Randy Mackay
52caed2573
Plane: QTUN df messages angle boost field as float
2016-04-01 11:59:30 +09:00
Randy Mackay
f6eabfdab2
AP_MotorsMulticopter: formatting fixes
2016-04-01 11:59:30 +09:00
Randy Mackay
6807b961e2
AP_MotorsMulticopter: protect against div-by-zero if MOT_SPIN_ARMED is zero
2016-04-01 11:59:30 +09:00
Randy Mackay
b39798ad90
AP_Motors: remove unused DESIRED_SPIN_MIN_THROTTLE
2016-04-01 11:59:30 +09:00
Randy Mackay
dc86e1472c
AP_MotorsTri: protect against div-by-zero if MOT_YAW_SV_ANGLE param was set to 90
2016-04-01 11:59:30 +09:00
Randy Mackay
9b5b6f3779
AP_MotorsHeli: constrain filtered throttle
...
This is required because we have removed the constraint on the throttle input. This also insures that there is no lag caused by the filtered throttle straying far outside the 0 to 1 range
2016-04-01 11:59:30 +09:00
Randy Mackay
b4a61e6ccf
AP_Motors: remove constrain on throttle input
...
This constraint is redundant because we already constrain the filtered throttle
2016-04-01 11:59:30 +09:00
Leonard Hall
fce426409e
AP_MotorsTri: fix stab patch
2016-04-01 11:59:30 +09:00
Randy Mackay
49562c5ca3
AP_MotorsMulticopter: reduce num bits used for spool-up-down-mode
2016-04-01 11:59:30 +09:00
Andrew Tridgell
c035ade402
Copter: removed slow_start() from throw mode
2016-04-01 11:59:30 +09:00
Randy Mackay
3ee88fd8c7
AP_MotorsCoax: remove output_min
...
This is now implemented by parent AP_MotorsMulticopter
2016-04-01 11:59:30 +09:00
Randy Mackay
8566a61660
AP_MotorsSingle: remove output_min
...
This is now implemented by parent AP_MotorsMulticopter
2016-04-01 11:59:30 +09:00
Randy Mackay
8621774040
AP_MotorsTri: remove output_min
...
This is now implemented by parent AP_MotorsMulticopter
2016-04-01 11:59:30 +09:00
Randy Mackay
f4d94806e5
AP_MotorsMatrix: remove output_min
...
This is now implemented by parent AP_MotorsMulticopter
2016-04-01 11:59:30 +09:00
Randy Mackay
b4b33db79b
AP_MotorsMulticopter: promote output_min from Matrix class
2016-04-01 11:59:30 +09:00
Randy Mackay
2e8acf1f74
AP_MotorsHeli: calculate_scalars made protected
...
No functional change
2016-04-01 11:59:30 +09:00
Randy Mackay
165d739b45
AC_AttControl_Heli: roll, pitch, yaw passthrough to motors in -1 to +1 range
2016-04-01 11:59:30 +09:00
Randy Mackay
344d86a095
AC_AttControl_Heli: fix parameter description
2016-04-01 11:59:30 +09:00
Randy Mackay
685be4083c
AC_AttControl_Heli: remove unnecessary cast to AC_HELI_PID
2016-04-01 11:59:30 +09:00
Randy Mackay
6c91e50f8c
AC_AttControl_Heli: remove scaling for centi-degrees and legacy motor input
2016-04-01 11:59:30 +09:00
Randy Mackay
32d238187f
AC_AttControl_Heli: get_althold_lean_angle_max in 0 to 1 range
2016-04-01 11:59:30 +09:00
Randy Mackay
db04dddba5
AC_AttControl_Heli: adjust rate gain param descriptions
2016-04-01 11:59:30 +09:00
Randy Mackay
35c6ea994d
AC_AttControl_Multi: fix parameter descriptions
2016-04-01 11:59:30 +09:00
Randy Mackay
ace58d114f
AC_AttControl_Multi: reduce rate gain defaults
2016-04-01 11:59:30 +09:00
Leonard Hall
b30606bb22
AC_AttControl: remove scaling for centi-degrees and legacy motor input
2016-04-01 11:59:30 +09:00
Randy Mackay
70f81ee338
Plane: remove multicopter PID parameters
...
