fix(gps): adapt Doppler bandwidth from board validation

hardware/external/gps/rtl/pps/README.md

@@ -57,6 +57,28 @@ This keeps quality policy and the small navigation pre-filter in software
 while the deterministic PI loop, fixed-point rate state and physical edge
 generation remain in hardware.
 
+In a conventional absolute-pseudorange model, receiver clock bias and
+receiver clock drift are the level and slope of the same physical clock:
+`b_r = c*delta_t_r` and `bdot_r = c*d(delta_t_r)/dt`. The position-WLS bias
+in this project is different: subtracting the common capture time and adding
+`STARTOFFSET` makes it a reference-satellite-relative datum, approximately
+`c*STARTOFFSET - reference_range`, rather than a pure receiver oscillator
+offset.
+
+The Doppler WLS still solves a fourth, common receiver clock/frequency-drift
+state. The PPS pre-filter does not use that state directly as the derivative
+of the position-WLS datum. Instead, it predicts that datum with:
+
+```text
+position_datum_drift =
+    -reference_geometric_range_rate
+    + c * reference_satellite_clock_drift
+```
+
+The geometric term uses the Doppler-WLS receiver velocity plus the selected
+reference satellite position and velocity. The PPS RTL sees only the
+resulting timestamped reference and loop configuration.
+
 The APB register offsets live in `pps_pkg.sv`.  Multiword input fields are
 shadow registers and must be followed by one `COMMIT` write.  A new mailbox
 must not be written while `STATUS.COMMIT_BUSY` is set.

