1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 358 359 360 361 362 363 364 365 366 367 368 369 370 371 372 373 374 375 376 377 378 379 380 381 382 383 384 385 386 387 388 389 390 391 392 393 394 395 396 397 398 399 400 401 402 403 404 405 406 407 408 409 410 411 412 413 414 415 416 417 418 419 420 421 422 423 424 425 426 427 428 429 430 431 432 433 434 435 436 437 438 439 440 441 442 443 444 445 446 447 448 449 450 451 452 453 454 455 456 457 458 459 460 461 462 463 464 465 466 467 468 469 470 471 472 473 474 475 476 477 478 479 480 481 482 483 484 485 486 487 488 489 490 491 492 493 494 495 496 497 498 499 500 501 502 503 504 505 506 507 508 509 510 511 512 513 514 515 516 517 518 519 520 521 522 523 524 525 526 527 528 529 530 531 532 533 534 535 536 537 538 539 540 541 542 543 544 545 546 547 548 549 550 551 552 553 554 555 556 557 558 559 560 561 562 563 564 565
|
/*
* Copyright (C) 2011 The Android Open Source Project
*
* Licensed under the Apache License, Version 2.0 (the "License");
* you may not use this file except in compliance with the License.
* You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
#include <stdio.h>
#include <utils/Log.h>
#include "Fusion.h"
namespace android {
// -----------------------------------------------------------------------
/*==================== BEGIN FUSION SENSOR PARAMETER =========================*/
/* Note:
* If a platform uses software fusion, it is necessary to tune the following
* parameters to fit the hardware sensors prior to release.
*
* The DEFAULT_ parameters will be used in FUSION_9AXIS and FUSION_NOMAG mode.
* The GEOMAG_ parameters will be used in FUSION_NOGYRO mode.
*/
/*
* GYRO_VAR gives the measured variance of the gyro's output per
* Hz (or variance at 1 Hz). This is an "intrinsic" parameter of the gyro,
* which is independent of the sampling frequency.
*
* The variance of gyro's output at a given sampling period can be
* calculated as:
* variance(T) = GYRO_VAR / T
*
* The variance of the INTEGRATED OUTPUT at a given sampling period can be
* calculated as:
* variance_integrate_output(T) = GYRO_VAR * T
*/
static const float DEFAULT_GYRO_VAR = 1e-7; // (rad/s)^2 / Hz
static const float DEFAULT_GYRO_BIAS_VAR = 1e-12; // (rad/s)^2 / s (guessed)
static const float GEOMAG_GYRO_VAR = 1e-4; // (rad/s)^2 / Hz
static const float GEOMAG_GYRO_BIAS_VAR = 1e-8; // (rad/s)^2 / s (guessed)
/*
* Standard deviations of accelerometer and magnetometer
*/
static const float DEFAULT_ACC_STDEV = 0.015f; // m/s^2 (measured 0.08 / CDD 0.05)
static const float DEFAULT_MAG_STDEV = 0.1f; // uT (measured 0.7 / CDD 0.5)
static const float GEOMAG_ACC_STDEV = 0.05f; // m/s^2 (measured 0.08 / CDD 0.05)
static const float GEOMAG_MAG_STDEV = 0.1f; // uT (measured 0.7 / CDD 0.5)
/* ====================== END FUSION SENSOR PARAMETER ========================*/
static const float SYMMETRY_TOLERANCE = 1e-10f;
/*
* Accelerometer updates will not be performed near free fall to avoid
* ill-conditioning and div by zeros.
* Threshhold: 10% of g, in m/s^2
*/
static const float NOMINAL_GRAVITY = 9.81f;
static const float FREE_FALL_THRESHOLD = 0.1f * (NOMINAL_GRAVITY);
/*
* The geomagnetic-field should be between 30uT and 60uT.
* Fields strengths greater than this likely indicate a local magnetic
* disturbance which we do not want to update into the fused frame.
