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authorGravatar Levi2021-01-10 22:09:56 -0700
committerGravatar Levi2021-01-10 22:09:56 -0700
commit7a3c884e39fccfbb498b855080bffabc9ce2e7f1 (patch)
tree5056f9406dec188439cb0deb87603498243a9412 /src/input_common/motion_input.cpp
parentMore forgetting... duh (diff)
parentMerge pull request #5229 from Morph1984/fullscreen-opt (diff)
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Merge remote-tracking branch 'upstream/master' into int-flags
Diffstat (limited to 'src/input_common/motion_input.cpp')
-rw-r--r--src/input_common/motion_input.cpp144
1 files changed, 132 insertions, 12 deletions
diff --git a/src/input_common/motion_input.cpp b/src/input_common/motion_input.cpp
index 22a849866..6a65f175e 100644
--- a/src/input_common/motion_input.cpp
+++ b/src/input_common/motion_input.cpp
@@ -2,13 +2,13 @@
2// Licensed under GPLv2 or any later version 2// Licensed under GPLv2 or any later version
3// Refer to the license.txt file included 3// Refer to the license.txt file included
4 4
5#include <random>
5#include "common/math_util.h" 6#include "common/math_util.h"
6#include "input_common/motion_input.h" 7#include "input_common/motion_input.h"
7 8
8namespace InputCommon { 9namespace InputCommon {
9 10
10MotionInput::MotionInput(f32 new_kp, f32 new_ki, f32 new_kd) 11MotionInput::MotionInput(f32 new_kp, f32 new_ki, f32 new_kd) : kp(new_kp), ki(new_ki), kd(new_kd) {}
11 : kp(new_kp), ki(new_ki), kd(new_kd), quat{{0, 0, -1}, 0} {}
12 12
13void MotionInput::SetAcceleration(const Common::Vec3f& acceleration) { 13void MotionInput::SetAcceleration(const Common::Vec3f& acceleration) {
14 accel = acceleration; 14 accel = acceleration;
@@ -16,8 +16,16 @@ void MotionInput::SetAcceleration(const Common::Vec3f& acceleration) {
16 16
17void MotionInput::SetGyroscope(const Common::Vec3f& gyroscope) { 17void MotionInput::SetGyroscope(const Common::Vec3f& gyroscope) {
18 gyro = gyroscope - gyro_drift; 18 gyro = gyroscope - gyro_drift;
19
20 // Auto adjust drift to minimize drift
21 if (!IsMoving(0.1f)) {
22 gyro_drift = (gyro_drift * 0.9999f) + (gyroscope * 0.0001f);
23 }
24
19 if (gyro.Length2() < gyro_threshold) { 25 if (gyro.Length2() < gyro_threshold) {
20 gyro = {}; 26 gyro = {};
27 } else {
28 only_accelerometer = false;
21 } 29 }
22} 30}
23 31
@@ -50,7 +58,7 @@ bool MotionInput::IsCalibrated(f32 sensitivity) const {
50} 58}
51 59
52void MotionInput::UpdateRotation(u64 elapsed_time) { 60void MotionInput::UpdateRotation(u64 elapsed_time) {
53 const f32 sample_period = elapsed_time / 1000000.0f; 61 const auto sample_period = static_cast<f32>(elapsed_time) / 1000000.0f;
54 if (sample_period > 0.1f) { 62 if (sample_period > 0.1f) {
55 return; 63 return;
56 } 64 }
@@ -66,9 +74,9 @@ void MotionInput::UpdateOrientation(u64 elapsed_time) {
66 f32 q2 = quat.xyz[0]; 74 f32 q2 = quat.xyz[0];
67 f32 q3 = quat.xyz[1]; 75 f32 q3 = quat.xyz[1];
68 f32 q4 = quat.xyz[2]; 76 f32 q4 = quat.xyz[2];
69 const f32 sample_period = elapsed_time / 1000000.0f; 77 const auto sample_period = static_cast<f32>(elapsed_time) / 1000000.0f;
70 78
71 // ignore invalid elapsed time 79 // Ignore invalid elapsed time
72 if (sample_period > 0.1f) { 80 if (sample_period > 0.1f) {