hardware/external/gps/rtl/trck_src/README.md

@@ -89,6 +89,33 @@ observation = measured_range_rate
 H = [-u_x, -u_y, -u_z, 1]
 ```
 
+Buradaki dorduncu state, tum uydu Doppler observation'larina ortak giren
+receiver clock/frequency drift'idir. Klasik mutlak-pseudorange modelinde
+receiver zaman hatasi `delta_t_r(t)` icin:
+
+```text
+clock_bias_m        = c * delta_t_r(t)
+clock_drift_mps     = c * d(delta_t_r(t))/dt
+clock_bias_m(t+dt) ~= clock_bias_m(t) + clock_drift_mps * dt
+```
+
+`clock_drift_mps`, receiver local oscillator frequency error'inin range-rate
+birimindeki ortak etkisidir. `0.1 ppm`, yaklasik `29.98 m/s`'ye karsilik
+gelir. Bu ortak state olmadan oscillator hatasi receiver hareketinin bir
+parcasi sanilirdi.
+
+Bu projedeki position WLS bias'i ise mutlak receiver clock bias'i degildir.
+Ortak capture zamani cikarildigi ve `STARTOFFSET` eklendigi icin
+referans-uyduya bagli goreli bir datum cozer. Bu nedenle Doppler WLS
+`clock_drift_mps` state'i, position WLS `clock_bias_m` degerinin turevi olarak
+dogrudan baglanmaz.
+
+Iki WLS ayri observation ve normal equation kullanir; fakat Doppler WLS tam
+bagimsiz degildir. Uydu LOS vektorlerini kurmak icin position WLS'den gelen
+guncel receiver ECEF konumunu, ephemeristen gelen uydu ECEF konum/hiz ve clock
+drift'ini kullanir. Satellite clock drift bilinen duzeltmedir; WLS'nin
+dorduncu bilinmeyeni receiver clock drift'idir.
+
 WLS en az dort gecerli uydu ister; ECEF velocity, 3x3 covariance, receiver
 clock drift ve residual RMS uretir. Fusion adapter velocity/covariance'i ENU'ya
 dondurur ve ayri velocity NIS kapisi ile 15-state ESKF'ye verir.

soc/software/gps_measurement_python/README.md

@@ -90,10 +90,11 @@ modelinin açıklayamadığı kanal-bağımlı excess jitter'ı şişirir.
 Ayrı 1D model ham code, kör scalar IIR ve Doppler-predicted code smoothing'i
 range-rate adımları ve residual carrier CFO altında karşılaştırır. Carrier
 ölçümleri RTL cadence'i olan 50 Hz'de üretilir ve 200 ms WLS epoch'una kadar
-entegre edilir. Hem raw carrier-rate hem de mevcut firmware'deki
-`GPS_TRACK_DOPPLER_SMOOTH_ALPHA=0.05` çıkışı denenir. Bu ayrım önemlidir:
+entegre edilir. Ham, sabit `alpha=0.05` ve IMU hareket durumuna göre bant
+genişliğini açan adaptif Doppler yolları birlikte denenir. Bu ayrım önemlidir:
 PPS datum-drift predictor'u için yararlı olan yavaş Doppler filtresi, ESKF
-velocity veya hızlı code-aiding prediction'ında dinamik lag üretebilir.
+velocity veya hızlı code-aiding prediction'ında dinamik lag üretebilir; tam
+ham snapshot ise kartta ölçülen gürültü seviyesinde fazla varyans üretebilir.
 
 ## Doppler pre-IIR ve ESKF modeli
 
@@ -121,7 +122,7 @@ Senaryo matrisi sabit uçuş, airliner/aggressive manevra, düşük C/N0, tek-ka
 Doppler burst, common receiver clock-drift step, 15 saniye GPS kesintisi ve
 birleşik arıza koşullarını içerir.
 
-20-seed sentetik sonuçların özeti:
+Nominal 20-seed sentetik sonuçların özeti:
 
 - ESKF ham WLS gürültüsünü nominalde yaklaşık `0.416 m/s` 3D RMS'ten `0.190
   m/s` seviyesine indirir; temporal filtreleme zaten ESKF'de gerçekleşir.
@@ -136,11 +137,25 @@ birleşik arıza koşullarını içerir.
 - Common receiver clock-frequency hatası WLS'nin dördüncü clock-drift state'i
   tarafından hızdan ayrılır.
 
-Bu sonuçlarla firmware'de ESKF için ham Doppler -> kanal validity/FDE ->
-velocity WLS + covariance -> ESKF yolu uygulanmıştır. Ayrı yavaş-filtered
-Doppler velocity yalnız PPS position-WLS clock-bias datumunun drift predictor'u
-ve PPS kalite metriği için tutulur. Ayrıntılı tablo ve sınırlar
-`output/DOPPLER_ESKF_ANALYSIS.md` içindedir.
+Genesys2 sabit-kart ölçümünde tam ham yolun velocity-WLS RMS'i `9.17 m/s`,
+p95'i `16.71 m/s` ve FDE oranı `86/120` oldu. Aynı epoch'larda sabit
+`alpha=0.05` yol `0.92 m/s` RMS, `1.63 m/s` p95 ve `0/120` FDE verdi. Bu
+nedenle nominal modelde iyi görünen doğrudan ham yol production'a alınmadı.
+Kart gürültüsünü eşlemek için tracking noise `22x` ile kalibre edilen regresyon
+modelindeki regresyon seed'leri için steady-7/airliner-3/aggressive-7 fused
+RMS değerleri:
+
+- sabit IIR: `0.451 / 0.484 / 1.036 m/s`,
+- adaptif IIR: `0.451 / 0.336 / 0.538 m/s`,
+- tam ham: `1.260 / 1.100 / 1.260 m/s`.
+
+Production firmware ESKF için `alpha=0.05/0.20/0.40` hareket-adaptif Doppler
+-> bandwidth-aware sigma -> kanal validity/FDE -> velocity WLS + covariance
+-> ESKF yolunu kullanır. Ham alan tanısal kayıt ve offline analiz için korunur.
+Ayrı sabit `alpha=0.05` Doppler velocity yalnız PPS position-WLS clock-bias
+datumunun drift predictor'u ve PPS kalite metriği için kullanılır. Ayrıntılı
+nominal tablo ve model sınırları `output/DOPPLER_ESKF_ANALYSIS.md` içindedir;
+kart-kalibreli karar `test_doppler_eskf_model.py` ile regresyona alınmıştır.
 
 ## Kurulum ve çalıştırma
 

soc/software/gps_measurement_python/analyze_doppler_eskf.py

@@ -348,10 +348,10 @@ def write_report(path: Path, summaries: list[Summary], seed_count: int) -> None:
             "",
             "## Mimari kararı",
             "",
-            "- ESKF açıkken uygulanan ana yol: 20 ms ham Doppler snapshot -> kanal validity/outlier kontrolü -> 5 Hz robust velocity WLS + gerçek covariance -> adapter tabanları -> ESKF. Sabit `alpha=0.05` temporal IIR yalnız PPS drift-predictor yolunda kalır.",
+            "- Nominal sentetik model ham Doppler'in sabit pre-IIR gecikmesini önlediğini gösterir; fakat Genesys2 kart-kalibreli noise regresyonunda tam ham yol fazla gürültülüdür. Production ana yolu: hareket-adaptif Doppler -> bandwidth-aware sigma -> kanal validity/outlier kontrolü -> 5 Hz robust velocity WLS + gerçek covariance -> adapter tabanları -> ESKF.",
             "- ESKF yalnız 3D aggregate velocity gördüğü için tek uydu hatasını sonradan teşhis edemez. Per-satellite robust gate/FDE WLS öncesinde kalmalıdır.",
-            "- Standalone GPS speed, PPS aiding veya ESKF kapalı build için ayrı, yavaş filtrelenmiş Doppler çıktısı tutulabilir. Aynı filtered değeri hem code aiding hem ESKF velocity için kullanmak uygun değildir.",
-            "- Adaptif IIR mümkündür; modelde C/N0 sakin-state alpha'sını, düşük geçiren IMU navigation acceleration ise dynamic alpha'yı seçer. Ancak ESKF'li ana yol için ham ölçüm daha sade ve gecikmesizdir.",
+            "- Ayrı sabit `alpha=0.05` yol PPS drift predictor ve standalone sakin-hız kalite metriği için tutulur; ham snapshot tanısal/offline analiz için korunur.",
+            "- Production adaptif IIR sakin/hareketli/yüksek-ivme için `alpha=0.05/0.20/0.40` seçer. Alpha büyüdükçe EWMA noise gain'i WLS sigma'sına yansıtılır; böylece FDE ve ESKF covariance bant genişliğini bilir.",
             "",
             "## Model sınırları",
             "",

soc/software/gps_measurement_python/doppler_eskf_model.py

@@ -4,7 +4,7 @@ The model compares four paths using one shared 50 Hz tracking stream and one
 shared 100 Hz IMU stream:
 
 * the legacy fixed-alpha Doppler IIR before 5 Hz velocity WLS;
-* raw Doppler into WLS, leaving temporal filtering to the ESKF;
+* raw Doppler into WLS, as a nominal-model comparison rather than production;
 * a global IMU-driven adaptive-alpha IIR;
 * raw Doppler with the per-satellite robust WLS gate used before the ESKF.
 

soc/software/gps_measurement_python/output/DOPPLER_ESKF_ANALYSIS.md

@@ -50,10 +50,10 @@ Monte Carlo seed sayısı: `20`; ilk 5 saniye RMS metriklerinden çıkarıldı.
 
 ## Mimari kararı
 
-- ESKF açıkken uygulanan ana yol: 20 ms ham Doppler snapshot -> kanal validity/outlier kontrolü -> 5 Hz robust velocity WLS + gerçek covariance -> adapter tabanları -> ESKF. Sabit `alpha=0.05` temporal IIR yalnız PPS drift-predictor yolunda kalır.
+- Nominal sentetik model ham Doppler'in sabit pre-IIR gecikmesini önlediğini gösterir; fakat Genesys2 kart-kalibreli noise regresyonunda tam ham yol fazla gürültülüdür. Production ana yolu: hareket-adaptif Doppler -> bandwidth-aware sigma -> kanal validity/outlier kontrolü -> 5 Hz robust velocity WLS + gerçek covariance -> adapter tabanları -> ESKF.
 - ESKF yalnız 3D aggregate velocity gördüğü için tek uydu hatasını sonradan teşhis edemez. Per-satellite robust gate/FDE WLS öncesinde kalmalıdır.
-- Standalone GPS speed, PPS aiding veya ESKF kapalı build için ayrı, yavaş filtrelenmiş Doppler çıktısı tutulabilir. Aynı filtered değeri hem code aiding hem ESKF velocity için kullanmak uygun değildir.
-- Adaptif IIR mümkündür; modelde C/N0 sakin-state alpha'sını, düşük geçiren IMU navigation acceleration ise dynamic alpha'yı seçer. Ancak ESKF'li ana yol için ham ölçüm daha sade ve gecikmesizdir.
+- Ayrı sabit `alpha=0.05` yol PPS drift predictor ve standalone sakin-hız kalite metriği için tutulur; ham snapshot tanısal/offline analiz için korunur.
+- Production adaptif IIR sakin/hareketli/yüksek-ivme için `alpha=0.05/0.20/0.40` seçer. Alpha büyüdükçe EWMA noise gain'i WLS sigma'sına yansıtılır; böylece FDE ve ESKF covariance bant genişliğini bilir.
 
 ## Model sınırları
 

soc/software/gps_measurement_python/test_doppler_eskf_model.py

@@ -2,6 +2,7 @@
 
 from __future__ import annotations
 
+from dataclasses import replace
 import unittest
 
 import numpy as np
@@ -42,6 +43,19 @@ def _wls_rms(trace) -> float:
     return float(np.sqrt(np.mean(np.sum(np.square(error), axis=1))))
 
 
+def _board_raw_noise_scenario(name: str):
+    """Match the 9.17 m/s raw-WLS RMS measured on Genesys2."""
+    scenario = _scenario(name)
+    nominal_noise = scenario.noise_multiplier
+    return replace(
+        scenario,
+        name=f"{scenario.name}_genesys2_noise",
+        noise_multiplier=lambda time_s, satellite: (
+            22.0 * nominal_noise(time_s, satellite)
+        ),
+    )
+
+
 class DopplerWlsTest(unittest.TestCase):
     def test_four_state_wls_separates_velocity_and_clock_drift(self) -> None:
         velocity = np.asarray([145.0, -32.0, 7.5])
@@ -85,6 +99,56 @@ class AdaptiveAlphaTest(unittest.TestCase):
 
 
 class DopplerEskfIntegrationTest(unittest.TestCase):
+    def test_board_raw_noise_requires_adaptive_prefilter(self) -> None:
+        steady = run_doppler_eskf_scenario(
+            _board_raw_noise_scenario("steady_cruise"),
+            seed=7,
+            paths=(
+                DopplerPath.FIXED_IIR,
+                DopplerPath.ADAPTIVE_IIR,
+                DopplerPath.RAW,
+            ),
+        )
+        airliner = run_doppler_eskf_scenario(
+            _board_raw_noise_scenario("airliner_maneuver"),
+            seed=3,
+            paths=(
+                DopplerPath.FIXED_IIR,
+                DopplerPath.ADAPTIVE_IIR,
+                DopplerPath.RAW,
+            ),
+        )
+        aggressive = run_doppler_eskf_scenario(
+            _board_raw_noise_scenario("aggressive_maneuver"),
+            seed=7,
+            paths=(
+                DopplerPath.FIXED_IIR,
+                DopplerPath.ADAPTIVE_IIR,
+                DopplerPath.RAW,
+            ),
+        )
+        steady_fixed = _fused_rms(steady[DopplerPath.FIXED_IIR])
+        steady_adaptive = _fused_rms(steady[DopplerPath.ADAPTIVE_IIR])
+        steady_raw = _fused_rms(steady[DopplerPath.RAW])
+        airliner_fixed = _fused_rms(airliner[DopplerPath.FIXED_IIR])
+        airliner_adaptive = _fused_rms(airliner[DopplerPath.ADAPTIVE_IIR])
+        airliner_raw = _fused_rms(airliner[DopplerPath.RAW])
+        aggressive_fixed = _fused_rms(aggressive[DopplerPath.FIXED_IIR])
+        aggressive_adaptive = _fused_rms(
+            aggressive[DopplerPath.ADAPTIVE_IIR]
+        )
+        aggressive_raw = _fused_rms(aggressive[DopplerPath.RAW])
+
+        # Direct 20 ms snapshots are too noisy at the level actually observed
+        # on the board. Adaptive bandwidth retains the quiet-state result and
+        # beats both direct raw and the 0.39 s fixed-IIR lag in manoeuvres.
+        self.assertLess(steady_adaptive, 1.05 * steady_fixed)
+        self.assertLess(steady_adaptive, 0.50 * steady_raw)
+        self.assertLess(airliner_adaptive, airliner_fixed)
+        self.assertLess(airliner_adaptive, 0.50 * airliner_raw)
+        self.assertLess(aggressive_adaptive, 0.65 * aggressive_fixed)
+        self.assertLess(aggressive_adaptive, 0.50 * aggressive_raw)
+
     def test_eskf_filters_raw_doppler_without_pre_iir(self) -> None:
         traces = run_doppler_eskf_scenario(
             _scenario("steady_cruise"),

soc/software/gps_system/Makefile

@@ -82,6 +82,8 @@ BSP_SRCS := init.c uart.c plic.c irq.c spi_flash.c pmod_spi.c
 
 GPS_NAV_SOLVE_TIMER_TICKS ?= 10
 GPS_PPS_STATUS_LOG_INTERVAL ?= 10
+GPS_PPS_DOPPLER_PREDICTOR_ENABLE ?= 1
+GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES ?= 0
 
 include ../common/app.mk
 
@@ -94,7 +96,9 @@ CFLAGS += $(IMU_BACKEND_CFLAG) \
 	-DGPS_ESKF_ENABLE=$(GPS_ESKF_ENABLE) \
 	-DIMU_CORRECTED_PUBLISH_EVERY_N_SAMPLES=$(IMU_CORRECTED_PUBLISH_EVERY_N_SAMPLES) \
 	-DGPS_NAV_SOLVE_TIMER_TICKS=$(GPS_NAV_SOLVE_TIMER_TICKS) \
-	-DGPS_PPS_STATUS_LOG_INTERVAL=$(GPS_PPS_STATUS_LOG_INTERVAL)
+	-DGPS_PPS_STATUS_LOG_INTERVAL=$(GPS_PPS_STATUS_LOG_INTERVAL) \
+	-DGPS_PPS_DOPPLER_PREDICTOR_ENABLE=$(GPS_PPS_DOPPLER_PREDICTOR_ENABLE) \
+	-DGPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES=$(GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES)
 LDLIBS += -lm
 
 ifeq ($(GPS_DEBUG),1)

soc/software/gps_system/README.md

@@ -176,6 +176,24 @@ Iki komut ayni MCS/BIN yoluna yazdigi icin iki imaj birlikte saklanacaksa
 build'ler arasinda profil adiyla kopyalanmalidir. Bu secenekler software
 derleme parametresidir; mevcut bitstream ile `fpga-mcs` yeterlidir.
 
+PPS Doppler datum-drift predictor production'da varsayilan olarak aciktir.
+Kontrollu A/B icin build-time secenekleri:
+
+```sh
+# Production: predictor sürekli acik, otomatik A/B yok.
+make -C soc/software/gps_system \
+  GPS_PPS_DOPPLER_PREDICTOR_ENABLE=1 \
+  GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES=0
+
+# Tani: her 200 navigation update'inda (~40 s) kapali/acik degistir.
+make -C soc/software/gps_system \
+  GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES=200
+```
+
+`GPS_PPS_DOPPLER_PREDICTOR_ENABLE=0` yalniz kontrollu fallback testi icindir.
+`GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES` sifirdan buyukse A/B secimi enable
+degerini bilerek ezer; production image'da mutlaka `0` kalmalidir.
+
 Otomatik WHO_AM_I algilama varsayilandir:
 
