Paparazzi UAS  v5.8.2_stable-0-g6260b7c
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ahrs_float_utils.h
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1 /*
2  * Copyright (C) 2009 Felix Ruess <felix.ruess@gmail.com>
3  * Copyright (C) 2009 Antoine Drouin <poinix@gmail.com>
4  *
5  * This file is part of paparazzi.
6  *
7  * paparazzi is free software; you can redistribute it and/or modify
8  * it under the terms of the GNU General Public License as published by
9  * the Free Software Foundation; either version 2, or (at your option)
10  * any later version.
11  *
12  * paparazzi is distributed in the hope that it will be useful,
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15  * GNU General Public License for more details.
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21  */
22 
30 #ifndef AHRS_FLOAT_UTILS_H
31 #define AHRS_FLOAT_UTILS_H
32 
35 
36 #include "std.h" // for ABS
37 
38 static inline void ahrs_float_get_euler_from_accel_mag(struct FloatEulers *e, struct Int32Vect3 *accel,
39  struct Int32Vect3 *mag)
40 {
41  /* get phi and theta from accelerometer */
42  struct FloatVect3 accelf;
43  ACCELS_FLOAT_OF_BFP(accelf, *accel);
44  const float phi = atan2f(-accelf.y, -accelf.z);
45  const float cphi = cosf(phi);
46  const float theta = atan2f(cphi * accelf.x, -accelf.z);
47 
48  /* get psi from magnetometer */
49  /* project mag on local tangeant plane */
50  struct FloatVect3 magf;
51  MAGS_FLOAT_OF_BFP(magf, *mag);
52  const float sphi = sinf(phi);
53  const float ctheta = cosf(theta);
54  const float stheta = sinf(theta);
55  const float mn = ctheta * magf.x + sphi * stheta * magf.y + cphi * stheta * magf.z;
56  const float me = 0. * magf.x + cphi * magf.y - sphi * magf.z;
57  float psi = -atan2f(me, mn) + atan2(AHRS_H_Y, AHRS_H_X);
58  if (psi > M_PI) { psi -= 2.*M_PI; } if (psi < -M_PI) { psi += 2.*M_PI; }
59  EULERS_ASSIGN(*e, phi, theta, psi);
60 
61 }
62 
64 static inline void ahrs_float_get_quat_from_accel(struct FloatQuat *q, struct Int32Vect3 *accel)
65 {
66  /* normalized accel measurement in floating point */
67  struct FloatVect3 acc_normalized;
68  ACCELS_FLOAT_OF_BFP(acc_normalized, *accel);
69  FLOAT_VECT3_NORMALIZE(acc_normalized);
70 
71  /* check for 180deg case */
72  if (ABS(acc_normalized.z - 1.0) < 5 * FLT_MIN) {
73  QUAT_ASSIGN(*q, 0.0, 1.0, 0.0, 0.0);
74  } else {
75  /*
76  * axis we want to rotate around is cross product of accel and reference [0,0,-g]
77  * normalized: cross(acc_normalized, [0,0,-1])
78  * vector part of quaternion is the axis
79  * scalar part (angle): 1.0 + dot(acc_normalized, [0,0,-1])
80  */
81  q->qx = - acc_normalized.y;
82  q->qy = acc_normalized.x;
83  q->qz = 0.0;
84  q->qi = 1.0 - acc_normalized.z;
86  }
87 }
88 
89 static inline void ahrs_float_get_quat_from_accel_mag(struct FloatQuat *q, struct Int32Vect3 *accel,
90  struct Int32Vect3 *mag)
91 {
92 
93  /* the quaternion representing roll and pitch from acc measurement */
94  struct FloatQuat q_a;
95  ahrs_float_get_quat_from_accel(&q_a, accel);
96 
97 
98  /* convert mag measurement to float */
99  struct FloatVect3 mag_float;
100  MAGS_FLOAT_OF_BFP(mag_float, *mag);
101 
102  /* and rotate to horizontal plane using the quat from above */
103  struct FloatRMat rmat_phi_theta;
104  float_rmat_of_quat(&rmat_phi_theta, &q_a);
105  struct FloatVect3 mag_ltp;
106  float_rmat_transp_vmult(&mag_ltp, &rmat_phi_theta, &mag_float);
107 
108  /* heading from mag -> make quaternion to rotate around ltp z axis*/
109  struct FloatQuat q_m;
110 
111  /* dot([mag_n.x, mag_n.x, 0], [AHRS_H_X, AHRS_H_Y, 0]) */
112  float dot = mag_ltp.x * AHRS_H_X + mag_ltp.y * AHRS_H_Y;
113 
114  /* |v1||v2| */
115  float norm2 = sqrtf(SQUARE(mag_ltp.x) + SQUARE(mag_ltp.y))
116  * sqrtf(SQUARE(AHRS_H_X) + SQUARE(AHRS_H_Y));
117 
118  // catch 180deg case
119  if (ABS(norm2 + dot) < 5 * FLT_MIN) {
120  QUAT_ASSIGN(q_m, 0.0, 0.0, 0.0, 1.0);
121  } else {
122  /* q_xyz = cross([mag_n.x, mag_n.y, 0], [AHRS_H_X, AHRS_H_Y, 0]) */
123  q_m.qx = 0.0;
124  q_m.qy = 0.0;
125  q_m.qz = mag_ltp.x * AHRS_H_Y - mag_ltp.y * AHRS_H_X;
126  q_m.qi = norm2 + dot;
127  float_quat_normalize(&q_m);
128  }
129 
130  // q_ltp2imu = q_a * q_m
131  // and wrap and normalize
132  float_quat_comp_norm_shortest(q, &q_m, &q_a);
133 }
134 
135 #endif /* AHRS_FLOAT_UTILS_H */
#define SQUARE(_a)
Definition: pprz_algebra.h:47
#define EULERS_ASSIGN(_e, _phi, _theta, _psi)
Definition: pprz_algebra.h:273
euler angles
Roation quaternion.
void float_rmat_transp_vmult(struct FloatVect3 *vb, struct FloatRMat *m_b2a, struct FloatVect3 *va)
rotate 3D vector by transposed rotation matrix.
Paparazzi floating point algebra.
void float_rmat_of_quat(struct FloatRMat *rm, struct FloatQuat *q)
#define QUAT_ASSIGN(_q, _i, _x, _y, _z)
Definition: pprz_algebra.h:516
static void ahrs_float_get_quat_from_accel_mag(struct FloatQuat *q, struct Int32Vect3 *accel, struct Int32Vect3 *mag)
static void float_quat_normalize(struct FloatQuat *q)
#define ACCELS_FLOAT_OF_BFP(_ef, _ei)
Definition: pprz_algebra.h:728
static void ahrs_float_get_quat_from_accel(struct FloatQuat *q, struct Int32Vect3 *accel)
Compute a quaternion representing roll and pitch from an accelerometer measurement.
void float_quat_comp_norm_shortest(struct FloatQuat *a2c, struct FloatQuat *a2b, struct FloatQuat *b2c)
Composition (multiplication) of two quaternions with normalization.
rotation matrix
#define MAGS_FLOAT_OF_BFP(_ef, _ei)
Definition: pprz_algebra.h:740
static void ahrs_float_get_euler_from_accel_mag(struct FloatEulers *e, struct Int32Vect3 *accel, struct Int32Vect3 *mag)
#define FLOAT_VECT3_NORMALIZE(_v)