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d0c6d087a5
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10748 Commits

Author SHA1 Message Date
Leonard Hall
d0c6d087a5 AP_MotorsMatrix: do not set limits in output_min 2016-04-01 11:59:30 +09:00
Leonard Hall
3fef60da45 AP_MotorsMatrix: stability patch in 0 to 1 range 
Includes storing motor level thrusts to _thrust_rpyt_out
rename _throttle_thr_mix_desired to _throttle_rpy_mix_desired
rename _throttle_thr_mix to _throttle_rpy_mix
use get_hover_throttle_as_high_end_pct
use throttle_thrust_max updated by multicopter spool logic
do not set limits in stability patch
 2016-04-01 11:59:30 +09:00
Leonard Hall
5841310ac7 AP_MotorsMulticopter: update_throttle_filter limits throttle to 0 to 1 2016-04-01 11:59:30 +09:00
Leonard Hall
420b90953c AP_MotorsMulticopter: throttle_radio_min, max to multicopter class 
Moved in from Motors class, only ever used by multicopters
No functional change
 2016-04-01 11:59:30 +09:00
Leonard Hall
2c9a02066d AP_MotorsMulticopter: remove unused functions and variables 2016-04-01 11:59:30 +09:00
Leonard Hall
290e657f61 AP_MotorsMulticopter: update_battery_resistance captures resting voltage while disarmed 
Previously it could also capture this when the input throttle was zero
 2016-04-01 11:59:30 +09:00
Leonard Hall
bc42cb2a66 AP_MotorsMulticopter: update_battery_resistance uses get_throttle accessor 2016-04-01 11:59:30 +09:00
Leonard Hall
8228d9e72c AP_MotorsMulticopter: current_limit_max_throttle uses get_throttle accessor 2016-04-01 11:59:30 +09:00
Leonard Hall
3cbc15bb5b AP_MotorsMulticopter: add get_throttle_thrust_max accessor 2016-04-01 11:59:30 +09:00
Leonard Hall
d7dc37bda0 AP_MotorsMulticopter: remove apply_thrust_curve_and_volt_scaling_pwm 2016-04-01 11:59:30 +09:00
Leonard Hall
06f25b669d AP_MotorsMulticopter: add roll, pitch, throttle and yaw pass through 2016-04-01 11:59:30 +09:00
Leonard Hall
d7c27c949c AP_MotorsMulticopter: add spool_up_complete accessor function 2016-04-01 11:59:30 +09:00
Leonard Hall
983d2dc97a AP_MotorsMulticopter: update_throttle_filter does not set throttle_in 
get_throttle method now used to access filtered throttle
 2016-04-01 11:59:30 +09:00
Leonard Hall
3fc3858fbd AP_MotorsMulticopter: set_throttle_range calcs _min_throttle before use 2016-04-01 11:59:30 +09:00
Leonard Hall
b26318c178 AP_MotorsMulticopter: output_logic implements spooling 2016-04-01 11:59:30 +09:00
Leonard Hall
b7fe6aa16e AP_MotorsMulticopter: remove update_max_throttle 2016-04-01 11:59:30 +09:00
Leonard Hall
be64c71065 AP_MotorsMulticopter: add get_current_limit_max_throttle 
returns the current limited maximum throttle as a number between 0 ~ 1 in the range throttle_min to throttle_max
 2016-04-01 11:59:30 +09:00
Leonard Hall
64ba45a683 AP_MotorsMulticopter: add spin_when_armed_low_end_pct 
returns the spin-when-armed value as a number from 0 to 1 in the range 0 to throttle_min
 2016-04-01 11:59:30 +09:00
Leonard Hall
49819d822f AP_MotorsMulticopter: add get_hover_throttle_as_high_end_pct 
Returns hover throttle as a number from 0 to 1 in the range from throttle_min to throttle_max
 2016-04-01 11:59:30 +09:00
Leonard Hall
e625c105a4 AP_MotorsMulticopter: remove get_throttle_warn 2016-04-01 11:59:30 +09:00
Leonard Hall
3854f2eda7 AP_MotorsMulticopter: rename _throttle_thr_mix_desired to _throttle_rpy_mix_desired 
No functional change
Also rename _throttle_thr_mix to _throttle_rpy_mix
 2016-04-01 11:59:30 +09:00
Leonard Hall
65bbc23a08 AP_MotorsMulticopter: apply_thrust_curve_and_volt_scaling in 0 to 1 range 
existing equivalent pwm function becomes apply_thrust_curve_and_volt_scaling_pwm
 2016-04-01 11:59:30 +09:00
Leonard Hall
cb39f8aab7 AP_MotorsMuticopter: calc_thrust_to_pwm converts thrust in 0 to 1 range to pwm 
pwm output is always between throttle min and throttle max
