fda2edb7c4
sensors only publish airspeed if finite
2018-03-26 09:42:50 -04:00
2acd431fcb
mc_att_control: revert to tested cutoff frequency
...
Revert the disabled d term filter which needs to be enabled
after reducing IMU filtering and was probably unintentionally
during a rebase.
2018-03-26 14:23:03 +02:00
a48e3bf68d
sensors fix uninitialized diffferential_pressure message
...
- fixes coverity CID 260383
2018-03-24 13:39:31 -04:00
0ef5d892a1
navigator precland initialize all fields
...
- fixes coverity CID 264259
2018-03-24 13:39:31 -04:00
ed261c76da
add timestamp for sensor_preflight
2018-03-24 07:57:04 +01:00
d2712dcb05
mc_pos_control move to matrix lib ( #9141 )
2018-03-23 12:53:49 -04:00
81a80e0d56
Airmode - Minor rewording
2018-03-23 10:35:08 +01:00
2b6ca2cf82
uavcan_main: use parameter_update to check for param updates
...
this avoids calling param_get() on every loop iteration.
2018-03-23 10:35:08 +01:00
72d22c4297
cleanup uavcan_main: replace warnx with PX4_{INFO,ERR,DEBUG}
2018-03-23 10:35:08 +01:00
99ce9cc2a8
Airmode - Add support for UAVCAN
2018-03-23 10:35:08 +01:00
6976232a20
Airmode - Add airmode parameter for multicopter mixer
2018-03-23 10:35:08 +01:00
44e3bd6c1c
navigator follow_target move to matrix lib
2018-03-22 11:16:34 -04:00
a8ddd9ef64
syslink_bridge: include <cstring> to fix compilation issue
...
GCC error:
error: 'memcpy' was not declared in this scope
2018-03-22 08:19:08 +01:00
b512d11e54
refactor fw_pos_control_l1: replace BlockParam* with Param* classes
...
Also change naming convention: add _ prefix to class attributes
2018-03-22 08:19:08 +01:00
51ca01ce04
FixedwingAttitudeControl: remove SuperBlock dependency
2018-03-22 08:19:08 +01:00
0fdd53f4c2
refactor simulator: replace BlockParam* with Param* classes
2018-03-22 08:19:08 +01:00
7937f9e82c
refactor Battery: replace BlockParam* with Param* classes
2018-03-22 08:19:08 +01:00
408cfd6ce1
err.h: remove unused declarations
2018-03-22 08:19:08 +01:00
68ce62f173
Commander.hpp: remove usage of BlockParam & SuperBlock
2018-03-22 08:19:08 +01:00
3a0a896a9c
sensors move to matrix lib
2018-03-22 08:17:32 +01:00
ad2b96b523
mavlink move to matrix lib
2018-03-22 07:46:16 +01:00
ac7242987c
delete unused tailsitter_recovery library ( #9103 )
2018-03-21 14:09:36 -04:00
b7bfeb442e
fw_att_control move to matrix lib math
2018-03-21 14:08:47 -04:00
d9fbf85c20
ekf2: remove early advertising of wind estimate topic
...
- if it's not estimating wind it won't publish it below (was fixed)
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
372a519ac4
wind estimator: added airspeed and sideslip gate sizes for innovation tests
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
3600225ed4
wind_estimator trim module documentation to fit in limit
2018-03-21 18:46:58 +01:00
f1bb61769f
wind_estimator fix LPWORK/HPWORK confusion and cleanup
2018-03-21 18:46:58 +01:00
8400d42988
wind estimator: fixed minor comments
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
86b525ad2c
wind_estimator: use ModuleParams class to handle parameters
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
d2ebb0c7a2
ekf2: advertise wind topic early to make sure ekf2 get the first instance
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
5b067df01e
wind_estimator: cleanup
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
33c1bcb983
wind_estimator: set missing task_id
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
53e22661d4
wind_estimator: unsubscribe from topics and unadvertise wind topic
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
7c0f043116
added module which implements wind & airspeed scale factor estimator via
...
work queue
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-21 18:46:58 +01:00
d87b7ac7f4
Fix scale application on FW throttle baro compensation
2018-03-20 00:13:36 +01:00
b6b7fddb9f
TECS and L1 switch to matrix math library ( #9101 )
2018-03-19 18:09:54 -04:00
cd250831d5
commander: removed duplicated startup tune
...
Addressing review comments in PR #9096
2018-03-19 14:15:52 +01:00
76aa044105
navigator mission: add yaw offset to vehicle's yaw for ROI cmds and disabled gimbal yaw
2018-03-19 09:42:41 +01:00
a0372c6183
vmount: implement VEHICLE_CMD_DO_SET_ROI_WPNEXT_OFFSET
2018-03-19 09:42:41 +01:00
aaa67632ca
navigator: remove redundant switch block for ROI handling
2018-03-19 09:42:41 +01:00
52e5e0df14
fw_att_control: schedule trims for airspeed and flap deployment ( #8937 )
2018-03-16 16:55:44 -04:00
34dd68bee1
Update syslink_main.cpp
2018-03-16 14:56:40 +01:00
a6e35ab7f7
Beat's changes to make QGC connect with crazyflie
2018-03-16 14:56:40 +01:00
ed0b6db2de
mc_att_control: clarify comment about yaw feed forward
2018-03-15 17:57:46 +01:00
ff25c7f48a
ensure attitude setpoint initialization before arming
...
- On initialization _v_att_sp got filled with zeros
leaving invalid quaternions
- While not armed mc_pos_control did not publish any
attitude setpoint which makes no sense
- The attitude control just uses the data in _v_att_sp
if it was (ever) updated or not
2018-03-15 17:16:14 +01:00
e32b04fff1
mc_att_control: catch numerical out of domain case
...
While operating on exactly normalized float quaternions
it can aparently still happen that one of the elements
gets just slightly above 1 or below -1 and hence out of
the domain of the acosf and asinf functions resulting in
NaN. The constrain function uses stricly smaller/bigger
comparisons and catches all tested cases.
2018-03-15 17:16:14 +01:00
42f4e62a04
mc_att_control: clarify corner case comment
2018-03-15 17:16:14 +01:00
9f69447e22
mc_att_control: replace nasty corner case condition
...
I found a better solution for the condition of the numerical
corner case and also tried to comment it more clearly.
2018-03-15 17:16:14 +01:00
d2ead02fb5
mc_att_control: catch numerical corner cases
...
- Delete left over identity matrix.
- Corner case with a zero element when using the signum function:
We always need a sign also for zero.
- Corner case with arbitrary yaw but and 180 degree roll or pitch:
Reduced attitude control calculation always rotates around roll
because there's no right choice when neglecting yaw. In that small
corner case it's better to just use full attitude contol and hence
rotate around the most efficient roll/pitch combination.
2018-03-15 17:16:14 +01:00
dc28c47544
mc_att_control: correct head comment
2018-03-15 17:16:14 +01:00
Daniel Agar