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bc42cb2a66
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10742 Commits

Author SHA1 Message Date
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
Lucas De Marchi
46936767c1 AP_Compass: LSM303D: check for overruns in compass values 2016-03-23 17:50:38 -03:00
Lucas De Marchi
cf2d866d51 AP_Compass: LSM303D: used AP_HAL::Device interface 
Initialization was also changed a little bit so we don't try to
initialize 25 times. We rather use the same methods as in the
AP_InertialSensor drivers.

Also move up the call to is_zero() in read_raw so we don't set
_mag_[x|y|z] in case of failure.
 2016-03-23 17:50:38 -03:00
Lucas De Marchi
5164fbb81b AP_Compass: LSM303D: cleanup driver 
Make it similar to other compass drivers, including method names.
 2016-03-23 17:50:38 -03:00
Lucas De Marchi
20a4a42cb3 AP_Compass: don't store raw and unfiltered fields 
These are not used. The only place where raw fields are used are in the
compass calibrator and we don't need to store them.

Additionally remove duplicated documentation about the meaning of the
functions to avoid them getting out of sync.
 2016-03-23 17:50:38 -03:00
Lucas De Marchi
e6059f5197 AP_Compass: rename files to follow other libraries 
AP_Compass.h is the main header to be exported and AP_Compass.cpp its
implementation. There's no need for an additional header.
 2016-03-23 17:50:38 -03:00
Lucas De Marchi
286697b844 AP_Compass: don't rebuild tree when single driver changes 
Let the drivers be internal to the library so we don't need to rebuild
the entire tree when a single driver changes.
 2016-03-23 17:50:38 -03:00