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@@ -1,307 +0,0 @@
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-// Copyright 2020 yuzu Emulator Project
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-// Licensed under GPLv2 or any later version
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-// Refer to the license.txt file included
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-
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-#include <random>
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-#include "common/math_util.h"
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-#include "input_common/motion_input.h"
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-
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-namespace InputCommon {
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-
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-MotionInput::MotionInput(f32 new_kp, f32 new_ki, f32 new_kd) : kp(new_kp), ki(new_ki), kd(new_kd) {}
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-
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-void MotionInput::SetAcceleration(const Common::Vec3f& acceleration) {
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- accel = acceleration;
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-}
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-
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-void MotionInput::SetGyroscope(const Common::Vec3f& gyroscope) {
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- gyro = gyroscope - gyro_drift;
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-
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- // Auto adjust drift to minimize drift
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- if (!IsMoving(0.1f)) {
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- gyro_drift = (gyro_drift * 0.9999f) + (gyroscope * 0.0001f);
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- }
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-
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- if (gyro.Length2() < gyro_threshold) {
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- gyro = {};
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- } else {
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- only_accelerometer = false;
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- }
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-}
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-
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-void MotionInput::SetQuaternion(const Common::Quaternion<f32>& quaternion) {
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- quat = quaternion;
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-}
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-
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-void MotionInput::SetGyroDrift(const Common::Vec3f& drift) {
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- gyro_drift = drift;
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-}
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-
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-void MotionInput::SetGyroThreshold(f32 threshold) {
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- gyro_threshold = threshold;
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-}
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-
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-void MotionInput::EnableReset(bool reset) {
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- reset_enabled = reset;
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-}
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-
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-void MotionInput::ResetRotations() {
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- rotations = {};
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-}
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-
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-bool MotionInput::IsMoving(f32 sensitivity) const {
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- return gyro.Length() >= sensitivity || accel.Length() <= 0.9f || accel.Length() >= 1.1f;
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-}
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-
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-bool MotionInput::IsCalibrated(f32 sensitivity) const {
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- return real_error.Length() < sensitivity;
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-}
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-
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-void MotionInput::UpdateRotation(u64 elapsed_time) {
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- const auto sample_period = static_cast<f32>(elapsed_time) / 1000000.0f;
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- if (sample_period > 0.1f) {
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- return;
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- }
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- rotations += gyro * sample_period;
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-}
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-
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-void MotionInput::UpdateOrientation(u64 elapsed_time) {
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- if (!IsCalibrated(0.1f)) {
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- ResetOrientation();
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- }
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- // Short name local variable for readability
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- f32 q1 = quat.w;
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- f32 q2 = quat.xyz[0];
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- f32 q3 = quat.xyz[1];
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- f32 q4 = quat.xyz[2];
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- const auto sample_period = static_cast<f32>(elapsed_time) / 1000000.0f;
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-
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- // Ignore invalid elapsed time
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- if (sample_period > 0.1f) {
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- return;
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- }
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-
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- const auto normal_accel = accel.Normalized();
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- auto rad_gyro = gyro * Common::PI * 2;
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- const f32 swap = rad_gyro.x;
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- rad_gyro.x = rad_gyro.y;
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- rad_gyro.y = -swap;
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- rad_gyro.z = -rad_gyro.z;
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-
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- // Clear gyro values if there is no gyro present
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- if (only_accelerometer) {
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- rad_gyro.x = 0;
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- rad_gyro.y = 0;
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- rad_gyro.z = 0;
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- }
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-
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- // Ignore drift correction if acceleration is not reliable
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- if (accel.Length() >= 0.75f && accel.Length() <= 1.25f) {
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- const f32 ax = -normal_accel.x;
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- const f32 ay = normal_accel.y;
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- const f32 az = -normal_accel.z;
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-
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- // Estimated direction of gravity
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- const f32 vx = 2.0f * (q2 * q4 - q1 * q3);
