Continuous gyro bias estimation (#17)

Estimate gyro bias continuously instead of calibrating the gyro at startup.
This commit is contained in:
Oleg Kalachev 2025-03-29 12:21:40 +03:00 committed by GitHub
parent 117ae42d1b
commit 66a43ab246
No known key found for this signature in database
GPG Key ID: B5690EEEBB952194
7 changed files with 11 additions and 24 deletions

View File

@ -16,7 +16,6 @@ Do the following:
* **Make sure correct IMU model is chosen**. If using ICM-20948 board, change `MPU9250` to `ICM20948` everywhere in the `imu.ino` file.
* **Check if the CLI is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the CLI using QGroundControl (*Vehicle Setup* ⇒ *Analyze Tools**MAVLink Console*).
* **Configure QGroundControl correctly before connecting to the drone** if you use it to control the drone. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
* **Make sure you're not moving the drone several seconds after the power on**. The drone calibrates its gyroscope on the start so it should stay still for a while.
* **Check the IMU is working**. Perform `imu` command and check its output:
* The `status` field should be `OK`.
* The `rate` field should be about 1000 (Hz).

View File

@ -34,7 +34,6 @@ const char* motd =
"mot - show motor output\n"
"log - dump in-RAM log\n"
"cr - calibrate RC\n"
"cg - calibrate gyro\n"
"ca - calibrate accel\n"
"mfr, mfl, mrr, mrl - test motor (remove props)\n"
"reset - reset drone's state\n"
@ -124,8 +123,6 @@ void doCommand(String str, bool echo = false) {
dumpLog();
} else if (command == "cr") {
calibrateRC();
} else if (command == "cg") {
calibrateGyro();
} else if (command == "ca") {
calibrateAccel();
} else if (command == "mfr") {

View File

@ -29,7 +29,7 @@ void applyGyro() {
void applyAcc() {
// test should we apply accelerometer gravity correction
float accNorm = acc.norm();
bool landed = !motorsActive() && abs(accNorm - ONE_G) < ONE_G * 0.1f;
landed = !motorsActive() && abs(accNorm - ONE_G) < ONE_G * 0.1f;
if (!landed) return;

View File

@ -18,6 +18,7 @@ Vector gyro; // gyroscope data
Vector acc; // accelerometer data, m/s/s
Vector rates; // filtered angular rates, rad/s
Quaternion attitude; // estimated attitude
bool landed; // are we landed and stationary
float motors[4]; // normalized motors thrust in range [-1..1]
void setup() {

View File

@ -5,6 +5,7 @@
#include <SPI.h>
#include <MPU9250.h>
#include "lpf.h"
#include "util.h"
MPU9250 IMU(SPI);
@ -17,8 +18,6 @@ void setupIMU() {
print("Setup IMU\n");
IMU.begin();
configureIMU();
delay(500); // wait a bit before calibrating
calibrateGyro();
}
void configureIMU() {
@ -32,6 +31,7 @@ void readIMU() {
IMU.waitForData();
IMU.getGyro(gyro.x, gyro.y, gyro.z);
IMU.getAccel(acc.x, acc.y, acc.z);
calibrateGyroOnce();
// apply scale and bias
acc = (acc - accBias) / accScale;
gyro = gyro - gyroBias;
@ -47,21 +47,13 @@ void rotateIMU(Vector& data) {
// Axes orientation for various boards: https://github.com/okalachev/flixperiph#imu-axes-orientation
}
void calibrateGyro() {
const int samples = 1000;
print("Calibrating gyro, stand still\n");
IMU.setGyroRange(IMU.GYRO_RANGE_250DPS); // the most sensitive mode
void calibrateGyroOnce() {
static float landedTime = 0;
landedTime = landed ? landedTime + dt : 0;
if (landedTime < 2) return; // calibrate only if definitely stationary
gyroBias = Vector(0, 0, 0);
for (int i = 0; i < samples; i++) {
IMU.waitForData();
IMU.getGyro(gyro.x, gyro.y, gyro.z);
gyroBias = gyroBias + gyro;
}
gyroBias = gyroBias / samples;
printIMUCal();
configureIMU();
static LowPassFilter<Vector> gyroCalibrationFilter(0.001);
gyroBias = gyroCalibrationFilter.update(gyro);
}
void calibrateAccel() {

View File

@ -48,9 +48,6 @@ Parameter parameters[] = {
{"ACC_SCALE_X", &accScale.x},
{"ACC_SCALE_Y", &accScale.y},
{"ACC_SCALE_Z", &accScale.z},
{"GYRO_BIAS_X", &gyroBias.x},
{"GYRO_BIAS_Y", &gyroBias.y},
{"GYRO_BIAS_Z", &gyroBias.z},
// rc
{"RC_NEUTRAL_0", &channelNeutral[0]},
{"RC_NEUTRAL_1", &channelNeutral[1]},

View File

@ -21,6 +21,7 @@ Vector acc;
Vector gyro;
Vector rates;
Quaternion attitude;
bool landed;
// declarations
void step();