000 (200/episode, 6.7s at 30 Hz) |
 
61
 
62
  - **DART-style coverage** ([Laskey et al. 2017](https://arxiv.org/abs/1703.09327)): the
63
  drone is driven by a *noised* command (σ = 0.15 m/s on the velocity channels) but each
64
+ frame is **labelled with the clean expert command** : so the policy sees
65
  off-distribution states *and* the optimal correction for them, mitigating
66
  behavior-cloning covariate shift.
67
  - **Slew-rate-limited setpoint** ramps the command from rest, taming the low-level
 
89
 
90
  State is the SOTA quadrotor policy observation (relative goal + velocity + orientation +
91
  body rates); **battery is intentionally excluded** (handled by domain randomization, not
92
+ observed : Hwangbo 2017, Molchanov 2019, Kaufmann ICRA 2022 / Nature 2023). Attitude is
93
  a unit quaternion; map to a continuous 6D rep
94
  ([Zhou et al., CVPR 2019](https://arxiv.org/abs/1812.07035)) if desired. `action` is a
95
  NED velocity + yaw rate clipped to the envelope (≤ 2 m/s horizontal, ≤ 1 m/s climb,
 
121
 
122
  Analysis across all three `ledrone` tasks, computed from this DART-regenerated data.
123
 
124
+ **Signature trajectories** : takeoff climbs from the ground, hover converges & station-keeps, circle flies full loops (>= 360 deg).
125
 
126
  ![Trajectories](figures/trajectories.png)
127
 
128
+ **Convergence & attitude** : every task drives the goal error to near-zero (circle keeps a small steady tracking lag from following a moving target); body tilt stays gentle (median ~10 deg, 95% <= 35 deg).
129
 
130
  ![Convergence and attitude](figures/convergence_attitude.png)
131
 
132
+ **Command / action space** : takeoff & hover station-keep at ~0.1 m/s while circle orbits at ~1.3 m/s; the climb command is bimodal for takeoff; yaw-rate is centered on the goal bearing.
133
 
134
  ![Action space](figures/action_space.png)
135