These have been moved to the AC_AttitudeControl class
2016-04-01 11:59:30 +09:00
Randy Mackay
badfdcf54c
Tools: autotest params renamed after copter moves PIDs to attitude controller
2016-04-01 11:59:30 +09:00
Randy Mackay
5090e6f4fb
Copter: init G_Dt with MAIN_LOOP_SECONDS definition
2016-04-01 11:59:30 +09:00
Leonard Hall
a9cda8b384
Copter: add convert_pid_parameters to ease migration to new PID gains
2016-04-01 11:59:30 +09:00
Randy Mackay
479a789325
Copter: remove call to attitude_control.set_dt
...
This is now passed into the constructor
2016-04-01 11:59:30 +09:00
Randy Mackay
c352e1bedf
Copter: fix attitude control parameter declaration
2016-04-01 11:59:30 +09:00
Randy Mackay
1f20a5ef69
Copter: access angle and rate PIDs through attitude controller
2016-04-01 11:59:30 +09:00
Randy Mackay
bde498375c
Copter: remove attitude PIDs
...
These are now part of AC_AttitudeControl
2016-04-01 11:59:30 +09:00
Randy Mackay
7f2c1f830f
AC_AttControl_Heli: add rate PIDs
2016-04-01 11:59:30 +09:00
Randy Mackay
5edc16dfb4
AC_AttControl_Multi: add rate PIDs
2016-04-01 11:59:30 +09:00
Randy Mackay
75042e5e27
AC_AttControl: remove rate PIDs
2016-04-01 11:59:30 +09:00
Randy Mackay
17c9db08f3
AC_AttControl: add angle and rate PIDs
2016-04-01 11:59:30 +09:00
Randy Mackay
de537390c2
AC_HELI_PID: adjust parameter descriptions
...
ILMI range is now 0 to 1
2016-04-01 11:59:30 +09:00
Randy Mackay
3465f05bec
AC_HELI_PID: shorten FILT_HZ to FILT, I_L_MIN to ILMI
...
Also minor formatting fix
2016-04-01 11:59:30 +09:00
Randy Mackay
425caeabf7
AC_PI_2D: fix parameter description
2016-04-01 11:59:30 +09:00
Randy Mackay
227e4f86d7
AC_PID: fix parameter description
2016-04-01 11:59:30 +09:00
Randy Mackay
920425567c
AC_PID: shorten FILT_HZ to FILT
2016-04-01 11:59:30 +09:00
Randy Mackay
bc1b8f415a
AP_Motors: example sketch output limit flags
2016-04-01 11:59:30 +09:00
Randy Mackay
c9055ccdb1
AP_Motors: example sketch tests Single and Coax
2016-04-01 11:59:30 +09:00
Randy Mackay
41c55ffbe7
AP_MotorsTri: use YAW_SV_REV to reverse yaw output
2016-04-01 11:59:30 +09:00
Leonard Hall
13d727c2c6
AP_MotorsTri: add YAW_SV_ANGLE parameter to capture yaw servo lean angle max
2016-04-01 11:59:30 +09:00
Randy Mackay
c939cc1551
AP_MotorsTri: clarify YAW_SV parameter descriptions and comments
2016-04-01 11:59:30 +09:00
Leonard Hall
267513d864
AP_MotorsTri: fixes to output_armed_stabilizing
...
Also minor comment fixes
2016-04-01 11:59:30 +09:00
Leonard Hall
250a444e57
AP_MotorsCoax: fixes to stab patch
...
Fix throttle_lower flag
Also some formatting changes
2016-04-01 11:59:30 +09:00
Randy Mackay
20565580ed
AP_MotorsCoax: remove disabling of output ch7
2016-04-01 11:59:30 +09:00