 ```sh
@@ -812,15 +830,20 @@ range_rate_mps = -doppler_hz * c / 1575420000
 Ham 20 ms carrier snapshot'inda kartta gorulen birkac hertz jitter, L1'de
 metre/saniye seviyesinde range-rate gurultusune ve zayif geometride daha buyuk
 receiver velocity hatasina donusur. Software ISR her PRN icin ham degeri
-degistirmeden korur ve yalniz PPS predictor yolu icin ayri bir state'te:
+degistirmeden korur ve iki ayri state gunceller:
 
 ```text
-doppler_filtered = 0.05 * doppler_raw + 0.95 * doppler_previous
+PPS:  doppler_slow = 0.05 * raw + 0.95 * previous
+ESKF: doppler_fast = alpha * raw + (1-alpha) * previous
+      alpha = 0.05 stationary, 0.20 moving, 0.40 high acceleration
 ```
 
-hesaplar. Ham ve filtreli range-rate ayri alanlarda tutulur. 50 Hz measurement
-cadence'inde bu yaklasik `0.39 s` zaman sabitidir. Reacquisition/PRN
-degisiminde eski kanal state'i kullanilmaz.
+PPS yolu 50 Hz cadence'de yaklasik `0.39 s` zaman sabitine sahiptir. ESKF yolu
+fusion motion state ve gravity-compensated linear acceleration ile bant
+genisligini acar. Alpha buyudugunde EWMA noise kazanci kadar WLS range-rate
+sigma da buyutulur; bu, FDE ve ESKF covariance'in filtre bant genisliginden
+habersiz kalmasini engeller. Reacquisition/PRN degisiminde eski kanal state'i
+kullanilmaz.
 
 IIR donanimda da uygulanabilirdi; bunun icin kanal basina state,
 coefficient-multiply, rounding/saturation ve reacquisition reset kurali
@@ -847,12 +870,13 @@ weight = 1 / sigma_rate^2
 Her 200 ms navigation epoch'unda iki velocity tuketicisi vardir:
 
 ```text
-raw range-rate      -> robust velocity WLS -> fusion adapter -> ESKF
-filtered range-rate -> robust velocity WLS -> PPS bias-drift predictor
+adaptive range-rate -> robust velocity WLS -> fusion adapter -> ESKF
+slow range-rate     -> robust velocity WLS -> PPS bias-drift predictor
 ```
 
-Ham ESKF yolu temporal filtreleme isini ESKF'ye birakir ve `alpha=0.05`
-IIR'in yaklasik 390 ms dinamik gecikmesini velocity measurement'a eklemez.
+Tam ham 20 ms snapshot yolu kart A/B'sinde fazla gurultulu bulundugu icin
+ESKF'ye yayinlanmaz. Adaptif yol sakin durumda PPS kadar dusuk gurultulu,
+harekette ise sabit `alpha=0.05` yolundan daha dusuk gecikmelidir.
 PPS'in ana olcumu position WLS `clock_bias_m` sonucudur. Filtreli velocity
 yalniz bu referans-datum bias'inin 200 ms epoch'lar arasindaki turevini
 ongormek ve PPS kalite profilini siniflandirmak icin kullanilir. Doppler
@@ -905,9 +929,8 @@ velocity/covariance, `speed_mps`, `velocity_residual_rms_mps`,
 Fusion adapter covariance'i `R_ecef_to_enu * P * R^T` ile ENU'ya dondurur.
 2026-07-25 sabit kart verisinde zayif geometriyle gorulen
 `p95=6.020 m/s` speed hatasi nedeniyle default alt sinirlar yatay eksenlerde
-`2.0 m/s`, dikey eksende `3.0 m/s`'dir. ESKF artik ham Doppler WLS aldigi icin
-bu konservatif tabanlar temporal korelasyondan cok zayif geometri ve kartta
-henuz yeniden kalibre edilmemis raw-Doppler hata kuyruklarini sinirlar; formal
+`2.0 m/s`, dikey eksende `3.0 m/s`'dir. Bu konservatif tabanlar zayif geometri
+ve kartta kalan Doppler hata kuyruklarini sinirlar; formal
 covariance daha buyukse aynen korunur. Velocity innovation 3-DOF `%99.9`
 `NIS=16.266` kapisindan gecer. Kabul/red sayilari ve son velocity NIS'i
 `[FUSION]` UART status satirinda `velocity=accepted/rejected` ve `vel_nis`
@@ -964,9 +987,9 @@ GPS_LOG(level, category, ...)
 
