31 lines
1.6 KiB
Markdown
31 lines
1.6 KiB
Markdown
# TODO
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This file tracks the active execution queue. Use [`MEMORY.md`](./MEMORY.md) for durable context, sourced facts, guardrails, and decisions.
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Last updated: `2026-03-28`
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## Now
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- [ ] Implement `getRho.m` and include the required stratosphere branch for altitude `> 11 km`.
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- [ ] Fill the known assignment constants in [`code/Interceptor_3DOF.m`](./code/Interceptor_3DOF.m) and [`code/getGuidance.m`](./code/getGuidance.m).
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- [ ] Replace the current syntax-breaking `XX` placeholders that prevent the model from starting in Octave.
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- [ ] Use [`docs/Addendum to Atomosphere Model Feb 26.pdf`](./docs/Addendum%20to%20Atomosphere%20Model%20Feb%2026.pdf) when implementing the `z > 11000 m` atmosphere branch.
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## Blocked
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- [ ] Transcribe missile and target reference areas, thrust curves, mass curves, and drag tables from [`docs/Missile and Target Data for 3DOF Spring 26.pdf`](./docs/Missile%20and%20Target%20Data%20for%203DOF%20Spring%2026.pdf).
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## Next
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- [ ] Replace the remaining `XX` arrays in [`code/T3dxdt.m`](./code/T3dxdt.m) and [`code/M3dxdt.m`](./code/M3dxdt.m) with sourced data.
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- [ ] Run [`code/Interceptor_3DOF.m`](./code/Interceptor_3DOF.m) in Octave and fix the next runtime errors.
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- [ ] Verify the required plots and inspect `Ttrajectory.csv` and `Mtrajectory.csv`.
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## Done Criteria
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- [ ] No remaining `XX` placeholders in executable code.
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- [ ] `getRho.m` exists and is used by both vehicle dynamics models.
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- [ ] The atmosphere model includes the required stratosphere handling for altitude `> 11 km`.
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- [ ] The full script runs in Octave without syntax or runtime errors.
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- [ ] The required plots and CSV outputs are generated.
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