*/
static const float MAX_VALID_MAGNETIC_FIELD = 100; // uT
static const float MAX_VALID_MAGNETIC_FIELD_SQ =
MAX_VALID_MAGNETIC_FIELD*MAX_VALID_MAGNETIC_FIELD;
/*
* Values of the field smaller than this should be ignored in fusion to avoid
* ill-conditioning. This state can happen with anomalous local magnetic
* disturbances canceling the Earth field.
*/
static const float MIN_VALID_MAGNETIC_FIELD = 10; // uT
static const float MIN_VALID_MAGNETIC_FIELD_SQ =
MIN_VALID_MAGNETIC_FIELD*MIN_VALID_MAGNETIC_FIELD;
/*
* If the cross product of two vectors has magnitude squared less than this,
* we reject it as invalid due to alignment of the vectors.
* This threshold is used to check for the case where the magnetic field sample
* is parallel to the gravity field, which can happen in certain places due
* to magnetic field disturbances.
*/
static const float MIN_VALID_CROSS_PRODUCT_MAG = 1.0e-3;
static const float MIN_VALID_CROSS_PRODUCT_MAG_SQ =
MIN_VALID_CROSS_PRODUCT_MAG*MIN_VALID_CROSS_PRODUCT_MAG;
static const float SQRT_3 = 1.732f;
static const float WVEC_EPS = 1e-4f/SQRT_3;
// -----------------------------------------------------------------------
template <typename TYPE, size_t C, size_t R>
static mat<TYPE, R, R> scaleCovariance(
const mat<TYPE, C, R>& A,
const mat<TYPE, C, C>& P) {
// A*P*transpose(A);
mat<TYPE, R, R> APAt;
for (size_t r=0 ; r<R ; r++) {
for (size_t j=r ; j<R ; j++) {
double apat(0);
for (size_t c=0 ; c<C ; c++) {
double v(A[c][r]*P[c][c]*0.5);
for (size_t k=c+1 ; k<C ; k++)
v += A[k][r] * P[c][k];
apat += 2 * v * A[c][j];
}
APAt[j][r] = apat;
APAt[r][j] = apat;
}
}
return APAt;
}
template <typename TYPE, typename OTHER_TYPE>
static mat<TYPE, 3, 3> crossMatrix(const vec<TYPE, 3>& p, OTHER_TYPE diag) {
mat<TYPE, 3, 3> r;
r[0][0] = diag;
r[1][1] = diag;
r[2][2] = diag;
r[0][1] = p.z;
r[1][0] =-p.z;
r[0][2] =-p.y;
r[2][0] = p.y;
r[1][2] = p.x;
r[2][1] =-p.x;
return r;
}
template<typename TYPE, size_t SIZE>
class Covariance {
mat<TYPE, SIZE, SIZE> mSumXX;
vec<TYPE, SIZE> mSumX;
size_t mN;
public:
Covariance() : mSumXX(0.0f), mSumX(0.0f), mN(0) { }
void update(const vec<TYPE, SIZE>& x) {
mSumXX += x*transpose(x);
mSumX += x;
mN++;
}
mat<TYPE, SIZE, SIZE> operator()() const {
const float N = 1.0f / mN;
return mSumXX*N - (mSumX*transpose(mSumX))*(N*N);
}
void reset() {
mN = 0;
mSumXX = 0;
mSumX = 0;
}
size_t getCount() const {
return mN;
}
};
// -----------------------------------------------------------------------
Fusion::Fusion() {
Phi[0][1] = 0;
Phi[1][1] = 1;
Ba.x = 0;
Ba.y = 0;
Ba.z = 1;
Bm.x = 0;
Bm.y = 1;
Bm.z = 0;
x0 = 0;
x1 = 0;
init();
}
void Fusion::init(int mode) {
mInitState = 0;
mGyroRate = 0;
mCount[0] = 0;
mCount[1] = 0;
mCount[2] = 0;
mData = 0;
mMode = mode;
if (mMode != FUSION_NOGYRO) { //normal or game rotation
mParam.gyroVar = DEFAULT_GYRO_VAR;
mParam.gyroBiasVar = DEFAULT_GYRO_BIAS_VAR;
mParam.accStdev = DEFAULT_ACC_STDEV;
mParam.magStdev = DEFAULT_MAG_STDEV;
} else {
mParam.gyroVar = GEOMAG_GYRO_VAR;
mParam.gyroBiasVar = GEOMAG_GYRO_BIAS_VAR;
mParam.accStdev = GEOMAG_ACC_STDEV;
mParam.magStdev = GEOMAG_MAG_STDEV;
}
}
void Fusion::initFusion(const vec4_t& q, float dT)
{
// initial estimate: E{ x(t0) }
x0 = q;
x1 = 0;