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- const f32 vy = 2.0f * (q1 * q2 + q3 * q4);
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- const f32 vz = q1 * q1 - q2 * q2 - q3 * q3 + q4 * q4;
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-
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- // Error is cross product between estimated direction and measured direction of gravity
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- const Common::Vec3f new_real_error = {
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- az * vx - ax * vz,
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- ay * vz - az * vy,
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- ax * vy - ay * vx,
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- };
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-
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- derivative_error = new_real_error - real_error;
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- real_error = new_real_error;
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-
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- // Prevent integral windup
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- if (ki != 0.0f && !IsCalibrated(0.05f)) {
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- integral_error += real_error;
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- } else {
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- integral_error = {};
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- }
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-
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- // Apply feedback terms
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- if (!only_accelerometer) {
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- rad_gyro += kp * real_error;
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- rad_gyro += ki * integral_error;
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- rad_gyro += kd * derivative_error;
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- } else {
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- // Give more weight to accelerometer values to compensate for the lack of gyro
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- rad_gyro += 35.0f * kp * real_error;
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- rad_gyro += 10.0f * ki * integral_error;
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- rad_gyro += 10.0f * kd * derivative_error;
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-
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- // Emulate gyro values for games that need them
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- gyro.x = -rad_gyro.y;
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- gyro.y = rad_gyro.x;
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- gyro.z = -rad_gyro.z;
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- UpdateRotation(elapsed_time);
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- }
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- }
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-
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- const f32 gx = rad_gyro.y;
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- const f32 gy = rad_gyro.x;
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- const f32 gz = rad_gyro.z;
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-
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- // Integrate rate of change of quaternion
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- const f32 pa = q2;
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- const f32 pb = q3;
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- const f32 pc = q4;
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- q1 = q1 + (-q2 * gx - q3 * gy - q4 * gz) * (0.5f * sample_period);
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- q2 = pa + (q1 * gx + pb * gz - pc * gy) * (0.5f * sample_period);
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- q3 = pb + (q1 * gy - pa * gz + pc * gx) * (0.5f * sample_period);
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- q4 = pc + (q1 * gz + pa * gy - pb * gx) * (0.5f * sample_period);
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-
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- quat.w = q1;
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- quat.xyz[0] = q2;
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- quat.xyz[1] = q3;
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- quat.xyz[2] = q4;
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- quat = quat.Normalized();
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-}
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-
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-std::array<Common::Vec3f, 3> MotionInput::GetOrientation() const {
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- const Common::Quaternion<float> quad{
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- .xyz = {-quat.xyz[1], -quat.xyz[0], -quat.w},
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- .w = -quat.xyz[2],
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- };
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- const std::array<float, 16> matrix4x4 = quad.ToMatrix();
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-
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- return {Common::Vec3f(matrix4x4[0], matrix4x4[1], -matrix4x4[2]),
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- Common::Vec3f(matrix4x4[4], matrix4x4[5], -matrix4x4[6]),
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- Common::Vec3f(-matrix4x4[8], -matrix4x4[9], matrix4x4[10])};
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-}
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-
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-Common::Vec3f MotionInput::GetAcceleration() const {
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- return accel;
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-}
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-
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-Common::Vec3f MotionInput::GetGyroscope() const {
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- return gyro;
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-}
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-
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-Common::Quaternion<f32> MotionInput::GetQuaternion() const {
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- return quat;
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-}
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-
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-Common::Vec3f MotionInput::GetRotations() const {
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- return rotations;
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-}
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-
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-Input::MotionStatus MotionInput::GetMotion() const {
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- const Common::Vec3f gyroscope = GetGyroscope();
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- const Common::Vec3f accelerometer = GetAcceleration();
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- const Common::Vec3f rotation = GetRotations();
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- const std::array<Common::Vec3f, 3> orientation = GetOrientation();
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- const Common::Quaternion<f32> quaternion = GetQuaternion();
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- return {accelerometer, gyroscope, rotation, orientation, quaternion};
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-}
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-
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-Input::MotionStatus MotionInput::GetRandomMotion(int accel_magnitude, int gyro_magnitude) const {
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- std::random_device device;
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- std::mt19937 gen(device());
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- std::uniform_int_distribution<s16> distribution(-1000, 1000);
