feat(gps): expose ESKF build profiles and 460800 UART

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2026-07-25 19:39:36 +03:00
parent ecbb8d0b68
commit 49b8609bb4
16 changed files with 393 additions and 39 deletions
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@@ -86,6 +86,93 @@ make -C soc/software app APP=gps_system
make -C targets/fpga/vcu118 debug-load APP=gps_system
```
## GPS Firmware Profilleri: ESKF ve GPS-only
`gps_system` varsayilan olarak ESKF acik (`GPS_ESKF_ENABLE=1`) ve UART
`460800` baud olacak sekilde derlenir. Kok Makefile'in kart varsayilani VCU118
oldugu icin Genesys2 komutlarinda `FPGA_BOARD=genesys2` acikca yazilmalidir.
TDK ICM42688 + GPS + ESKF iceren birlesik Genesys2 MCS/BIN:
```sh
make FPGA_BOARD=genesys2 APP=gps_system \
GPS_ESKF_ENABLE=1 IMU_SENSOR=tdk fpga-mcs
```
Yalniz GPS acquisition/tracking, WLS, Doppler velocity ve PPS calistiran;
IMU/ESKF baslatmayan firmware:
```sh
make FPGA_BOARD=genesys2 APP=gps_system \
GPS_ESKF_ENABLE=0 fpga-mcs
```
`GPS_ESKF_ENABLE` verilmezse deger `1`'dir. Iki komut ayni
`targets/fpga/genesys2/out/flash/genesys2_rocket.mcs` ve `.bin` yollarini
kullanir; ikinci build birincinin ciktisinin uzerine yazar. Iki profili
saklamak gerekiyorsa her build'den sonra dosyayi profil adiyla kopyalayin.
`fpga-mcs` mevcut `.bit` dosyasini kullanip bootloader ve uygulamayi yeniden
derler. Yalniz software profili veya baud degisikligi icin sentez gerekmez.
Tracking/PPS RTL veya Chisel degistiyse once:
```sh
make FPGA_BOARD=genesys2 APP=gps_system fpga-bitstream
make FPGA_BOARD=genesys2 APP=gps_system GPS_ESKF_ENABLE=1 \
IMU_SENSOR=tdk fpga-mcs
```
Firmware ve host UART dinleyicisinin varsayilani birlikte `460800`'dur:
```sh
make FPGA_BOARD=genesys2 fpga-uart
```
### Doppler, WLS ve ESKF veri yolu
```text
tracking loop, her 20 ms:
carrier Q7 + 20 prompt I/Q + wideband power + ABS_SAMPLE/code phase
-> sabit tracking snapshot
-> synchronizer + APB-domain atomik register + interrupt
-> C/N0 ve Doppler/range-rate donusumu
-> satellite velocity/clock-drift duzeltmeli C/N0-weighted velocity WLS
-> ECEF velocity + 3x3 covariance + receiver clock drift
-> ECEF->ENU adapter
-> ayri velocity NIS gate
-> ayni capture epoch'unda 15-state ESKF update
-> daha yeni IMU history replay
```
RTL Doppler veya C/N0 uzerinde IIR yapmaz; ham ve 20 ms sabit snapshot'i
software'e verir. Software ayni PRN icin C/N0'yi `alpha=0.2`, Doppler'i
`alpha=0.05` ile yumusatir. L1 range-rate
`-doppler_hz * c / 1575420000` ile hesaplanir. En az dort uyduyla cozulmus
velocity WLS state'i `[vx, vy, vz, receiver_clock_drift_mps]`'dir; uydu LOS
hizi ve broadcast satellite clock drift observation'dan ayrilir. C/N0,
range-rate agirligini belirler; post-fit residual gerekirse formal
covariance'i yalniz buyutur.
ESKF; ENU position/velocity, quaternion attitude, accel bias ve gyro bias
iceren 15 hata durumlu filtredir. Her timestamp'li IMU ornegi prediction'a
girer. Gecikmis GPS position ve Doppler velocity olcumleri kendi capture
epoch'unda uygulanir, ardindan daha yeni IMU history replay edilir. Position
ve velocity'nin ayri NIS kapilari vardir; kotu Doppler ayni epoch'taki gecerli
position update'ini iptal etmez. Durağanlik supervisor'u uygun oldugunda ZUPT
ve zero-gyro update uygular; GPS kesintisinde filtre sahte konum olcumu
uretmeden dead-reckoning yapar ve covariance buyur.
C/N0, geometri, WLS clock sigma, integrity ve Doppler residual metrikleri PPS
software'inin `acquire/precision/robust/holdover` profilini de secer. PPS
donanimi bu metrikleri dogrudan yorumlamaz; software v2.2 mailbox ile PI
`Kp/Ki`, slew ve lock esiklerini atomik olarak gunceller. Ayrintilar:
- `hardware/external/gps/rtl/trck_src/README.md`
- `soc/software/gps_system/README.md`
- `soc/software/fusion/README.md`
- `hardware/external/gps/rtl/pps/README.md`
- `soc/software/pps_python/README.md`
Alt girisler:
```sh