// process noise covariance matrix: G.Q.Gt, with
//
// G = | -1 0 | Q = | q00 q10 |
// | 0 1 | | q01 q11 |
//
// q00 = sv^2.dt + 1/3.su^2.dt^3
// q10 = q01 = 1/2.su^2.dt^2
// q11 = su^2.dt
//
const float dT2 = dT*dT;
const float dT3 = dT2*dT;
// variance of integrated output at 1/dT Hz (random drift)
const float q00 = mParam.gyroVar * dT + 0.33333f * mParam.gyroBiasVar * dT3;
// variance of drift rate ramp
const float q11 = mParam.gyroBiasVar * dT;
const float q10 = 0.5f * mParam.gyroBiasVar * dT2;
const float q01 = q10;
GQGt[0][0] = q00; // rad^2
GQGt[1][0] = -q10;
GQGt[0][1] = -q01;
GQGt[1][1] = q11; // (rad/s)^2
// initial covariance: Var{ x(t0) }
// TODO: initialize P correctly
P = 0;
}
bool Fusion::hasEstimate() const {
return ((mInitState & MAG) || (mMode == FUSION_NOMAG)) &&
((mInitState & GYRO) || (mMode == FUSION_NOGYRO)) &&
(mInitState & ACC);
}
bool Fusion::checkInitComplete(int what, const vec3_t& d, float dT) {
if (hasEstimate())
return true;
if (what == ACC) {
mData[0] += d * (1/length(d));
mCount[0]++;
mInitState |= ACC;
if (mMode == FUSION_NOGYRO ) {
mGyroRate = dT;
}
} else if (what == MAG) {
mData[1] += d * (1/length(d));
mCount[1]++;
mInitState |= MAG;
} else if (what == GYRO) {
mGyroRate = dT;
mData[2] += d*dT;
mCount[2]++;
mInitState |= GYRO;
}
if (hasEstimate()) {
// Average all the values we collected so far
mData[0] *= 1.0f/mCount[0];
if (mMode != FUSION_NOMAG) {
mData[1] *= 1.0f/mCount[1];
}
mData[2] *= 1.0f/mCount[2];
// calculate the MRPs from the data collection, this gives us
// a rough estimate of our initial state
mat33_t R;
vec3_t up(mData[0]);
vec3_t east;
if (mMode != FUSION_NOMAG) {
east = normalize(cross_product(mData[1], up));
} else {
east = getOrthogonal(up);
}
vec3_t north(cross_product(up, east));
R << east << north << up;
const vec4_t q = matrixToQuat(R);
initFusion(q, mGyroRate);
}
return false;
}
void Fusion::handleGyro(const vec3_t& w, float dT) {
if (!checkInitComplete(GYRO, w, dT))
return;
predict(w, dT);
}
status_t Fusion::handleAcc(const vec3_t& a, float dT) {
if (!checkInitComplete(ACC, a, dT))
return BAD_VALUE;
// ignore acceleration data if we're close to free-fall
const float l = length(a);
if (l < FREE_FALL_THRESHOLD) {
return BAD_VALUE;
}
const float l_inv = 1.0f/l;
if ( mMode == FUSION_NOGYRO ) {
//geo mag
vec3_t w_dummy;
w_dummy = x1; //bias
predict(w_dummy, dT);
}
if ( mMode == FUSION_NOMAG) {
vec3_t m;
m = getRotationMatrix()*Bm;
update(m, Bm, mParam.magStdev);
}
vec3_t unityA = a * l_inv;
const float d = sqrtf(fabsf(l- NOMINAL_GRAVITY));
const float p = l_inv * mParam.accStdev*expf(d);
update(unityA, Ba, p);
return NO_ERROR;
}
status_t Fusion::handleMag(const vec3_t& m) {
if (!checkInitComplete(MAG, m))
return BAD_VALUE;
// the geomagnetic-field should be between 30uT and 60uT
// reject if too large to avoid spurious magnetic sources
const float magFieldSq = length_squared(m);
if (magFieldSq > MAX_VALID_MAGNETIC_FIELD_SQ) {
return BAD_VALUE;
} else if (magFieldSq < MIN_VALID_MAGNETIC_FIELD_SQ) {
// Also reject if too small since we will get ill-defined (zero mag)
// cross-products below
return BAD_VALUE;
}
// Orthogonalize the magnetic field to the gravity field, mapping it into
// tangent to Earth.
