Leonard Hall
|
b50f065cab
|
Copter: use relax alt hold controllers
|
10 years ago |
|
Leonard Hall
|
0aca3c4be6
|
AC_PosControl: add relax Alt Hold controllers
|
10 years ago |
|
Leonard Hall
|
24b8d32b0e
|
AC_AttitudeControl: add comment
|
10 years ago |
|
Leonard Hall
|
7cb3c4ba39
|
AC_PosControl: add feed forward to Alt Hold
|
10 years ago |
Randy Mackay
|
d0036290c1
|
SITL: copter test displays which RTL failed
|
10 years ago |
|
Randy Mackay
|
a1e6a3ee32
|
AC_PosControl: minor format fix
|
10 years ago |
Jonathan Challinger
|
91a03ae0e7
|
Copter: add PILOT_THR_FILT and call set_throttle_out functions with that value
|
10 years ago |
|
Jonathan Challinger
|
3e0dab7b2d
|
AC_PosControl: remove accel error filter and set throttle output filter instead
|
10 years ago |
|
Jonathan Challinger
|
b7f7624aac
|
AC_AttitudeControl: add throttle filter cutoff parameter to set_throttle_out functions
|
10 years ago |
|
Jonathan Challinger
|
e80776f1f5
|
AP_Motors: remove MOT_THR_FILT parameter and add interface to configure filter
|
10 years ago |
|
Jonathan Challinger
|
518e798f53
|
AC_AttitudeControl: rework angle_boost
|
10 years ago |
|
Jonathan Challinger
|
7abd02baf2
|
AC_PosControl: change int32/int16 to float in accel_to_throttle
|
10 years ago |
|
Jonathan Challinger
|
d14893fcd5
|
AC_PosControl: don't limit throttle any more
|
10 years ago |
|
Jonathan Challinger
|
b27b9dd86e
|
Copter: use new throttle interface
|
10 years ago |
|
Jonathan Challinger
|
f3555d0d43
|
AC_AttitudeControl: modify throttle interface to specify stabilization
|
10 years ago |
|
Jonathan Challinger
|
5c2341009a
|
AC_AttitudeControl: throttle is a float
|
10 years ago |
|
Jonathan Challinger
|
8e442675a7
|
AP_Motors: introduce set_stabilize(bool), specifies whether torque demands should be output
|
10 years ago |
|
Jonathan Challinger
|
bc2afb31dd
|
AP_Motors: virtual not necessary in child class
|
10 years ago |
|
Jonathan Challinger
|
a2c69fe90d
|
AP_Motors: add optional motor output throttle filter
|
10 years ago |
|
Jonathan Challinger
|
f93df8997b
|
mk: add coax copter target
|
10 years ago |
|
Jonathan Challinger
|
d66eec536f
|
.gitattributes: automatically clean up newlines in source files
|
10 years ago |
|
Jonathan Challinger
|
0cff3a4292
|
Copter: fixup Windows newlines
|
10 years ago |
|
Leonard Hall
|
ee91be66cf
|
Copter: Update of land detector
|
10 years ago |
|
Leonard Hall
|
4d9da2720b
|
AC_AttitudeControl: add get for angle bf errors
|
10 years ago |
|
Leonard Hall
|
88be3d67e7
|
AP_Motors: add get for throttle comp
|
10 years ago |
|
Leonard Hall
|
791fbcf9b3
|
AP_Motors_Class: time constants of throttle comp
|
10 years ago |
Michael du Breuil
|
78a3ce46b9
|
Plane: Use tecs to control the throttle during takeoff
|
10 years ago |
|
Michael du Breuil
|
04e9141881
|
AP_TECS: Allow tecs to control throttle during takeoff
|
10 years ago |
|
Michael du Breuil
|
a9fc2b8a32
|
AP_Vehicle: Moved takeoff_throttle_max into plane parameters
|
10 years ago |
Andrew Tridgell
|
4586de6637
|
AP_NavEKF: enable optimisation in Linux build
only really need debugging for SITL
|
10 years ago |
|
Leonard Hall
|
48fb487a8c
|
AC_AttitudeControl: Formatting fix
|
10 years ago |
|
Leonard Hall
|
2b5fb850dd
|
Copter: Autotune adjustments
|
10 years ago |
|
Andrew Tridgell
|
3659cd7359
|
PX4: update bootloader with battery power boot fix from David
|
10 years ago |
|
Randy Mackay
|
f2993edc36
|
Copter: move MSG_BATTERY2 higher in select
No functional change
|
10 years ago |
Dario Lindo Andres
|
7dbd6c8509
|
ArduCopter: Enable MSG_BATTERY2 through Mavlink
For allow to show battery_2 voltage and current on GCS.
|
10 years ago |
|
Leonard Hall
|
f8a6684c12
|
Copter: Autotune update
|
10 years ago |
|
Randy Mackay
|
1af6fb13ad
|
SITL: clear glitches before running test
|
10 years ago |
|
Randy Mackay
|
90b02a2685
|
SITL: shorten GPS glitch duration for copter
|
10 years ago |
Paul Riseborough
|
dffa2e19bf
|
AP_NavEKF: Make copter glitch accel consistent with timeout and radius
|
10 years ago |
|
Paul Riseborough
|
5d70854c08
|
AP_NavEKF: Fix minor bug in calculation of innovation variance
the innovation variance for GPS should be the sum of squares of the state and measurement uncertainty.
|
10 years ago |
|
Paul Riseborough
|
1008c6390c
|
AP_NavEKF: Fail absolute position status if GPS repeatedly rejected
|
10 years ago |
|
Paul Riseborough
|
77d3798278
|
AP_NavEKF: Reduce recovery time after a GPS fusion timeout
|
10 years ago |
|
Paul Riseborough
|
0852aeab6e
|
AP_NavEKF: Allow raw innovations to be monitored during timeouts
|
10 years ago |
|
Paul Riseborough
|
d3f4b4a02b
|
AP_NavEKF: Fix name consistency for data check time stamps
|
10 years ago |
|
Andrew Tridgell
|
f4537f4dec
|
PX4: updated bootloaders to current version
|
10 years ago |
|
Jonathan Challinger
|
4e09c9832b
|
Copter: fix guided_posvel and guided_vel to update pos_control at same rate as wpnav
|
10 years ago |
|
Jonathan Challinger
|
6ea91d012e
|
AC_PID: calculate filt_alpha every time the filter is run
|
10 years ago |
|
Randy Mackay
|
55d8f440d4
|
Copter: fix alt sent to fence_check to be meters
|
10 years ago |
|
Randy Mackay
|
f06c859d93
|
AC_Fence: add comment re check_fence method
|
10 years ago |
|
Jonathan Challinger
|
be8c118b63
|
Copter: change altitude fence to work on home altitudes instead of origin altitudes
|
10 years ago |
