Make dt=0 on first step, simplify code

This commit is contained in:
Oleg Kalachev 2023-05-31 20:07:38 +03:00
parent 4160b8da07
commit 9a93367629
6 changed files with 29 additions and 51 deletions

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@ -13,50 +13,36 @@
void estimate()
{
if (dt == 0) {
return;
applyGyro();
applyAcc();
signalizeHorizontality();
}
void applyGyro()
{
// applying gyro
attitude *= Quaternion::fromAngularRates(rates * dt);
attitude.normalize();
}
// test should we apply acc
void applyAcc()
{
// test should we apply accelerometer gravity correction
float accNorm = acc.norm();
if (accNorm < ACC_MIN * ONE_G || accNorm > ACC_MAX * ONE_G) {
// use acc only when we're not accelerating
// use accelerometer only when we're not accelerating
return;
}
// calculate accelerometer correction
Vector up = attitude.rotate(Vector(0, 0, -1));
Vector accCorrDirection = Vector::angularRatesBetweenVectors(acc, up);
accCorrDirection.normalize();
if (!accCorrDirection.finite()) {
return;
}
Vector accCorr = accCorrDirection * Vector::angleBetweenVectors(up, acc) * dt * WEIGHT_ACC;
if (!accCorr.finite()) {
return; // TODO
}
// apply correction
attitude *= Quaternion::fromAngularRates(accCorr);
attitude.normalize();
if (!attitude.finite()) {
Serial.print("dt "); Serial.println(dt, 15);
Serial.print("up "); Serial.println(up);
Serial.print("acc "); Serial.println(acc);
Serial.print("acc norm "); Serial.println(acc.norm());
Serial.print("upp norm "); Serial.println(up.norm());
Serial.print("acc dot up "); Serial.println(Vector::dot(up, acc), 15);
Serial.print("acc cor ang "); Serial.println(Vector::angleBetweenVectors(up, acc), 15);
Serial.print("acc corr dir "); Serial.println(accCorrDirection);
Serial.print("acc cor "); Serial.println(accCorr);
Serial.print("att "); Serial.println(attitude);
}
}
void signalizeHorizontality()

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@ -62,5 +62,4 @@ void loop()
sendMavlink();
#endif
logData();
signalizeHorizontality();
}

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@ -20,21 +20,12 @@ public:
float update(float error, float dt)
{
if (!isfinite(error) || !isfinite(dt)) {
// TODO: brutal way to remove glitches
Serial.println("nan in error or dt");
return NAN;
}
if (dt > 0) {
// calculate integral if dt is valid
integral += error * dt;
if (isfinite(prevError)) {
if (isfinite(prevError) && dt > 0) {
// calculate derivative if both dt and prevError are valid
float _derivative = (error - prevError) / dt;
derivative = derivative * 0.8 + 0.2 * _derivative; // lpf WARNING:
}
}
prevError = error;

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@ -1,14 +1,16 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
#define FREQ_WINDOW 1
void step()
{
float now = micros() / 1000000.0;
dt = now - t; // dt is NAN on first step
dt = now - t;
t = now;
if (isnan(dt)) {
dt = 0; // assume dt to be zero on first step
}
computeLoopFreq();
}
@ -17,7 +19,7 @@ void computeLoopFreq()
static float windowStart = 0;
static uint32_t freq = 0;
freq++;
if (t - windowStart >= FREQ_WINDOW) {
if (t - windowStart >= 1) { // 1 second window
loopFreq = freq;
windowStart = t;
freq = 0;

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@ -13,10 +13,6 @@
#include <unistd.h>
#include <sys/poll.h>
using std::max;
using std::min;
using std::isfinite;
#define PI 3.1415926535897932384626433832795
#define DEG_TO_RAD 0.017453292519943295769236907684886
#define RAD_TO_DEG 57.295779513082320876798154814105

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@ -7,6 +7,7 @@
#include <stdio.h>
#include "vector.h"
#include "quaternion.h"
#include "Arduino.h"
#define RC_CHANNELS 6
@ -15,7 +16,7 @@
#define MOTOR_FRONT_RIGHT 2
#define MOTOR_REAR_RIGHT 1
float t;
float t = NAN;
float dt;
float loopFreq;
float motors[4];
@ -27,6 +28,9 @@ Quaternion attitude;
// declarations
void computeLoopFreq();
void applyGyro();
void applyAcc();
void signalizeHorizontality();
void control();
void interpretRC();
static void controlAttitude();