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Author SHA1 Message Date
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
Randy Mackay
63fefae7cf AP_MotorsCoax: use calc_pwm_output_1ot1 instead of local calc_pivot_radio_output 2016-04-01 11:59:30 +09:00
Leonard Hall
840e60c930 AP_MotorsSingle: fixes to stab patch 
Fixes throttle_lower flag
Also some formatting changes
 2016-04-01 11:59:30 +09:00
Randy Mackay
af9b18329c AP_MotorsSingle: use calc_pwm_output_1to1 instead of local calc_pivot_radio_output 2016-04-01 11:59:30 +09:00
Randy Mackay
ef5dbae707 Copter: remove setting of heli_servo_rsc pwm range 
This object is not used
 2016-04-01 11:59:30 +09:00
Randy Mackay
1f37f5a0e7 Copter: remove tradheli swash, yaw and rsc servos 
These are all created within the AP_MotorsSingle class now except for servo_rsc which was unused
 2016-04-01 11:59:30 +09:00
Randy Mackay
c4b88aafef AP_MotorsHeli: swash and tail servo objects moved into class 2016-04-01 11:59:30 +09:00
Randy Mackay
08a485eec4 AutoTest: reduce heli rate P values 
Also remove explicit params to use EKF2 because it is used by default now
 2016-04-01 11:59:30 +09:00
Randy Mackay
12d9ffee12 AutoTest: remove H_RSC_MIN and MAX from heli params 
These parameters are not used and having them causes errors during testing if we remove the corresponding parameters from the tradheli code
 2016-04-01 11:59:30 +09:00
Randy Mackay
d2a42a7a0e Copter: remove heli_radio_passthrough 
Replaced with set_radio_passthrough which can be used for all frames
 2016-04-01 11:59:30 +09:00
Randy Mackay
ce1fb7fb06 Copter: passthrough pilot input to motors to allow wiggling servos 2016-04-01 11:59:30 +09:00
Randy Mackay
4f1e62d551 AP_MotorsHeli: remove reset_radio_passthrough 2016-04-01 11:59:30 +09:00
Randy Mackay
b5593431bf AP_MotorsHeli_Single: replace collective_mid_pwm with collective_mid_pct 2016-04-01 11:59:30 +09:00
Randy Mackay
9790245bf1 AP_MotorsHeli: replace collective_mid_pwm with collective_mid_pct 2016-04-01 11:59:30 +09:00
Randy Mackay
a39bbc5421 AP_MotorsHeli: servo_test in range -1 to 1 2016-04-01 11:59:30 +09:00