feat: improve visualization notebook #167
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WalkthroughThe pull request introduces modifications to two Jupyter notebooks in the Astrodynamics Flight Dynamics directory. In the Access Computation notebook, a new variable Changes
Sequence DiagramsequenceDiagram
participant Notebook as Access Computation
participant DataProcessor as Data Processing
Notebook->>DataProcessor: Create first_target_accesses
Notebook->>DataProcessor: Create second_target_accesses
Notebook->>DataProcessor: Concatenate into all_accesses
DataProcessor-->>Notebook: Process combined accesses
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Actionable comments posted: 0
🧹 Nitpick comments (3)
notebooks/Astrodynamics/Flight Dynamics/Access Computation.ipynb (1)
416-416: Consider memory-efficient alternatives for large datasets.While using
+for list concatenation works, consider usingitertools.chain()for memory efficiency with large datasets:-all_accesses = first_target_accesses + second_target_accesses +from itertools import chain +all_accesses = list(chain(first_target_accesses, second_target_accesses))Or if modifying in-place is acceptable:
-all_accesses = first_target_accesses + second_target_accesses +all_accesses = first_target_accesses.copy() +all_accesses.extend(second_target_accesses)notebooks/Astrodynamics/Flight Dynamics/Visualize Satellite Trajectory (Cesium).ipynb (2)
114-119: Add error handling for Cesium token retrieval.The Cesium token is essential for visualization. Consider adding error handling to provide a better user experience when the token is missing.
- cesium_token=os.environ.get("CESIUM_TOKEN"), # Get a token from https://cesium.com/learn/ion/cesium-ion-access-tokens/ + cesium_token=os.environ.get("CESIUM_TOKEN") or ( + raise ValueError("CESIUM_TOKEN environment variable is required. Get a token from https://cesium.com/learn/ion/cesium-ion-access-tokens/") + ),
142-144: Consider adding validation for orbital frame type.While the VVLH frame type is appropriate, consider adding validation to ensure only supported frame types are used.
+ if orbital_frame_type not in Orbit.FrameType: + raise ValueError(f"Unsupported orbital frame type: {orbital_frame_type}") profile = Profile.local_orbital_frame_pointing( orbit=orbit, orbital_frame_type=Orbit.FrameType.VVLH, )
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📒 Files selected for processing (2)
notebooks/Astrodynamics/Flight Dynamics/Access Computation.ipynb(2 hunks)notebooks/Astrodynamics/Flight Dynamics/Visualize Satellite Trajectory (Cesium).ipynb(1 hunks)
🔇 Additional comments (3)
notebooks/Astrodynamics/Flight Dynamics/Access Computation.ipynb (1)
930-930: LGTM!The list comprehension using the combined
all_accesseslist simplifies the code structure while maintaining the same functionality.notebooks/Astrodynamics/Flight Dynamics/Visualize Satellite Trajectory (Cesium).ipynb (2)
101-104: LGTM! Well-defined time interval.The interval definition is clear and appropriate for visualization purposes.
127-133: LGTM! Helpful documentation.The markdown provides clear context for advanced visualization capabilities.
Summary by CodeRabbit
Release Notes
New Features
Improvements