const vec3_t up( getRotationMatrix() * Ba );
const vec3_t east( cross_product(m, up) );
// If the m and up vectors align, the cross product magnitude will
// approach 0.
// Reject this case as well to avoid div by zero problems and
// ill-conditioning below.
if (length_squared(east) < MIN_VALID_CROSS_PRODUCT_MAG_SQ) {
return BAD_VALUE;
}
// If we have created an orthogonal magnetic field successfully,
// then pass it in as the update.
vec3_t north( cross_product(up, east) );
const float l_inv = 1 / length(north);
north *= l_inv;
update(north, Bm, mParam.magStdev*l_inv);
return NO_ERROR;
}
void Fusion::checkState() {
// P needs to stay positive semidefinite or the fusion diverges. When we
// detect divergence, we reset the fusion.
// TODO(braun): Instead, find the reason for the divergence and fix it.
if (!isPositiveSemidefinite(P[0][0], SYMMETRY_TOLERANCE) ||
!isPositiveSemidefinite(P[1][1], SYMMETRY_TOLERANCE)) {
ALOGW("Sensor fusion diverged; resetting state.");
P = 0;
}
}
vec4_t Fusion::getAttitude() const {
return x0;
}
vec3_t Fusion::getBias() const {
return x1;
}
mat33_t Fusion::getRotationMatrix() const {
return quatToMatrix(x0);
}
mat34_t Fusion::getF(const vec4_t& q) {
mat34_t F;
// This is used to compute the derivative of q
// F = | [q.xyz]x |
// | -q.xyz |
F[0].x = q.w; F[1].x =-q.z; F[2].x = q.y;
F[0].y = q.z; F[1].y = q.w; F[2].y =-q.x;
F[0].z =-q.y; F[1].z = q.x; F[2].z = q.w;
F[0].w =-q.x; F[1].w =-q.y; F[2].w =-q.z;
return F;
}
void Fusion::predict(const vec3_t& w, float dT) {
const vec4_t q = x0;
const vec3_t b = x1;
vec3_t we = w - b;
if (length(we) < WVEC_EPS) {
we = (we[0]>0.f)?WVEC_EPS:-WVEC_EPS;
}
// q(k+1) = O(we)*q(k)
// --------------------
//
// O(w) = | cos(0.5*||w||*dT)*I33 - [psi]x psi |
// | -psi' cos(0.5*||w||*dT) |
//
// psi = sin(0.5*||w||*dT)*w / ||w||
//
//
// P(k+1) = Phi(k)*P(k)*Phi(k)' + G*Q(k)*G'
// ----------------------------------------
//
// G = | -I33 0 |
// | 0 I33 |
//
// Phi = | Phi00 Phi10 |
// | 0 1 |
//
// Phi00 = I33
// - [w]x * sin(||w||*dt)/||w||
// + [w]x^2 * (1-cos(||w||*dT))/||w||^2
//
// Phi10 = [w]x * (1 - cos(||w||*dt))/||w||^2
// - [w]x^2 * (||w||*dT - sin(||w||*dt))/||w||^3
// - I33*dT
const mat33_t I33(1);
const mat33_t I33dT(dT);