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- const Common::Vec3f gyroscope{
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- static_cast<f32>(distribution(gen)) * 0.001f,
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- static_cast<f32>(distribution(gen)) * 0.001f,
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- static_cast<f32>(distribution(gen)) * 0.001f,
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- };
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- const Common::Vec3f accelerometer{
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- static_cast<f32>(distribution(gen)) * 0.001f,
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- static_cast<f32>(distribution(gen)) * 0.001f,
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- static_cast<f32>(distribution(gen)) * 0.001f,
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- };
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- constexpr Common::Vec3f rotation;
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- constexpr std::array orientation{
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- Common::Vec3f{1.0f, 0.0f, 0.0f},
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- Common::Vec3f{0.0f, 1.0f, 0.0f},
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- Common::Vec3f{0.0f, 0.0f, 1.0f},
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- };
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- constexpr Common::Quaternion<f32> quaternion{
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- {0.0f, 0.0f, 0.0f},
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- 1.0f,
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- };
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- return {accelerometer * accel_magnitude, gyroscope * gyro_magnitude, rotation, orientation,
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- quaternion};
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-}
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-
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-void MotionInput::ResetOrientation() {
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- if (!reset_enabled || only_accelerometer) {
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- return;
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- }
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- if (!IsMoving(0.5f) && accel.z <= -0.9f) {
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- ++reset_counter;
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- if (reset_counter > 900) {
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- quat.w = 0;
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- quat.xyz[0] = 0;
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- quat.xyz[1] = 0;
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- quat.xyz[2] = -1;
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- SetOrientationFromAccelerometer();
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- integral_error = {};
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- reset_counter = 0;
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- }
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- } else {
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- reset_counter = 0;
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- }
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-}
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-
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-void MotionInput::SetOrientationFromAccelerometer() {
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- int iterations = 0;
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- const f32 sample_period = 0.015f;
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-
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- const auto normal_accel = accel.Normalized();
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-
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- while (!IsCalibrated(0.01f) && ++iterations < 100) {
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- // Short name local variable for readability
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- f32 q1 = quat.w;
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- f32 q2 = quat.xyz[0];
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- f32 q3 = quat.xyz[1];
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- f32 q4 = quat.xyz[2];
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-
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- Common::Vec3f rad_gyro;
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- const f32 ax = -normal_accel.x;
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- const f32 ay = normal_accel.y;
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- const f32 az = -normal_accel.z;
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-
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- // Estimated direction of gravity
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- const f32 vx = 2.0f * (q2 * q4 - q1 * q3);
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- const f32 vy = 2.0f * (q1 * q2 + q3 * q4);
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- const f32 vz = q1 * q1 - q2 * q2 - q3 * q3 + q4 * q4;
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-
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- // Error is cross product between estimated direction and measured direction of gravity
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- const Common::Vec3f new_real_error = {
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- az * vx - ax * vz,
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- ay * vz - az * vy,
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- ax * vy - ay * vx,
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- };
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-
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- derivative_error = new_real_error - real_error;
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- real_error = new_real_error;
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-
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- rad_gyro += 10.0f * kp * real_error;
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- rad_gyro += 5.0f * ki * integral_error;
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- rad_gyro += 10.0f * kd * derivative_error;
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-
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- const f32 gx = rad_gyro.y;
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- const f32 gy = rad_gyro.x;
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- const f32 gz = rad_gyro.z;
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-
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- // Integrate rate of change of quaternion
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- const f32 pa = q2;
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- const f32 pb = q3;
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- const f32 pc = q4;
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- q1 = q1 + (-q2 * gx - q3 * gy - q4 * gz) * (0.5f * sample_period);
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- q2 = pa + (q1 * gx + pb * gz - pc * gy) * (0.5f * sample_period);
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- q3 = pb + (q1 * gy - pa * gz + pc * gx) * (0.5f * sample_period);
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- q4 = pc + (q1 * gz + pa * gy - pb * gx) * (0.5f * sample_period);
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-
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- quat.w = q1;
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- quat.xyz[0] = q2;
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- quat.xyz[1] = q3;
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- quat.xyz[2] = q4;
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- quat = quat.Normalized();
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- }
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-}
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-} // namespace InputCommon
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