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mobile_robotics
wolf_projects
wolf_lib
plugins
gnss
Commits
47cb46d7
Commit
47cb46d7
authored
5 years ago
by
Joan Vallvé Navarro
Browse files
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Plain Diff
residual evaluated in ENU (more efficient)
parent
50263127
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2 merge requests
!28
release after RAL
,
!27
After 2nd RAL submission
Changes
2
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2 changed files
include/gnss/factor/factor_gnss_pseudo_range.h
+5
-7
5 additions, 7 deletions
include/gnss/factor/factor_gnss_pseudo_range.h
include/gnss/factor/factor_gnss_tdcp.h
+6
-8
6 additions, 8 deletions
include/gnss/factor/factor_gnss_tdcp.h
with
11 additions
and
15 deletions
include/gnss/factor/factor_gnss_pseudo_range.h
+
5
−
7
View file @
47cb46d7
...
...
@@ -20,7 +20,7 @@ class FactorGnssPseudoRange : public FactorAutodiff<FactorGnssPseudoRange, 1, 3,
GnssUtils
::
Combination
mode_
;
double
pseudo_range_
;
double
std_dev_
;
Eigen
::
Vector3d
satellite_
position
_
;
Eigen
::
Vector3d
satellite_
ENU
_
;
public:
...
...
@@ -50,7 +50,7 @@ class FactorGnssPseudoRange : public FactorAutodiff<FactorGnssPseudoRange, 1, 3,
sensor_gnss_ptr_
(
_sensor_gnss_ptr
),
mode_
(
_mode
),
std_dev_
(
_std_dev
),
satellite_
position_
(
_ftr_ptr
->
getSatellitePosition
())
satellite_
ENU_
(
sensor_gnss_ptr_
->
getREnuEcef
()
*
_ftr_ptr
->
getSatellitePosition
()
+
sensor_gnss_ptr_
->
gettEnuEcef
())
{
WOLF_WARN_COND
(
!
sensor_gnss_ptr_
->
isEnuDefined
()
&&
_status
==
FAC_ACTIVE
,
"Creating an ACTIVE GNSS Fix 3d factor without initializing ENU"
);
...
...
@@ -102,16 +102,14 @@ inline bool FactorGnssPseudoRange::operator ()(const T* const _x,
Eigen
::
Map
<
const
Eigen
::
Quaternion
<
T
>
>
q_map_base
(
_o
);
Eigen
::
Map
<
const
Eigen
::
Matrix
<
T
,
3
,
1
>
>
t_base_antena
(
_x_antena
);
Eigen
::
Matrix
<
T
,
3
,
3
>
R_ECEF_ENU
=
sensor_gnss_ptr_
->
getREnuEcef
().
transpose
().
cast
<
T
>
();
Eigen
::
Matrix
<
T
,
3
,
1
>
t_ECEF_ENU
=
R_ECEF_ENU
*
-
sensor_gnss_ptr_
->
gettEnuEcef
().
cast
<
T
>
();
Eigen
::
Matrix
<
T
,
3
,
3
>
R_ENU_map
=
sensor_gnss_ptr_
->
computeREnuMap
(
_roll_ENU_map
[
0
],
_pitch_ENU_map
[
0
],
_yaw_ENU_map
[
0
]);
Eigen
::
Map
<
const
Eigen
::
Matrix
<
T
,
3
,
1
>
>
t_ENU_map
(
_t_ENU_map
);
// Antenna position in E
CEF
coordinates
Eigen
::
Matrix
<
T
,
3
,
1
>
antena_E
CEF
=
t_ECEF_ENU
+
R_ECEF_ENU
*
(
t_ENU_map
+
R_ENU_map
*
(
t_map_base
+
q_map_base
*
t_base_antena
)
)
;
// Antenna position in E
NU
coordinates
Eigen
::
Matrix
<
T
,
3
,
1
>
antena_E
NU
=
t_ENU_map
+
R_ENU_map
*
(
t_map_base
+
q_map_base
*
t_base_antena
);
// Expected pseudo-range
T
exp
=
(
antena_E
CEF
-
satellite_
position
_
.
cast
<
T
>
()).
norm
()
+
_clock_drift
[
0
];
T
exp
=
(
antena_E
NU
-
satellite_
ENU
_
.
cast
<
T
>
()).
norm
()
+
_clock_drift
[
0
];
// Residual
_residual
[
0
]
=
(
exp
-
pseudo_range_
)
/
std_dev_
;
...
...
This diff is collapsed.
Click to expand it.
include/gnss/factor/factor_gnss_tdcp.h
+
6
−
8
View file @
47cb46d7
...
...