73 return; 81 return;
74 } 82 }
@@ -80,6 +88,13 @@ void MotionInput::UpdateOrientation(u64 elapsed_time) {
80 rad_gyro.y = -swap; 88 rad_gyro.y = -swap;
81 rad_gyro.z = -rad_gyro.z; 89 rad_gyro.z = -rad_gyro.z;
82 90
91 // Clear gyro values if there is no gyro present
92 if (only_accelerometer) {
93 rad_gyro.x = 0;
94 rad_gyro.y = 0;
95 rad_gyro.z = 0;
96 }
97
83 // Ignore drift correction if acceleration is not reliable 98 // Ignore drift correction if acceleration is not reliable
84 if (accel.Length() >= 0.75f && accel.Length() <= 1.25f) { 99 if (accel.Length() >= 0.75f && accel.Length() <= 1.25f) {
85 const f32 ax = -normal_accel.x; 100 const f32 ax = -normal_accel.x;
@@ -92,8 +107,11 @@ void MotionInput::UpdateOrientation(u64 elapsed_time) {
92 const f32 vz = q1 * q1 - q2 * q2 - q3 * q3 + q4 * q4; 107 const f32 vz = q1 * q1 - q2 * q2 - q3 * q3 + q4 * q4;
93 108
94 // Error is cross product between estimated direction and measured direction of gravity 109 // Error is cross product between estimated direction and measured direction of gravity
95 const Common::Vec3f new_real_error = {az * vx - ax * vz, ay * vz - az * vy, 110 const Common::Vec3f new_real_error = {
96 ax * vy - ay * vx}; 111 az * vx - ax * vz,
112 ay * vz - az * vy,
113 ax * vy - ay * vx,
114 };
97 115
98 derivative_error = new_real_error - real_error; 116 derivative_error = new_real_error - real_error;
99 real_error = new_real_error; 117 real_error = new_real_error;
@@ -106,9 +124,22 @@ void MotionInput::UpdateOrientation(u64 elapsed_time) {
106 } 124 }
107 125
108 // Apply feedback terms 126 // Apply feedback terms
109 rad_gyro += kp * real_error; 127 if (!only_accelerometer) {
110 rad_gyro += ki * integral_error; 128 rad_gyro += kp * real_error;
111 rad_gyro += kd * derivative_error; 129 rad_gyro += ki * integral_error;
130 rad_gyro += kd * derivative_error;
131 } else {
132 // Give more weight to accelerometer values to compensate for the lack of gyro
133 rad_gyro += 35.0f * kp * real_error;
134 rad_gyro += 10.0f * ki * integral_error;
135 rad_gyro += 10.0f * kd * derivative_error;
136
137 // Emulate gyro values for games that need them
138 gyro.x = -rad_gyro.y;
139 gyro.y = rad_gyro.x;
140 gyro.z = -rad_gyro.z;
141 UpdateRotation(elapsed_time);
142 }
112 } 143 }
113 144
114 const f32 gx = rad_gyro.y; 145 const f32 gx = rad_gyro.y;
@@ -159,18 +190,49 @@ Common::Vec3f MotionInput::GetRotations() const {
159 return rotations; 190 return rotations;
160} 191}
161 192
193Input::MotionStatus MotionInput::GetMotion() const {
194 const Common::Vec3f gyroscope = GetGyroscope();
195 const Common::Vec3f accelerometer = GetAcceleration();
196 const Common::Vec3f rotation = GetRotations();
197 const std::array<Common::Vec3f, 3> orientation = GetOrientation();
198 return {accelerometer, gyroscope, rotation, orientation};
199}
200
201Input::MotionStatus MotionInput::GetRandomMotion(int accel_magnitude, int gyro_magnitude) const {
202 std::random_device device;
203 std::mt19937 gen(device());
204 std::uniform_int_distribution<s16> distribution(-1000, 1000);
205 const Common::Vec3f gyroscope{
206 static_cast<f32>(distribution(gen)) * 0.001f,
207 static_cast<f32>(distribution(gen)) * 0.001f,
208 static_cast<f32>(distribution(gen)) * 0.001f,