const mat33_t wx(crossMatrix(we, 0));
const mat33_t wx2(wx*wx);
const float lwedT = length(we)*dT;
const float hlwedT = 0.5f*lwedT;
const float ilwe = 1.f/length(we);
const float k0 = (1-cosf(lwedT))*(ilwe*ilwe);
const float k1 = sinf(lwedT);
const float k2 = cosf(hlwedT);
const vec3_t psi(sinf(hlwedT)*ilwe*we);
const mat33_t O33(crossMatrix(-psi, k2));
mat44_t O;
O[0].xyz = O33[0]; O[0].w = -psi.x;
O[1].xyz = O33[1]; O[1].w = -psi.y;
O[2].xyz = O33[2]; O[2].w = -psi.z;
O[3].xyz = psi; O[3].w = k2;
Phi[0][0] = I33 - wx*(k1*ilwe) + wx2*k0;
Phi[1][0] = wx*k0 - I33dT - wx2*(ilwe*ilwe*ilwe)*(lwedT-k1);
x0 = O*q;
if (x0.w < 0)
x0 = -x0;
P = Phi*P*transpose(Phi) + GQGt;
checkState();
}
void Fusion::update(const vec3_t& z, const vec3_t& Bi, float sigma) {
vec4_t q(x0);
// measured vector in body space: h(p) = A(p)*Bi
const mat33_t A(quatToMatrix(q));
const vec3_t Bb(A*Bi);
// Sensitivity matrix H = dh(p)/dp
// H = [ L 0 ]
const mat33_t L(crossMatrix(Bb, 0));
// gain...
// K = P*Ht / [H*P*Ht + R]
vec<mat33_t, 2> K;
const mat33_t R(sigma*sigma);
const mat33_t S(scaleCovariance(L, P[0][0]) + R);
const mat33_t Si(invert(S));
const mat33_t LtSi(transpose(L)*Si);
K[0] = P[0][0] * LtSi;
K[1] = transpose(P[1][0])*LtSi;
// update...
// P = (I-K*H) * P
// P -= K*H*P
// | K0 | * | L 0 | * P = | K0*L 0 | * | P00 P10 | = | K0*L*P00 K0*L*P10 |
// | K1 | | K1*L 0 | | P01 P11 | | K1*L*P00 K1*L*P10 |
// Note: the Joseph form is numerically more stable and given by:
// P = (I-KH) * P * (I-KH)' + K*R*R'
const mat33_t K0L(K[0] * L);
const mat33_t K1L(K[1] * L);
P[0][0] -= K0L*P[0][0];
P[1][1] -= K1L*P[1][0];
P[1][0] -= K0L*P[1][0];
P[0][1] = transpose(P[1][0]);
const vec3_t e(z - Bb);
const vec3_t dq(K[0]*e);
q += getF(q)*(0.5f*dq);
x0 = normalize_quat(q);
if (mMode != FUSION_NOMAG) {
const vec3_t db(K[1]*e);
x1 += db;
}
checkState();
}
vec3_t Fusion::getOrthogonal(const vec3_t &v) {
vec3_t w;
if (fabsf(v[0])<= fabsf(v[1]) && fabsf(v[0]) <= fabsf(v[2])) {
w[0]=0.f;
w[1] = v[2];
w[2] = -v[1];
} else if (fabsf(v[1]) <= fabsf(v[2])) {
w[0] = v[2];
w[1] = 0.f;
w[2] = -v[0];
}else {
w[0] = v[1];
w[1] = -v[0];
w[2] = 0.f;
}
return normalize(w);
}
// -----------------------------------------------------------------------
}; // namespace android
|