vibe coding an orbital mechanics simulation to try out claude code
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4.7 KiB

Config Validation Refactoring Plan

Status: COMPLETED

Overview

Refactor config validation logic to separate it from parsing logic in config_loader.cpp, creating a dedicated config_validator module.

Phase 1: Create Config Validator Module - COMPLETE

Goal: Separate validation logic from parsing logic

Tasks:

  1. Create src/config_validator.h with function declarations:

    • bool validate_initial_positions(SimulationState* sim) - move from simulation
    • bool validate_mass_ratios(SimulationState* sim) - new
    • bool validate_soi_overlap(SimulationState* sim) - new
    • bool validate_nested_orbits(SimulationState* sim) - new
    • bool run_all_config_validations(SimulationState* sim) - wrapper
  2. Create src/config_validator.cpp with implementations:

    • Move validate_initial_positions() from simulation.cpp
    • Implement validate_mass_ratios() - check parent mass / child mass >= MIN_MASS_RATIO (1000)
    • Implement validate_soi_overlap() - for bodies sharing same parent, check if distance < (soi_a + soi_b), ERROR if true
    • Implement validate_nested_orbits() - for chains like Sun→Earth→Moon, ensure child's orbital radius is < (fraction) of parent's SOI
    • Implement run_all_config_validations() - calls all validators and returns false if any fail

Design Decisions:

  • SOI overlap: ERROR (reject configs with overlapping SOIs)
  • Mass ratio threshold: MACRO/DEFINE for easy adjustment (default 1000)
  • Nested orbit check: Use SOI (not Hill sphere), check child_semi_major_axis < (0.5 * parent_soi_radius)

Phase 2: Update Existing Modules - COMPLETE

  • Updated: src/config_loader.h - Added #include "config_validator.h"
  • Updated: src/config_loader.cpp:
    • Replaced validate_initial_positions() call with run_all_config_validations()
    • Removed inline validation blocks (parent_index_ordering, orbital_elements)
  • Updated: src/simulation.h - Removed declaration of validate_initial_positions()
  • Updated: src/simulation.cpp - Removed implementation of validate_initial_positions()

Phase 3: Update Tests - COMPLETE

  • Updated: tests/test_invalid_parent_assignment.cpp:
    • Deleted Test 1: "Earth should not become child of spacecraft" (obsolete)
    • Deleted Test 3: "Detect placeholder config values" (obsolete)
    • Updated Test 4: "Mutual SOI" to expect load_system_config() failure

Phase 4: Update Build System - COMPLETE

  • Updated: Makefile:
    • Added config_validator.o to test-build dependencies

File Changes Summary - COMPLETE

New Files:

  • src/config_validator.h
  • src/config_validator.cpp

Modified Files:

  • src/config_loader.h
  • src/config_loader.cpp
  • src/simulation.h
  • src/simulation.cpp
  • Makefile
  • tests/test_invalid_parent_assignment.cpp

New Test Configs:

  • tests/configs/small_comet_bad_mass_ratio.toml (invalid config for Test 2)

Existing Test Configs (keep as-is):

  • tests/configs/mutual_soi_close.toml (invalid config for Test 4)

Implementation Order

  1. Create config_validator module (Phase 1)
  2. Update simulation and config_loader (Phase 2)
  3. Update build system (Phase 4 - test compile)
  4. Update tests and configs (Phase 3)
  5. Run full test suite to verify changes

Validation Logic Details

validate_mass_ratios(SimulationState* sim)

  • For all bodies with parent_index >= 0:
    • Calculate ratio = parent_mass / child_mass
    • If ratio < MIN_MASS_RATIO (1000), print error and return false
    • Skip check for spacecraft (they have their own validation)

validate_soi_overlap(SimulationState* sim)

  • For all pairs of bodies sharing the same parent:
    • Calculate distance between their orbital positions
    • Calculate sum of their SOI radii
    • If distance < (soi_a + soi_b), print error and return false

validate_nested_orbits(SimulationState* sim)

  • For all bodies with parent that is not root (parent_index != 0):
    • Calculate child's orbital radius (semi_major_axis)
    • Get parent's SOI radius
    • If child_semi_major_axis > (0.5 * parent_soi_radius), print error and return false
    • Ensures child is well within parent's gravitational dominance region

run_all_config_validations(SimulationState* sim)

  • Calls all validators in sequence:
    1. validate_parent_index_ordering()
    2. validate_orbital_elements()
    3. validate_mass_ratios()
    4. validate_soi_overlap()
    5. validate_nested_orbits()
    6. validate_initial_positions()
  • Returns false if any validator fails
  • Stops on first failure for efficiency

Constants and Thresholds

#define MIN_MASS_RATIO 1000.0
#define NESTED_ORBIT_FRACTION 0.5  // Child orbit must be < 50% of parent SOI