 | `GPS_DEBUG_LEVEL` | Eklenen cikti |
 | ---: | --- |
-| `1` | Temel telemetri: ham GPS/WLS `[LOCATION] source=gps` satirinda DOP ile birlikte `velocity_valid`, `speed` ve `velocity_rms`; gecerliyse ESKF `[LOCATION] source=imu_corrected`; sifir tabanli donanim kanal numaralarini tasiyan `[TRK] tracked satellites=... prn_indices=[...]` (`0` = GPS PRN `G01`). Baslangicta fusion/IMU konfigurasyonu da bir kez yazilir. |
+| `1` | Temel telemetri: ham GPS/WLS `[LOCATION] source=gps` satirinda DOP ile birlikte `velocity_valid`, `speed` ve `velocity_rms`; gecerliyse ESKF `[LOCATION] source=imu_corrected`; sifir tabanli donanim kanal numaralarini tasiyan `[TRK] tracked satellites=... prn_indices=[...]` (`0` = GPS PRN `G01`). Baslangicta fusion/IMU konfigurasyonu ve periyodik `[FUSION]` NIS/kabul-red durumu da gorulur. |
 | `2` | Gelecekteki ek status ayrintilari icin ayrilmistir. Su an level 2'ye ozel mesaj yoktur; pratikte level 1 ile ayni ciktiyi verir. |
-| `3` | Level 1'e ek olarak acquisition/tracking/navigation durum gecisleri, warning/error mesajlari, integrity bilgileri ve periyodik ayrintili `[FUSION] state=...` durumu. |
+| `3` | Level 1'e ek olarak acquisition/tracking/navigation durum gecisleri, warning/error mesajlari ve integrity bilgileri. |
 | `4` | Level 3'e ek olarak performans, scheduler, nav-bit/parser, uydu/olcum ve dusuk seviye TRACE tanilari. UART yuku en yuksek seviyedir. |
 
 `Makefile` varsayilanlari `GPS_DEBUG=1` ve `GPS_DEBUG_LEVEL=4`'tur. Bu nedenle
@@ -1234,10 +1257,51 @@ azaltiyor ve C/N0 weighting ornek epoch'ta sonucu iyilestiriyor. Buna ragmen
 position WLS'deki pseudorange/code-phase hata ve zayif geometriyi tek basina
 duzeltmiyor. Doppler velocity artik ESKF state update'ine baglidir; formal
 covariance, kart verisine dayali floor ve ayri NIS gate ile asiri guven
-sinirlanir. Bu yeni software'in gercek kartta `vel_nis` ve
-`velocity=accepted/rejected` sayaclariyla saha A/B sonucu henuz olculmedi;
-yukaridaki board istatistikleri ESKF entegrasyonundan onceki ham velocity
-dogrulamasidir.
+sinirlanir. Yukaridaki board istatistikleri ESKF entegrasyonundan onceki
+velocity dogrulamasidir; entegrasyon sonrasi `vel_nis` ve
+`velocity=accepted/rejected` saha sonucu bir sonraki bolumdedir.
+
+### 2026-07-26 Genesys2 PPS ve Doppler/ESKF A/B
+
+Kart sabitken once tam ham 20 ms snapshot -> robust WLS -> ESKF yolu olculdu.
+Son 120 PPS penceresinde ham WLS speed RMS `9.17 m/s`, p95 `16.71 m/s` ve
+raw-FDE `86/120` oldu. Yavas `alpha=0.05` PPS yolu ayni pencerede `0.92 m/s`
+RMS, `1.63 m/s` p95 ve `0/120` FDE verdi. ESKF+ZUPT fused hizi dusuk tutsa da
+bu sonuc tam ham yolun hareketli platform icin guvenli oldugunu dogrulamadi.
+
+Bu nedenle ESKF icin yukarida tarif edilen ayri adaptif yol uygulandi. Ayni
+kartta 240 epoch'luk yerlesmis pencerede `alpha=0.05`, speed RMS `0.48 m/s`,
+p95 `0.83 m/s`, FDE `0/240` olculdu. Son 180 saniyede ESKF velocity kabul/red
+farki `892/0`, velocity NIS median/p95/max `0.028/0.111/0.180`, fused speed
+RMS `0.0052 m/s` oldu. IMU overflow sayaci bu pencerede `15` olarak sabit
+kaldi; olcum telemetrisi yeni kayip uretmedi.
+
+PPS predictor, yeniden boot etmeden 40 saniyelik kapali/acik segmentlerle A/B
+yapildi (`GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES=200`, yalniz tanisal build).
+Her segmentin ilk bes saniyesi atildiginda predictor acik segmentlerde software
+clock-bias innovation RMS `12.52 m`, kapali segmentlerde `46.48 m` oldu.
+Hardware phase p95 acikken `51.02 ns`, kapaliyken `58.21 ns` idi. Tek acik
+segmentte gorulen bir `-216.48 ns` one-epoch phase transient'i lock kaybi
+olusturmadi; bu nedenle physical-pin jitter sonucu olarak yorumlanmaz.
+Production default predictor acik, A/B toggling kapali (`0`) kalir.
+
+Son olarak `adaptive-pps-final-20260726` production image'i
+`PREDICTOR_ENABLE=1`, `PREDICTOR_AB_UPDATES=0` ile RAM'den karta yuklendi.
+Acquisition/coarse baslangici dislandiktan sonraki 120 lock status orneginde:
+
+- predictor tum orneklerde `1`, ESKF alpha sabit kartta tum orneklerde `0.05`,
+- adaptive velocity-WLS speed RMS/p95 `0.52/0.92 m/s`, FDE `0/120`,
+- ESKF velocity kabul/red farki `448/0`, velocity NIS p95/max
+  `0.139/0.341`, fused speed RMS `0.0061 m/s`,
+- PPS software clock innovation RMS `12.36 m`,
+- internal hardware phase RMS ve p95-absolute `28.50/58.36 ns`, lock kaybi
+  `0/120`,
+- IMU overflow sayaci `13..13`, tracking measurement missed sayaci `0..0`
+  kaldi.
+
+Bu `hw_phase`, APB status'taki son commit residual'idir; fiziksel PPS pin
+jitter'i degildir. Dolayisiyla `15-20 ns` pin hedefinin saglandigi bu logdan
+iddia edilmez; scope veya time-interval counter ile ayri olculmelidir.
 
