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Refactor documentation to replace the Validation Harness with a separate E2E Test Suite, updating references throughout various documents. Adjust the autodev state to reflect the transition from the Decompose phase to the Implement phase, and revise the architecture documentation to clarify system boundaries and component relationships. Enhance risk mitigation documentation to specify affected components and update the component overview diagram accordingly.

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Oleksandr Bezdieniezhnykh
2026-05-03 11:50:39 +03:00
parent 5bf2dbd85f
commit dd9afe2797
31 changed files with 1479 additions and 396 deletions
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_docs/02_document/risk_mitigations.md
+4 -4
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@@ -55,7 +55,7 @@
**Trigger conditions**: Manufacturer documentation or hardware testing contradicts assumed FPS, interface, temperature, or lens characteristics.
**Affected components**: Camera ingest/calibration, BASALT VIO adapter, validation harness, deployment procedures.
**Affected components**: Camera ingest/calibration, BASALT VIO adapter, separate e2e test suite, deployment procedures.
**Mitigation strategy**:
1. Make camera specification verification a bootstrap task.
@@ -76,7 +76,7 @@
**Trigger conditions**: Public or representative replay shows high drift, frequent tracking loss, or poor initialization.
**Affected components**: BASALT VIO adapter, safety/anchor wrapper, validation harness.
**Affected components**: BASALT VIO adapter, safety/anchor wrapper, separate e2e test suite.
**Mitigation strategy**:
1. Run MUN-FRL first for synchronized nadir camera + IMU + ground truth.
@@ -160,7 +160,7 @@
**Trigger conditions**: Relocalization exceeds p95 latency, memory budget, or causes thermal throttling.
**Affected components**: Satellite Service, anchor verification, validation harness.
**Affected components**: Satellite Service, anchor verification, separate e2e test suite.
**Mitigation strategy**:
1. Keep VPR/local matching trigger-based.
@@ -244,7 +244,7 @@
**Trigger conditions**: Plane SITL rejects or mishandles emitted `GPS_INPUT`, or QGC status is insufficient.
**Affected components**: MAVLink/GCS integration, safety/anchor wrapper, validation harness.
**Affected components**: MAVLink/GCS integration, safety/anchor wrapper, separate e2e test suite.
**Mitigation strategy**:
1. Use pymavlink for exact `GPS_INPUT` field control.