209 };
210 const Common::Vec3f accelerometer{
211 static_cast<f32>(distribution(gen)) * 0.001f,
212 static_cast<f32>(distribution(gen)) * 0.001f,
213 static_cast<f32>(distribution(gen)) * 0.001f,
214 };
215 constexpr Common::Vec3f rotation;
216 constexpr std::array orientation{
217 Common::Vec3f{1.0f, 0.0f, 0.0f},
218 Common::Vec3f{0.0f, 1.0f, 0.0f},
219 Common::Vec3f{0.0f, 0.0f, 1.0f},
220 };
221 return {accelerometer * accel_magnitude, gyroscope * gyro_magnitude, rotation, orientation};
222}
223
162void MotionInput::ResetOrientation() { 224void MotionInput::ResetOrientation() {
163 if (!reset_enabled) { 225 if (!reset_enabled || only_accelerometer) {
164 return; 226 return;
165 } 227 }
166 if (!IsMoving(0.5f) && accel.z <= -0.9f) { 228 if (!IsMoving(0.5f) && accel.z <= -0.9f) {
167 ++reset_counter; 229 ++reset_counter;
168 if (reset_counter > 900) { 230 if (reset_counter > 900) {
169 // TODO: calculate quaternion from gravity vector
170 quat.w = 0; 231 quat.w = 0;
171 quat.xyz[0] = 0; 232 quat.xyz[0] = 0;
172 quat.xyz[1] = 0; 233 quat.xyz[1] = 0;
173 quat.xyz[2] = -1; 234 quat.xyz[2] = -1;
235 SetOrientationFromAccelerometer();
174 integral_error = {}; 236 integral_error = {};
175 reset_counter = 0; 237 reset_counter = 0;
176 } 238 }
@@ -178,4 +240,62 @@ void MotionInput::ResetOrientation() {
178 reset_counter = 0; 240 reset_counter = 0;
179 } 241 }
180} 242}
243
244void MotionInput::SetOrientationFromAccelerometer() {
245 int iterations = 0;
246 const f32 sample_period = 0.015f;
247
248 const auto normal_accel = accel.Normalized();
249
250 while (!IsCalibrated(0.01f) && ++iterations < 100) {
251 // Short name local variable for readability
252 f32 q1 = quat.w;
253 f32 q2 = quat.xyz[0];
254 f32 q3 = quat.xyz[1];
255 f32 q4 = quat.xyz[2];
256
257 Common::Vec3f rad_gyro;
258 const f32 ax = -normal_accel.x;
259 const f32 ay = normal_accel.y;
260 const f32 az = -normal_accel.z;
261
262 // Estimated direction of gravity
263 const f32 vx = 2.0f * (q2 * q4 - q1 * q3);
264 const f32 vy = 2.0f * (q1 * q2 + q3 * q4);
265 const f32 vz = q1 * q1 - q2 * q2 - q3 * q3 + q4 * q4;
266
267 // Error is cross product between estimated direction and measured direction of gravity
268 const Common::Vec3f new_real_error = {
269 az * vx - ax * vz,
270 ay * vz - az * vy,
271 ax * vy - ay * vx,
272 };
273
274 derivative_error = new_real_error - real_error;
275 real_error = new_real_error;
276
277 rad_gyro += 10.0f * kp * real_error;
278 rad_gyro += 5.0f * ki * integral_error;
279 rad_gyro += 10.0f * kd * derivative_error;
280
281 const f32 gx = rad_gyro.y;
282 const f32 gy = rad_gyro.x;
283 const f32 gz = rad_gyro.z;
284
285 // Integrate rate of change of quaternion
286 const f32 pa = q2;
287 const f32 pb = q3;
288 const f32 pc = q4;
289 q1 = q1 + (-q2 * gx - q3 * gy - q4 * gz) * (0.5f * sample_period);
290 q2 = pa + (q1 * gx + pb * gz - pc * gy) * (0.5f * sample_period);
291 q3 = pb + (q1 * gy - pa * gz + pc * gx) * (0.5f * sample_period);
292 q4 = pc + (q1 * gz + pa * gy - pb * gx) * (0.5f * sample_period);
293
294 quat.w = q1;
295 quat.xyz[0] = q2;
296 quat.xyz[1] = q3;
297 quat.xyz[2] = q4;
298 quat = quat.Normalized();
299 }
300}
181} // namespace InputCommon 301} // namespace InputCommon