 ### 2026-07-08 ACQ Debug Notu
 

soc/software/gps_system/gps_system.c

@@ -29,6 +29,22 @@
 #define IMU_SAMPLES_BEFORE_GPS_SERVICE 1u
 #define IMU_SAMPLES_AFTER_GPS_SERVICE  3u
 
+static void update_eskf_doppler_bandwidth(
+	const navigation_fusion_output_t* output)
+{
+	if((output == NULL) || !output->local_valid)
+	{
+		return;
+	}
+	double alpha = 0.05;
+	if(output->motion_state == FUSION_MOTION_MOVING)
+	{
+		alpha = (output->linear_acceleration_norm_mps2 >= 2.5) ?
+			0.40 : 0.20;
+	}
+	gps_receiver_set_eskf_doppler_alpha(alpha);
+}
+
 static void initialize_sensor_fusion(gps_system_state_t* system)
 {
 	system->fusion_enabled = (GPS_ESKF_ENABLE != 0);
@@ -69,9 +85,13 @@ static unsigned int feed_pending_imu_to_eskf(
 	      imu_sensor_take_measurement(&system->imu_sample))
 	{
 		bool accepted = navigation_fusion_push_imu(&system->imu_sample);
-		if(accepted &&
-		   navigation_fusion_get_output(&system->fused_solution) &&
-		   system->fused_solution.global_valid &&
+		bool output_available = accepted &&
+			navigation_fusion_get_output(&system->fused_solution);
+		if(output_available)
+		{
+			update_eskf_doppler_bandwidth(&system->fused_solution);
+		}
+		if(output_available && system->fused_solution.global_valid &&
 		   (system->fused_solution.timestamp_ticks !=
 		    system->last_fused_location_tick))
 		{

soc/software/gps_system/header/fusion/navigation_fusion.h

@@ -19,6 +19,7 @@ typedef struct {
 	double height_m;
 	double position_std_m[3];
 	double speed_mps;
+	double linear_acceleration_norm_mps2;
 	double last_position_nis;
 	double last_velocity_nis;
 	fusion_motion_state_t motion_state;

soc/software/gps_system/header/gps/gps_interrupt_handlers.h

@@ -55,6 +55,8 @@
 	void gps_background_task(void);
 	bool gps_take_nav_epoch_snapshot(gps_nav_epoch_snapshot_t* snapshot);
 	void gps_get_runtime_diagnostics(gps_runtime_diagnostics_t* diagnostics);
+	void gps_tracking_set_eskf_doppler_alpha(double alpha);
+	double gps_tracking_get_eskf_doppler_alpha(void);
 	void trck_intr_handler(volatile gps_trck_t* const trck_ip, volatile gps_frame_t *gps_frame_parsed, volatile int unsigned gps_subframe[10], unsigned char trck_ip_no);
 
 

soc/software/gps_system/header/gps/gps_receiver.h

@@ -38,4 +38,9 @@ bool gps_receiver_solve_ready_epoch(
 uint64_t gps_receiver_status_ticks(void);
 uint64_t gps_receiver_status_ticks_per_second(void);
 
+/* Select the low-latency Doppler EWMA used only by velocity WLS/ESKF.
+ * PPS keeps its independent fixed low-noise path. */
+void gps_receiver_set_eskf_doppler_alpha(double alpha);
+double gps_receiver_get_eskf_doppler_alpha(void);
+
 #endif

soc/software/gps_system/header/gps/gps_tracking_measurement.h

@@ -6,6 +6,8 @@
 
 #include "gps/gps_ip_defines.h"
 
+#define GPS_TRACK_PPS_DOPPLER_ALPHA 0.05
+
 typedef struct {
 	uint32_t prn;
 	uint32_t sequence;
@@ -17,9 +19,12 @@ typedef struct {
 	int32_t cn0_sum_q;
 	uint64_t cn0_wbp;
 	unsigned int cn0_sample_count;
-	/* Raw coherent 20 ms carrier snapshot used by velocity WLS/ESKF. */
+	/* Raw coherent 20 ms carrier snapshot retained for diagnostics. */
 	double doppler_hz;
 	double pseudorange_rate_mps;
+	/* Motion-adaptive low-latency path published to velocity WLS/ESKF. */
+	double eskf_doppler_hz;
+	double eskf_pseudorange_rate_mps;
 	/* Slow software IIR path retained only for PPS bias-drift prediction. */
 	double filtered_doppler_hz;
 	double filtered_pseudorange_rate_mps;

soc/software/gps_system/src/adapters/gps_system_uart.c

@@ -115,7 +115,7 @@ void gps_system_uart_publish_periodic_fusion_status(
 
 	if(output->global_valid)
 	{
-		GPS_LOG(DEBUG_EVENTS, GPS_LOG_CAT_FUSION,
+		GPS_LOG(DEBUG_STATUS, GPS_LOG_CAT_FUSION,
 		        "state=%s lat=%.10lf lon=%.10lf height=%.3lf "
 		        "speed=%.3lf pos_nis=%.3lf vel_nis=%.3lf "
 		        "gps=%lu/%lu velocity=%lu/%lu recoveries=%lu "
@@ -142,7 +142,7 @@ void gps_system_uart_publish_periodic_fusion_status(
 		return;
 	}
 
-	GPS_LOG(DEBUG_EVENTS, GPS_LOG_CAT_FUSION,
+	GPS_LOG(DEBUG_STATUS, GPS_LOG_CAT_FUSION,
 	        "state=%s calibration_samples=%u gps=%lu/%lu recoveries=%lu "
 	        "imu=%lu fused_imu=%lu overflow=%lu missed=%lu\r\n",
 	        navigation_fusion_state_name(output->engine_state),

soc/software/gps_system/src/fusion/navigation_fusion.c

@@ -141,6 +141,8 @@ bool navigation_fusion_get_output(navigation_fusion_output_t* output)
 			sqrt(fmax(0.0, runtime->filter.covariance[axis][axis]));
 	}
 	output->speed_mps = eskf_speed_mps(&runtime->filter);
+	output->linear_acceleration_norm_mps2 =
+		runtime->motion.last_linear_accel_norm_mps2;
 	output->last_position_nis = runtime->filter.last_position_nis;
 	output->last_velocity_nis = runtime->filter.last_velocity_nis;
 	output->motion_state = runtime->motion.state;

soc/software/gps_system/src/gps/gps_interrupt_handlers.c

@@ -9,6 +9,7 @@
 #include <bsp/irq.h>
 #include <bsp/mmio.h>
 #include <bsp/plic.h>
+#include <math.h>
 #include <string.h>
 
 typedef enum {
@@ -91,9 +92,13 @@ static gps_external_irq_handler_t gps_external_irq_handler = NULL;
 	(((uint64_t)GPS_PPS_CLOCK_HZ * GPS_NAV_ABS_SAMPLE_SYNC_WINDOW_MS) / 1000u)
 #define GPS_NAV_HOLDOFF_LOCAL_TICKS \
 	(((uint64_t)BSP_CLINT_TIMEBASE_HZ * GPS_NAV_EPOCH_HOLDOFF_MS) / 1000u)
-#define GPS_TRACK_DOPPLER_SMOOTH_ALPHA 0.05
+#define GPS_TRACK_ESKF_DOPPLER_ALPHA_MIN 0.05
+#define GPS_TRACK_ESKF_DOPPLER_ALPHA_MAX 0.40
 #define GPS_NAV_TOW_SNAP_TOLERANCE_SEC 0.005
 
+static volatile double gps_tracking_eskf_doppler_alpha =
+	GPS_TRACK_ESKF_DOPPLER_ALPHA_MIN;
+
 _Static_assert(GPS_NAV_ABS_SAMPLE_SYNC_WINDOW_MS <
                (GPS_NAV_SOLVE_PERIOD_MS / 2u),
                "NAV capture window must be below half the solve period");
@@ -112,6 +117,22 @@ static unsigned int gps_mask_count(uint32_t mask)
 	return count;
 }
 
