From 8f60ba54f0202ce13a46213330b1ee4f545b8169 Mon Sep 17 00:00:00 2001 From: cinnaboot Date: Sun, 18 Jan 2026 11:04:37 -0500 Subject: [PATCH] Fix compiler warnings: remove unused variables, increase buffer size --- src/mission_planning.cpp | 2 -- src/renderer.cpp | 2 +- 2 files changed, 1 insertion(+), 3 deletions(-) diff --git a/src/mission_planning.cpp b/src/mission_planning.cpp index 94a660b..8a0f20d 100644 --- a/src/mission_planning.cpp +++ b/src/mission_planning.cpp @@ -21,7 +21,6 @@ TransferParameters calculate_hohmann_transfer(double r_departure, double r_arriv params.delta_v_capture = 0.0; - double departure_period = 2.0 * M_PI * sqrt(pow(r_departure, 3) / (G * central_mass)); double arrival_period = 2.0 * M_PI * sqrt(pow(r_arrival, 3) / (G * central_mass)); params.phase_angle_deg = calculate_required_phase_angle(params.transfer_time, arrival_period); @@ -112,7 +111,6 @@ int spawn_spacecraft_on_transfer(SimulationState* sim, int departure_idx, } CelestialBody* departure = &sim->bodies[departure_idx]; - CelestialBody* sun = &sim->bodies[0]; CelestialBody spacecraft; spacecraft.name[0] = 'S'; diff --git a/src/renderer.cpp b/src/renderer.cpp index c1fc8bc..054941c 100644 --- a/src/renderer.cpp +++ b/src/renderer.cpp @@ -414,7 +414,7 @@ void render_info(SimulationState* sim) { // Prepare info text char info_text[1024]; - char temp_buffer[256]; + char temp_buffer[512]; snprintf(info_text, sizeof(info_text), "Orbital Mechanics Simulation\n\n");