 2016-04-01 11:59:30 +09:00
Leonard Hall
80ddce103f AP_Motors: move set_throttle_filter_cutoff declaration 
No functional change
 2016-04-01 11:59:30 +09:00
Leonard Hall
649a8c461d AP_Motors: remove unused throttle_radio_min, max 
Moved to AP_MotorsMulticopter
 2016-04-01 11:59:30 +09:00
Leonard Hall
e84011603c AP_Motors: remove unused throttle_pwm_scalar, rpy_pwm_scalar 2016-04-01 11:59:30 +09:00
Leonard Hall
8e1351e474 AP_Motors: init member to resolve compiler warning 2016-04-01 11:59:30 +09:00
Leonard Hall
ed51c7a28d AP_Motors: replace throttle_control_input with throttle_in 
throttle_control_input was 0 to 1000 range, throttle_in is 0 to 1
 2016-04-01 11:59:30 +09:00
Leonard Hall
c96b91efb6 AP_Motors: add output_to_motors 2016-04-01 11:59:30 +09:00
Leonard Hall
ac579685df AP_Motors: remove output_armed_not_stabilizing 2016-04-01 11:59:30 +09:00
Leonard Hall
666a92ae2f AP_Motors: set_throttle accepts 0 to 1 range 2016-04-01 11:59:30 +09:00
Leonard Hall
3c74b4cc69 Motors: add get_roll_thrust which returns roll input in range 0 to 1 
Also added get_pitch_thrust, get_yaw_thrust
 2016-04-01 11:59:30 +09:00
Lucas De Marchi
f304fcf4da AP_InertialSensor: examples: add coding style fixes 
Several coding style problems were already fixed by previous commit,
just finish the cleanup on this example:

  - replace tabs with spaces
  - remove unneeded \r
  - remove extra spaces
 2016-03-31 14:54:17 -03:00
AndersonRayner
10e7d43007 AP_InertialSensor: Add output of all IMUs to example 2016-03-31 14:54:17 -03:00
Lucas De Marchi
a502c0924c GCS_MAVLink: simplify sanity check 2016-03-30 01:32:45 -03:00
Francisco Ferreira
d3e149e5d7 GCS_MAVLink: ignore Clang out-of-range warning 
warning: comparison of constant 4 with expression of type 'mavlink_channel_t' is always false [-Wtautological-constant-out-of-range-compare]
    if (chan >= MAVLINK_COMM_NUM_BUFFERS) {
        ~~~~ ^  ~~~~~~~~~~~~~~~~~~~~~~~~
 2016-03-30 01:32:45 -03:00
Marc MERLIN
5bcd1b02ef RSSI channel is not limited to 5-8. 
Fix doc per my request on https://github.com/ArduPilot/ardupilot/issues/3280
 2016-03-29 08:16:42 -07:00
Tom Pittenger
6718241dad cleanup comments 2016-03-29 05:32:28 -07:00
Andrew Tridgell
894e07a0bd AP_Parachute: added CHUTE_DELAY_MS parameter 
on fixed wing it may take quite some time for the propeller to stop
 2016-03-29 05:48:40 +11:00
Andrew Tridgell
73a2c99d56 SITL: limit rotational rate to 2000dps 2016-03-26 14:23:05 +11:00
Andrew Tridgell
4d01cb1716 HAL_SITL: fixed SITL engine mul error 
expression without get() was treated as int
 2016-03-26 14:17:12 +11:00
Andrew Tridgell
b4c6a0e30e AP_TECS: added logging of speed_weight and state flags 2016-03-26 08:41:09 +11:00
Andrew Tridgell
8ff932b61c AP_TECS: allow underspeed to end faster 
we now can exit an underspeed condition if we stay above min speed for
3 seconds and also reach 15% above min speed. This prevents a problem
with the thrust line causing downpitch leading to a crash due to too
much throttle
 2016-03-26 07:44:22 +11:00
Andrew Tridgell
1ecfa6b487 RC_Channel: fixed example in SITL 2016-03-25 21:35:33 +11:00
Andrew Tridgell
5c92adddf9 HAL_SITL: allow examples to run under SITL 2016-03-25 21:35:16 +11:00
Andrew Tridgell
1e4fe7996e HAL_Linux: update URL 2016-03-25 20:47:53 +11:00
Andrew Tridgell
9737050a23 HAL_FLYMAPLE: update URL 2016-03-25 20:47:44 +11:00
Andrew Tridgell
664d91802e HAL_AVR: update URL 2016-03-25 20:47:35 +11:00
Andrew Tridgell
075dd49afe DataFlash: added Log_Write_Rate() 
needed for quadplane as well as copter so should be in common code
 2016-03-25 12:13:58 +11:00
Andrew Tridgell
ab07781c66 APM_Control: raise default P and I gains, and set a lower limit on I for pitch 
Too many users have very low I gains, which causes a lot of problems for TECS
 2016-03-25 09:54:53 +11:00