1.6 KiB
1.6 KiB
TODO
This file tracks the active execution queue. Use MEMORY.md for durable context, sourced facts, guardrails, and decisions.
Last updated: 2026-03-28
Now
- Implement
getRho.mand include the required stratosphere branch for altitude> 11 km. - Fill the known assignment constants in
code/Interceptor_3DOF.mandcode/getGuidance.m. - Replace the current syntax-breaking
XXplaceholders that prevent the model from starting in Octave. - Use
docs/Addendum to Atomosphere Model Feb 26.pdfwhen implementing thez > 11000 matmosphere branch.
Blocked
- Transcribe missile and target reference areas, thrust curves, mass curves, and drag tables from
docs/Missile and Target Data for 3DOF Spring 26.pdf.
Next
- Replace the remaining
XXarrays incode/T3dxdt.mandcode/M3dxdt.mwith sourced data. - Run
code/Interceptor_3DOF.min Octave and fix the next runtime errors. - Verify the required plots and inspect
Ttrajectory.csvandMtrajectory.csv.
Done Criteria
- No remaining
XXplaceholders in executable code. getRho.mexists and is used by both vehicle dynamics models.- The atmosphere model includes the required stratosphere handling for altitude
> 11 km. - The full script runs in Octave without syntax or runtime errors.
- The required plots and CSV outputs are generated.