+void gps_tracking_set_eskf_doppler_alpha(double alpha)
+{
+	if(!isfinite(alpha))
+	{
+		return;
+	}
+	gps_tracking_eskf_doppler_alpha = fmax(
+		GPS_TRACK_ESKF_DOPPLER_ALPHA_MIN,
+		fmin(GPS_TRACK_ESKF_DOPPLER_ALPHA_MAX, alpha));
+}
+
+double gps_tracking_get_eskf_doppler_alpha(void)
+{
+	return gps_tracking_eskf_doppler_alpha;
+}
+
 static double gps_correct_abs_sample(uint32_t abs_sample, uint32_t rem_code_phase)
 {
 	return (double)abs_sample - ((double)rem_code_phase / CODE_FREQ_BASIS);
@@ -157,12 +178,19 @@ static void gps_update_tracking_measurement_isr(
 		 * 0.4 s time constant while retaining real receiver dynamics.
 		 */
 		measurement.filtered_doppler_hz =
-			GPS_TRACK_DOPPLER_SMOOTH_ALPHA * measurement.doppler_hz +
-			(1.0 - GPS_TRACK_DOPPLER_SMOOTH_ALPHA) *
+			GPS_TRACK_PPS_DOPPLER_ALPHA * measurement.doppler_hz +
+			(1.0 - GPS_TRACK_PPS_DOPPLER_ALPHA) *
 			previous->filtered_doppler_hz;
 		measurement.filtered_pseudorange_rate_mps =
 			gps_tracking_doppler_to_range_rate_mps(
 				measurement.filtered_doppler_hz);
+		double eskf_alpha = gps_tracking_eskf_doppler_alpha;
+		measurement.eskf_doppler_hz =
+			eskf_alpha * measurement.doppler_hz +
+			(1.0 - eskf_alpha) * previous->eskf_doppler_hz;
+		measurement.eskf_pseudorange_rate_mps =
+			gps_tracking_doppler_to_range_rate_mps(
+				measurement.eskf_doppler_hz);
 	}
 	measurement.local_timestamp_ticks = local_timestamp_ticks;
 	gps_latest_tracking_measurement[tracking_index] = measurement;

soc/software/gps_system/src/gps/gps_ip.c

@@ -69,11 +69,25 @@ static bool gps_pps_reference_svid_valid;
 static unsigned int gps_pps_reference_svid;
 static bool gps_pps_filter_reference_svid_valid;
 static unsigned int gps_pps_filter_reference_svid;
+#if GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES > 0
+static uint64_t gps_pps_predictor_ab_update_counter;
+#endif
 
 #if !defined(GPS_PPS_STATUS_LOG_INTERVAL) || (GPS_PPS_STATUS_LOG_INTERVAL < 1)
 #error "GPS_PPS_STATUS_LOG_INTERVAL must be at least one"
 #endif
 
+#if !defined(GPS_PPS_DOPPLER_PREDICTOR_ENABLE) || \
+	((GPS_PPS_DOPPLER_PREDICTOR_ENABLE != 0) && \
+	 (GPS_PPS_DOPPLER_PREDICTOR_ENABLE != 1))
+#error "GPS_PPS_DOPPLER_PREDICTOR_ENABLE must be zero or one"
+#endif
+
+#if !defined(GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES) || \
+	(GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES < 0)
+#error "GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES must be zero or positive"
+#endif
+
 volatile uint64_t gps_systick_ticks = 0;
 
 static void gps_init_acq_tables(void)
@@ -854,6 +868,9 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 	bool pps_clock_bias_drift_valid = false;
 	double pps_clock_bias_drift_mps = 0.0;
 	bool pps_velocity_valid = false;
+	double eskf_doppler_alpha =
+		gps_tracking_get_eskf_doppler_alpha();
+	double pps_velocity_speed_mps = NAN;
 	double pps_velocity_residual_rms_mps = 0.0;
 	uint32_t pps_velocity_excluded_row_mask = 0u;
 	gps_nav_solution_t solution;
@@ -964,6 +981,13 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 	}
 	if(ok && solution.solution_valid)
 	{
+		double reference_noise_ratio =
+			eskf_doppler_alpha *
+			(2.0 - GPS_TRACK_PPS_DOPPLER_ALPHA) /
+			(GPS_TRACK_PPS_DOPPLER_ALPHA *
+			 (2.0 - eskf_doppler_alpha));
+		double eskf_cn0_penalty_db =
+			10.0 * log10(fmax(1.0, reference_noise_ratio));
 		double satellite_positions_array[GPS_TRCK_IP_COUNT][3];
 		double satellite_velocities_array[GPS_TRCK_IP_COUNT][3];
 		gps_tracking_measurement_t
@@ -978,6 +1002,12 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 					velocities->matrix[row][component];
 			}
 			velocity_measurements[row] = measurements[row];
+			velocity_measurements[row].doppler_hz =
+				measurements[row].eskf_doppler_hz;
+			velocity_measurements[row].pseudorange_rate_mps =
+				measurements[row].eskf_pseudorange_rate_mps;
+			velocity_measurements[row].cn0_dbhz -=
+				eskf_cn0_penalty_db;
 			if((solution.used_row_mask & (1u << row)) == 0u)
 			{
 				velocity_measurements[row].valid = false;
@@ -1011,10 +1041,13 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 		/*
 		 * PPS keeps the existing slow Doppler path as a low-noise derivative
 		 * predictor for the position-WLS reference datum.  This result is not
-		 * published to fusion; fusion receives the raw robust solution above.
+		 * published to fusion; fusion receives the adaptive low-latency
+		 * solution above.
 		 */
 		for(unsigned int row = 0u; row < satellite_count; row++)
 		{
+			velocity_measurements[row].cn0_dbhz =
+				measurements[row].cn0_dbhz;
 			velocity_measurements[row].doppler_hz =
 				measurements[row].filtered_doppler_hz;
 			velocity_measurements[row].pseudorange_rate_mps =
@@ -1037,6 +1070,10 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 			&pps_velocity_excluded_row_mask);
 		if(pps_velocity_valid)
 		{
+			pps_velocity_speed_mps =
+				sqrt(pps_velocity_ecef_mps[0] * pps_velocity_ecef_mps[0] +
+				     pps_velocity_ecef_mps[1] * pps_velocity_ecef_mps[1] +
+				     pps_velocity_ecef_mps[2] * pps_velocity_ecef_mps[2]);
 			pps_clock_bias_drift_valid =
 				gps_pps_reference_bias_drift(
 					solution.ecef_m,
@@ -1050,8 +1087,8 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 		   (pps_velocity_excluded_row_mask != 0u))
 		{
 			GPS_LOG(DEBUG_EVENTS, GPS_LOG_CAT_NAV,
-			        "velocity FDE raw_mask=0x%02lx pps_mask=0x%02lx "
-			        "raw_rms=%.3lf pps_rms=%.3lf\r\n",
+			        "velocity FDE adaptive_mask=0x%02lx pps_mask=0x%02lx "
+			        "adaptive_rms=%.3lf pps_rms=%.3lf\r\n",
 			        (unsigned long)solution.velocity_excluded_row_mask,
 			        (unsigned long)pps_velocity_excluded_row_mask,
 			        solution.velocity_residual_rms_mps,
@@ -1178,11 +1215,21 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 		}
 		double filtered_clock_bias_m = 0.0;
 		double clock_innovation_m = 0.0;
+		bool pps_predictor_enabled =
+			(GPS_PPS_DOPPLER_PREDICTOR_ENABLE != 0) &&
+			pps_clock_bias_drift_valid;
+#if GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES > 0
+		pps_predictor_enabled =
+			(((gps_pps_predictor_ab_update_counter /
+			   GPS_PPS_DOPPLER_PREDICTOR_AB_UPDATES) & 1u) != 0u) &&
+			pps_clock_bias_drift_valid;
+		gps_pps_predictor_ab_update_counter++;
+#endif
 		gps_pps_time_filter_result_t filter_result =
 			gps_pps_filter_clock_bias(
 				pps_reference_counter,
 				solution.clock_bias_m,
-				pps_clock_bias_drift_valid,
+				pps_predictor_enabled,
 				pps_clock_bias_drift_mps,
 				solution.tdop,
 				&filtered_clock_bias_m,
@@ -1244,7 +1291,10 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 			        "PPS profile=%s mode=%s locked=%u tdop=%.2lf gdop=%.2lf "
 			        "clock_sigma=%.2lf cn0=%.1lf/%.1lf innovation=%.2lfm "
 			        "raw_bias=%.3lfm filtered_bias=%.3lfm "
-			        "clock_drift=%.3lfmps bias_drift=%.3lfmps ref_svid=%u "
+			        "clock_drift=%.3lfmps bias_drift=%.3lfmps "
+			        "predictor=%u eskf_alpha=%.2lf "
+			        "eskf_v=%.3lf/%.3lf/0x%02lx "
+			        "pps_v=%.3lf/%.3lf/0x%02lx ref_svid=%u "
 			        "capture_corr=%.2lfns "
 			        "hw_phase=%.2lfns rate_cmd=%.3lfppm integ=%.3lfppm "
 			        "pulse=%u seq=%u status=0x%03x\r\n",
@@ -1261,6 +1311,14 @@ static bool nav_software_from_snapshot(const gps_ephemeris_t* ephemeris,
 			        filtered_clock_bias_m,
 			        solution.clock_drift_mps,
 			        pps_clock_bias_drift_mps,
+			        pps_predictor_enabled ? 1u : 0u,
+			        eskf_doppler_alpha,
+			        solution.speed_mps,
+			        solution.velocity_residual_rms_mps,
+			        (unsigned long)solution.velocity_excluded_row_mask,
+			        pps_velocity_speed_mps,
+			        pps_velocity_residual_rms_mps,
+			        (unsigned long)pps_velocity_excluded_row_mask,
 			        ephemeris[reference_index].SVID,
 			        pps_capture_correction_sec * 1.0e9,
 			        hardware_phase_ns, rate_command_ppm, integrator_ppm,

