Mission Command Layer- Module 1: Startup and Igniter(System boot and ignition)Guidance & Navigation Control- Module 2: Real-Time Sensor(Real‑time observation)- Module 3: Timeline Adjuster(Time‑axis correction)- Module 4: Feedback Uplinker(Upstream feedback link)Telemetry Downlink Receiver- Module 5: Data Telemetry Receiver(Downlink data processing)Timeline Dynamics Processor- Module 6: Velocity Vector Stabilizer(Stabilization of temporal velocity vectors)- Module 7: Timeline Interpolation(Time‑axis interpolation)- Module 8: Timeline Thruster(Time‑axis propulsion output)
static void i2s_prime_and_enable(i2s_chan_handle_t handle) { // Initialize monitoring parameters g_ddc.ddc_ring_looses = 0; g_ddc.ddc_ring_wl = 0.0f; g_ddc.ddc_rx_size = 0, g_ddc.ddc_tx_size = 0, // Initialize PCNT counter normal_fscount(&g_cnt_ideal); // Set normal position // Initialize clock reference values g_cnt_ideal.last_fb = (1 << 14), // Q14 = 1.0 g_cnt_ideal.acc_q14 = 0, g_cnt_ideal.delta_fb_q = 0, g_cnt_ideal.source_clock_ratio = 1.0f, // Initial ASRC ratio // Prepare I2S launch pad g_ddc.i2s_starting = true; g_ddc.i2s_start_ms = xTaskGetTickCount(); g_ddc.counter_warmup_rollout = false; g_ddc.i2s_src_locked = false; g_ddc.i2s_src_lockcount = 0; g_ddc.i2s_src_phase_ratio = 1.0f; g_ddc.i2s_src_smooth_ratio = 1.0f; g_ddc.i2s_src_phase = 0; g_ddc.i2s_src_in_idx = 0; g_ddc.i2s_src_prev_consumed = -1; g_ddc.i2s_pcnt_delta_hz = 0; // Prepare UAC feedback engine g_ddc.uac_fb_inverval_count = 0; g_ddc.uac_fb_started = false; g_ddc.uac_fb_start_pending = true; // Important g_ddc.uac_fb_locked = false; g_ddc.uac_fb_lockcount = 0; g_ddc.uac_long_err_mHz = 0; // Clear any remaining audio buffer rb_dropall(&g_audio_ring); // Reboot count timer gptimer_stop(g_gptimer); gptimer_start(g_gptimer); // Now enable to start DMA i2s_channel_enable(handle);}