@@ -21,7 +21,7 @@ class FactorGnssTdcp : public FactorAutodiff<FactorGnssTdcp, 1, 3, 4, 1, 3, 4, 1
GnssUtils
::
Combination
mode_
;
double
d_pseudo_range_
;
double
std_dev_
;
Eigen
::
Vector3d
satellite_
position
_k_
,
satellite_
position
_r_
;
Eigen
::
Vector3d
satellite_
ENU
_k_
,
satellite_
ENU
_r_
;
public:
...
...
@@ -55,8 +55,8 @@ class FactorGnssTdcp : public FactorAutodiff<FactorGnssTdcp, 1, 3, 4, 1, 3, 4, 1
sensor_gnss_ptr_
(
_sensor_gnss_ptr
),
mode_
(
_mode
),
std_dev_
(
_std_dev
),
satellite_
position_k_
(
_ftr_k
->
getSatellitePosition
()),
satellite_
position_r_
(
_ftr_r
->
getSatellitePosition
())
satellite_
ENU_k_
(
sensor_gnss_ptr_
->
getREnuEcef
()
*
_ftr_k
->
getSatellitePosition
()
+
sensor_gnss_ptr_
->
gettEnuEcef
()),
satellite_
ENU_r_
(
sensor_gnss_ptr_
->
getREnuEcef
()
*
_ftr_r
->
getSatellitePosition
()
+
sensor_gnss_ptr_
->
gettEnuEcef
())
{
assert
(
_ftr_r
!=
_ftr_k
);
assert
(
_ftr_r
->
getCapture
()
->
getStateBlock
(
"T"
)
!=
nullptr
);
...
...
@@ -126,17 +126,15 @@ inline bool FactorGnssTdcp::operator ()(const T* const _x_r,
Eigen
::
Map
<
const
Eigen
::
Quaternion
<
T
>
>
q_map_base_k
(
_o_k
);
Eigen
::
Map
<
const
Eigen
::
Matrix
<
T
,
3
,
1
>
>
t_base_antena
(
_x_antena
);
Eigen
::
Matrix
<
T
,
3
,
3
>
R_ECEF_ENU
=
sensor_gnss_ptr_
->
getREnuEcef
().
transpose
().
cast
<
T
>
();
Eigen
::
Matrix
<
T
,
3
,
1
>
t_ECEF_ENU
=
R_ECEF_ENU
*
-
sensor_gnss_ptr_
->
gettEnuEcef
().
cast
<
T
>
();
Eigen
::
Matrix
<
T
,
3
,
3
>
R_ENU_map
=
sensor_gnss_ptr_
->
computeREnuMap
(
_roll_ENU_map
[
0
],
_pitch_ENU_map
[
0
],
_yaw_ENU_map
[
0
]);
Eigen
::
Map
<
const
Eigen
::
Matrix
<
T
,
3
,
1
>
>
t_ENU_map
(
_t_ENU_map
);
// Antenna position in ECEF coordinates
Eigen
::
Matrix
<
T
,
3
,
1
>
antena_r_E
CEF
=
t_ECEF_ENU
+
R_ECEF_ENU
*
(
t_ENU_map
+
R_ENU_map
*
(
t_map_base_r
+
q_map_base_r
*
t_base_antena
)
)
;
Eigen
::
Matrix
<
T
,
3
,
1
>
antena_k_E
CEF
=
t_ECEF_ENU
+
R_ECEF_ENU
*
(
t_ENU_map
+
R_ENU_map
*
(
t_map_base_k
+
q_map_base_k
*
t_base_antena
)
)
;
Eigen
::
Matrix
<
T
,
3
,
1
>
antena_r_E
NU
=
t_ENU_map
+
R_ENU_map
*
(
t_map_base_r
+
q_map_base_r
*
t_base_antena
);
Eigen
::
Matrix
<
T
,
3
,
1
>
antena_k_E
NU
=
t_ENU_map
+
R_ENU_map
*
(
t_map_base_k
+
q_map_base_k
*
t_base_antena
);
// Expected tdcp
T
exp
=
(
antena_k_E
CEF
-
satellite_
position
_k_
.
cast
<
T
>
()).
norm
()
-
(
antena_r_E
CEF
-
satellite_
position
_r_
.
cast
<
T
>
()).
norm
()
+
(
_clock_drift_k
[
0
]
-
_clock_drift_r
[
0
]);
T
exp
=
(
antena_k_E
NU
-
satellite_
ENU
_k_
.
cast
<
T
>
()).
norm
()
-
(
antena_r_E
NU
-
satellite_
ENU
_r_
.
cast
<
T
>
()).
norm
()
+
(
_clock_drift_k
[
0
]
-
_clock_drift_r
[
0
]);
// Residual
_residual
[
0
]
=
(
exp
-
d_pseudo_range_
)
/
std_dev_
;
...
...
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Click to expand it.
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