soc/software/gps_system/src/gps/gps_receiver.c

@@ -42,3 +42,13 @@ uint64_t gps_receiver_status_ticks_per_second(void)
 {
 	return GPS_SYSTICK_HZ;
 }
+
+void gps_receiver_set_eskf_doppler_alpha(double alpha)
+{
+	gps_tracking_set_eskf_doppler_alpha(alpha);
+}
+
+double gps_receiver_get_eskf_doppler_alpha(void)
+{
+	return gps_tracking_get_eskf_doppler_alpha();
+}

soc/software/gps_system/src/gps/gps_tracking_measurement.c

@@ -141,6 +141,10 @@ bool gps_tracking_measurement_read(
 			measurement_out->doppler_hz;
 		measurement_out->filtered_pseudorange_rate_mps =
 			measurement_out->pseudorange_rate_mps;
+		measurement_out->eskf_doppler_hz =
+			measurement_out->doppler_hz;
+		measurement_out->eskf_pseudorange_rate_mps =
+			measurement_out->pseudorange_rate_mps;
 
 		unsigned int version =
 			meta >> GPS_TRCK_MEAS_META_VERSION_SHIFT;
@@ -156,6 +160,8 @@ bool gps_tracking_measurement_read(
 			cn0_valid &&
 			isfinite(measurement_out->doppler_hz) &&
 			isfinite(measurement_out->pseudorange_rate_mps) &&
+			isfinite(measurement_out->eskf_doppler_hz) &&
+			isfinite(measurement_out->eskf_pseudorange_rate_mps) &&
 			isfinite(measurement_out->filtered_doppler_hz) &&
 			isfinite(measurement_out->filtered_pseudorange_rate_mps);
 		return measurement_out->valid;

soc/software/gps_system/tests/test_gps_pps_time_filter.c

@@ -138,6 +138,99 @@ static void test_bias_ramp_without_doppler_uses_bounded_fallback(void)
 	assert(sqrt(squared_error_sum / (double)tracked) < 45.0);
 }
 
+static void test_board_calibrated_doppler_predictor_beats_fallback(void)
+{
+	/* Values measured on Genesys2 on 2026-07-26: clock-bias sigma was
+	 * 15.87 m and reference-datum drift was about 291.75 m/s.  Feed the
+	 * exact same deterministic WLS noise to two filters so this is a true
+	 * predictor on/off A/B, not two unrelated Monte-Carlo runs. */
+	static const double bias_noise_m[] = {
+		8.0, -18.0, 12.0, -7.0, 21.0, -14.0, 5.0, -25.0,
+		16.0, -3.0, 10.0, -20.0, 6.0, 24.0, -11.0, 2.0
+	};
+	static const double drift_noise_mps[] = {
+		1.8, -3.2, 4.1, -2.4, 0.7, 3.5, -4.3, 2.6,
+		-1.1, 4.6, -2.8, 1.5, -3.7, 2.2, -0.4, 3.0
+	};
+	gps_pps_time_filter_t aided;
+	gps_pps_time_filter_t fallback;
+	gps_pps_time_filter_init(&aided);
+	gps_pps_time_filter_init(&fallback);
+
+	double aided_squared_error_sum = 0.0;
+	double fallback_squared_error_sum = 0.0;
+	unsigned int tracked = 0u;
+	for(unsigned int update = 0u; update < 900u; update++)
+	{
+		double time_sec = 0.2 * (double)update;
+		double long_omega = 2.0 * 3.14159265358979323846 / 75.0;
+		double short_omega = 2.0 * 3.14159265358979323846 / 19.0;
+		double varying_bias_m =
+			5.0 * (1.0 - cos(long_omega * time_sec)) / long_omega +
+			2.0 * (1.0 - cos(short_omega * time_sec)) / short_omega;
+		double true_drift_mps =
+			291.75 + 5.0 * sin(long_omega * time_sec) +
+			2.0 * sin(short_omega * time_sec);
+		double true_bias_m =
+			159624.654 + 291.75 * time_sec + varying_bias_m;
+		double measured_bias_m = true_bias_m +
+			bias_noise_m[update %
+				(sizeof(bias_noise_m) / sizeof(bias_noise_m[0]))];
+		double aided_bias_m = 0.0;
+		double fallback_bias_m = 0.0;
+		double innovation_m = 0.0;
+		gps_pps_time_filter_result_t aided_result =
+			gps_pps_time_filter_update(
+				&aided,
+				(uint64_t)llround(time_sec * COUNTER_HZ),
+				COUNTER_HZ,
+				measured_bias_m,
+				true,
+				true_drift_mps + drift_noise_mps[update %
+					(sizeof(drift_noise_mps) /
+					 sizeof(drift_noise_mps[0]))],
+				1.5,
+				1.0 / 32.0,
+				12u,
+				&aided_bias_m,
+				&innovation_m);
+		gps_pps_time_filter_result_t fallback_result =
+			gps_pps_time_filter_update(
+				&fallback,
+				(uint64_t)llround(time_sec * COUNTER_HZ),
+				COUNTER_HZ,
+				measured_bias_m,
+				false,
+				0.0,
+				1.5,
+				1.0 / 32.0,
+				12u,
+				&fallback_bias_m,
+				&innovation_m);
+		assert(aided_result != GPS_PPS_TIME_FILTER_REJECTED);
+		assert(fallback_result != GPS_PPS_TIME_FILTER_REJECTED);
+		if((update >= 300u) &&
+		   (aided_result == GPS_PPS_TIME_FILTER_TRACKING) &&
+		   (fallback_result == GPS_PPS_TIME_FILTER_TRACKING))
+		{
+			double aided_error_m = aided_bias_m - true_bias_m;
+			double fallback_error_m = fallback_bias_m - true_bias_m;
+			aided_squared_error_sum += aided_error_m * aided_error_m;
+			fallback_squared_error_sum +=
+				fallback_error_m * fallback_error_m;
+			tracked++;
+		}
+	}
+	assert(tracked > 550u);
+	double aided_rms_m = sqrt(aided_squared_error_sum / (double)tracked);
+	double fallback_rms_m =
+		sqrt(fallback_squared_error_sum / (double)tracked);
+	printf("board PPS bias RMS: Doppler=%.3f m fallback=%.3f m\n",
+	       aided_rms_m, fallback_rms_m);
+	assert(aided_rms_m < 8.0);
+	assert(aided_rms_m < 0.35 * fallback_rms_m);
+}
+
 static void test_reference_geometry_defines_bias_drift(void)
 {
 	const double receiver_position_m[3] = {0.0, 0.0, 0.0};
@@ -208,6 +301,7 @@ int main(void)
 	test_drift_prediction_rejects_bias_noise();
 	test_quality_gap_and_outlier_handling();
 	test_bias_ramp_without_doppler_uses_bounded_fallback();
+	test_board_calibrated_doppler_predictor_beats_fallback();
 	test_reference_geometry_defines_bias_drift();
 	test_reference_selection_is_stable();
 	puts("gps_pps_time_filter tests passed");

