Tree: 86416e8f05

AP_Periph-1.3

Copter-4.2

Copter-4.2-BW

apm_2208

apm_2208-rover

apm_2208-rover-debug

c421

copter407

gps-1.3.1

main

master

master_rangefinder

mission-4.1.18

periph-1.3.1

release-4.2.3

rover_4.3

zr-sdk-4.3.1

zr-v5.0

zr-v5.1

zr/Rover-4.3

zr/main-4.3

zr_rover4.2

数字绿土/zr-v5.0

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21331 Commits (86416e8f0553dd07363392e127a1a8aed00e301d)

 

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Author	SHA1	Message	Date
Andrew Tridgell	86416e8f05	AP_Param: added set_default_by_name()	9 years ago
Andrew Tridgell	dd6c4d6225	Plane: fixed up parameters for quadplane ... this fixes quadplane parameters for the new AP_Motors code	9 years ago
Andrew Tridgell	0530af93aa	AP_Param: allow top level parameters to be pointers ... this will allow for the attitude_control variable in quadplane to be a pointer	9 years ago
Randy Mackay	b96ea15220	Plane: quadplane uses AC_AttitudeControl_Multi	9 years ago
Randy Mackay	87399776a3	AC_PosControl: hover throttle default to 0.5	9 years ago
Randy Mackay	41b584ac9e	Plane: fix quadplane qstabilize throttle input	9 years ago
Randy Mackay	52caed2573	Plane: QTUN df messages angle boost field as float	9 years ago
Randy Mackay	f6eabfdab2	AP_MotorsMulticopter: formatting fixes	9 years ago
Randy Mackay	6807b961e2	AP_MotorsMulticopter: protect against div-by-zero if MOT_SPIN_ARMED is zero	9 years ago
Randy Mackay	b39798ad90	AP_Motors: remove unused DESIRED_SPIN_MIN_THROTTLE	9 years ago
Randy Mackay	dc86e1472c	AP_MotorsTri: protect against div-by-zero if MOT_YAW_SV_ANGLE param was set to 90	9 years ago
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	9 years ago
Randy Mackay	b4a61e6ccf	AP_Motors: remove constrain on throttle input ... This constraint is redundant because we already constrain the filtered throttle	9 years ago
Leonard Hall	fce426409e	AP_MotorsTri: fix stab patch	9 years ago
Randy Mackay	49562c5ca3	AP_MotorsMulticopter: reduce num bits used for spool-up-down-mode	9 years ago
Andrew Tridgell	c035ade402	Copter: removed slow_start() from throw mode	9 years ago
Randy Mackay	3ee88fd8c7	AP_MotorsCoax: remove output_min ... This is now implemented by parent AP_MotorsMulticopter	9 years ago
Randy Mackay	8566a61660	AP_MotorsSingle: remove output_min ... This is now implemented by parent AP_MotorsMulticopter	9 years ago
Randy Mackay	8621774040	AP_MotorsTri: remove output_min ... This is now implemented by parent AP_MotorsMulticopter	9 years ago
Randy Mackay	f4d94806e5	AP_MotorsMatrix: remove output_min ... This is now implemented by parent AP_MotorsMulticopter	9 years ago
Randy Mackay	b4b33db79b	AP_MotorsMulticopter: promote output_min from Matrix class	9 years ago
Randy Mackay	2e8acf1f74	AP_MotorsHeli: calculate_scalars made protected ... No functional change	9 years ago
Randy Mackay	165d739b45	AC_AttControl_Heli: roll, pitch, yaw passthrough to motors in -1 to +1 range	9 years ago
Randy Mackay	344d86a095	AC_AttControl_Heli: fix parameter description	9 years ago
Randy Mackay	685be4083c	AC_AttControl_Heli: remove unnecessary cast to AC_HELI_PID	9 years ago
Randy Mackay	6c91e50f8c	AC_AttControl_Heli: remove scaling for centi-degrees and legacy motor input	9 years ago
Randy Mackay	32d238187f	AC_AttControl_Heli: get_althold_lean_angle_max in 0 to 1 range	9 years ago
Randy Mackay	db04dddba5	AC_AttControl_Heli: adjust rate gain param descriptions	9 years ago
Randy Mackay	35c6ea994d	AC_AttControl_Multi: fix parameter descriptions	9 years ago
Randy Mackay	ace58d114f	AC_AttControl_Multi: reduce rate gain defaults	9 years ago
Leonard Hall	b30606bb22	AC_AttControl: remove scaling for centi-degrees and legacy motor input	9 years ago
Randy Mackay	70f81ee338	Plane: remove multicopter PID parameters ... These have been moved to the AC_AttitudeControl class	9 years ago
Randy Mackay	badfdcf54c	Tools: autotest params renamed after copter moves PIDs to attitude controller	9 years ago
Randy Mackay	5090e6f4fb	Copter: init G_Dt with MAIN_LOOP_SECONDS definition	9 years ago
Leonard Hall	a9cda8b384	Copter: add convert_pid_parameters to ease migration to new PID gains	9 years ago
Randy Mackay	479a789325	Copter: remove call to attitude_control.set_dt ... This is now passed into the constructor	9 years ago
Randy Mackay	c352e1bedf	Copter: fix attitude control parameter declaration	9 years ago
Randy Mackay	1f20a5ef69	Copter: access angle and rate PIDs through attitude controller	9 years ago
Randy Mackay	bde498375c	Copter: remove attitude PIDs ... These are now part of AC_AttitudeControl	9 years ago
Randy Mackay	7f2c1f830f	AC_AttControl_Heli: add rate PIDs	9 years ago
Randy Mackay	5edc16dfb4	AC_AttControl_Multi: add rate PIDs	9 years ago
Randy Mackay	75042e5e27	AC_AttControl: remove rate PIDs	9 years ago
Randy Mackay	17c9db08f3	AC_AttControl: add angle and rate PIDs	9 years ago
Randy Mackay	de537390c2	AC_HELI_PID: adjust parameter descriptions ... ILMI range is now 0 to 1	9 years ago
Randy Mackay	3465f05bec	AC_HELI_PID: shorten FILT_HZ to FILT, I_L_MIN to ILMI ... Also minor formatting fix	9 years ago
Randy Mackay	425caeabf7	AC_PI_2D: fix parameter description	9 years ago
Randy Mackay	227e4f86d7	AC_PID: fix parameter description	9 years ago
Randy Mackay	920425567c	AC_PID: shorten FILT_HZ to FILT	9 years ago
Randy Mackay	bc1b8f415a	AP_Motors: example sketch output limit flags	9 years ago
Randy Mackay	c9055ccdb1	AP_Motors: example sketch tests Single and Coax	9 years ago