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21512 Commits

Author SHA1 Message Date
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
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