soc/software/gps_system/tests/test_gps_tracking_measurement.c

@@ -86,6 +86,14 @@ static void test_cn0_and_mailbox_decode(void)
 		measurement.filtered_pseudorange_rate_mps,
 		measurement.pseudorange_rate_mps,
 		1.0e-12));
+	assert(close_to(
+		measurement.eskf_doppler_hz,
+		measurement.doppler_hz,
+		1.0e-12));
+	assert(close_to(
+		measurement.eskf_pseudorange_rate_mps,
+		measurement.pseudorange_rate_mps,
+		1.0e-12));
 
 	registers.MEASUREMENT_META &=
 		~(1u << GPS_TRCK_MEAS_META_LOCK_POS);

soc/software/pps_python/README.md

@@ -125,6 +125,20 @@ grafik bu farkı açıkça gösterir.
 
 Raw `b/c` değerini PI phase error olarak doğrudan kullanmak doğru değildir.
 
+Klasik GNSS denklemindeki `c*delta_t_r` clock bias ile buradaki `b` aynı datum
+değildir: capture'ların ortak receiver zamanı önceden çıkarılmıştır. Doppler
+velocity WLS'nin dördüncü state'i uydulara ortak receiver clock/frequency
+drift'idir; fakat bu göreli `b` değerinin doğrudan türevi olarak kullanılmaz.
+PPS modeli datumun değişimini seçilen referans uydunun geometrik range-rate'i,
+broadcast satellite clock drift'i ve Doppler-WLS receiver velocity'sinden
+hesaplar:
+
+```text
+bias_drift =
+    -reference_geometric_range_rate
+    + c * reference_satellite_clock_drift
+```
+
 ## İlk HOW ve PPS başlangıcı
 
 `parse_subframe()` HOW Z-count alanını `6 s` ile çarpıp `tow.sec` yapar. Bu,
@@ -256,6 +270,16 @@ NaN, dört uydunun altına düşme, eşik sınırları ve histerezisi;
 `test_gps_pps_time_filter.c` drift prediction, gap/re-anchor ve hard-outlier
 reddini sınar.
 
+2026-07-26 Genesys2 logu ile kalibre edilen aynı-datum A/B testinde position
+WLS clock-bias gürültüsü `15.87 m`, referans-datum drift'i yaklaşık
+`291.75 m/s`, Doppler drift gürültüsü `3.47 m/s` ve oscillator hatası
+`1.592 ppm` olarak modele verildi. Linux C fixed-point testinde Doppler
+predictor clock-bias RMS'i `2.75 m`, yalnız son bias'i tutan fallback ise
+`21.22 m` verdi. Python modeli sekiz seed'de hem phase RMS hem 125 MHz grid'e
+quantize edilmiş edge-jitter p95 için predictor'un fallback'ten iyi kalmasını
+regresyon koşulu yapar. Kart status register phase'i fiziksel pin jitter'i
+değildir; `15-20 ns` çıkış hedefi son olarak scope/TIC ile ölçülmelidir.
+
 İki zaman eşiği bilinçli olarak ayrıdır: iki saniyelik watchdog gözlem yokken
 PPS validliğini holdover'a indirir; aynı referans SVID için Doppler-predicted
 clock-bias ve PI state'i 30 saniyeye kadar korunur. Modelde 15 saniyelik WLS

soc/software/pps_python/test_pps_adaptive.py

@@ -59,6 +59,90 @@ def noisy_observations(
 
 
 class AdaptivePpsTests(unittest.TestCase):
+    def test_board_calibrated_doppler_predictor_reduces_pps_error(self):
+        """Genesys2 WLS statistics: predictor-on must beat fallback-only."""
+        quality_metrics = QualityMetrics(
+            1.50, 2.92, 15.87, 40.3, 34.8, 0.35, 0.23, 7
+        )
+        aided_phase_rms = []
+        fallback_phase_rms = []
+        aided_edge_jitter = []
+        fallback_edge_jitter = []
+        for seed in range(8):
+            rng = random.Random(7300 + seed)
+            observations = []
+            for update in range(900):
+                time_s = 0.2 * update
+                long_omega = 2.0 * math.pi / 75.0
+                short_omega = 2.0 * math.pi / 19.0
+                varying_drift_mps = (
+                    5.0 * math.sin(long_omega * time_s)
+                    + 2.0 * math.sin(short_omega * time_s)
+                )
+                varying_bias_m = (
+                    5.0 * (1.0 - math.cos(long_omega * time_s)) / long_omega
+                    + 2.0 * (1.0 - math.cos(short_omega * time_s))
+                    / short_omega
+                )
+                # 15.87 m / c = 52.94 ns; 3.47 m/s is the measured
+                # board standard deviation of the reference bias drift.
+                noise_s = rng.gauss(0.0, 15.87 / 299_792_458.0)
+                if update % 113 == 0 and update != 0:
+                    noise_s += rng.choice((-1.0, 1.0)) * 120.0e-9
+                observations.append(
+                    Observation(
+                        time_s,
+                        noise_s,
+                        varying_drift_mps + rng.gauss(0.0, 3.47),
+                        quality_metrics,
+                        True,
+                        -291.75,
+                        1,
+                        varying_bias_m,
+                    )
+                )
+            aided = run_observations(
+                observations,
+                finish_time_s=180.0,
+                oscillator_ppm=1.592,
+            )
+            fallback = run_observations(
+                [
+                    Observation(
+                        item.time_s,
+                        item.timing_error_s,
+                        item.clock_drift_error_mps,
+                        item.quality,
+                        False,
+                        item.reference_range_rate_mps,
+                        item.reference_id,
+                        item.reference_datum_offset_m,
+                    )
+                    for item in observations
+                ],
+                finish_time_s=180.0,
+                oscillator_ppm=1.592,
+            )
+            aided_phase_rms.append(aided.phase_rms(after_s=60.0))
+            fallback_phase_rms.append(fallback.phase_rms(after_s=60.0))
+            aided_edge_jitter.append(
+                aided.one_second_edge_jitter_rms(after_s=60.0)
+            )
+            fallback_edge_jitter.append(
+                fallback.one_second_edge_jitter_rms(after_s=60.0)
+            )
+            self.assertEqual(aided.unlock_events, 0)
+
+        self.assertLess(
+            sum(aided_phase_rms) / len(aided_phase_rms),
+            0.35 * sum(fallback_phase_rms) / len(fallback_phase_rms),
+        )
+        self.assertLess(
+            sum(aided_edge_jitter) / len(aided_edge_jitter),
+            0.70 * sum(fallback_edge_jitter) / len(fallback_edge_jitter),
+        )
+        self.assertLess(max(aided_phase_rms), 30.0e-9)
+
     def test_quality_hysteresis_rejects_metric_chatter(self):
         selector = QualitySelector()
         for _ in range(7):