745df9b13c
Copter: add SONAR_GAIN to tune reaction to sonar
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Some users report the response to sonar is too violent, this allows that
reaction to be reduced
2013-04-20 15:58:36 +09:00
50515e28e1
Copter: replace fabs with fabsf
2013-04-20 15:40:56 +09:00
f5955d8915
Copter: auto climb and descent params removed
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These params now reside in the AC_WPNav library
2013-04-18 14:52:21 +09:00
1ee825ee9a
Copter: move alt and wp checking to AC_WPNAV
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RTL fix so that if it starts rtl-ing from above 80m it returns home
while descending instead of descending at initial position.
add get and set_target_alt_for_reporting
2013-04-14 10:39:23 +09:00
7c559333f5
Copter: get_throttle_rate's target_speed a float
2013-04-14 10:38:51 +09:00
ee7f40cfe9
Copter: Leonard's alt-hold feed forward
2013-04-14 10:38:37 +09:00
f82ce449d7
AC_WPNav: add angle limits and set from AC's throttle controller
2013-04-14 10:38:34 +09:00
1516972eaa
Copter: add panorama to CIRCLE mode
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Yaw will slowly rotate if CIRCLE_RADIUS is set to zero
Circle center is projected forward CIRCLE_RADIUS from current position
and heading
2013-04-14 10:38:01 +09:00
49828eba7d
Copter: integrate AC_WPNav
2013-04-14 10:37:48 +09:00
24dd167607
Copter: ACRO bug fix from Jason
2013-04-01 11:44:28 +09:00
b280857025
Copter: use common angle wrap code
2013-03-29 13:14:31 +11:00
fdcb78ccf7
Copter: leonard's smoother alt-hold transition
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Target altitude when entering alt-hold is based on a projection from
current alt and climb rate
2013-03-17 13:24:49 +09:00
37040adfaa
Copter: bug fix for auto missions over 320m
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get_throttle_althold_with_slew's target_alt parameter defined as int16_t
(instead of int32_t) meaning missions with altitudes >320m could wrap
around and become negative.
2013-03-17 11:14:35 +09:00
f9539384a1
Copter: rename failsafe to failsafe_radio
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Makes way for separation of failsafes for throttle, gps and gcs
2013-03-16 17:14:21 +09:00
476a6d0164
Copter: fix for acro throttle bug
2013-03-02 10:28:44 +09:00
d8515ff85e
Compass: basic compensation for motor interference
2013-03-02 00:03:16 +09:00
df1c0d92bd
Copter: manual throttle scaling fix
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Scaling of bottom half of throttle was changed from THR_MIN ~ 500.
Previously it was from 0 ~ 500.
2013-02-01 22:37:33 +09:00
a0b65a262b
Copter: use scaled throttle for accel-throttle's I term
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Accel throttle's I term is taken from scaled manual throttle
2013-02-01 22:37:25 +09:00
06a71af12f
Copter: THR_MID used to scale manual throttle
2013-02-01 22:37:16 +09:00
aaecc25ac7
Copter: leonard's inav2
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Moved loiter controller to navigation.pde
2013-01-25 15:16:35 +09:00
deafbf1f56
Copter: inav loiter comment changes
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removed unused get_loiter_vel function
2013-01-24 11:14:38 +09:00
68fc9ac1d8
Copter: add "f" to end of float constants
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This is a small performance improvement for the px4
2013-01-23 14:51:37 +09:00
9a09f086d2
Copter: Leonard Hall's inertial nav ver 2
2013-01-23 12:34:49 +09:00
ab1978ad50
Copter: Leonard Hall's inertial nav based loiter
2013-01-22 18:38:00 +09:00
5631f865b2
Update floating point calculations to use floats instead of doubles.
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- Allows use of hardware floating point on the Cortex-M4.
- Added "f" suffix to floating point literals.
- Call floating point versions of stdlib math functions.
2013-01-16 13:52:01 +11:00
175f69a64f
ArduCopter: smooth throttle when switching from manual throttle to alt hold
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new set_accel_throttle_I_from_pilot_throttle function copies the
difference between the pilot's throttle and hover throttle to the
accelerometer based throttle controller's I term.
2013-01-13 20:00:59 +11:00
21b6c78d12
ArduCopter: added get_throttle_althold_with_slew to allow slower altitude target changes
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Improved surface tracking by using slewed althold controller
Reduced sonar mode filter to just 3 elements to reduce lag but at the possible consequence of allowing sonar noise to creep through for people with margin sonar set-ups.
2013-01-13 19:51:47 +11:00
860f4b2605
Copter: merge the latest 2.9 changes into master
2013-01-08 14:37:40 -08:00
ead38f917f
Copter: use GRAVITY_MSS
2013-01-02 14:45:08 +11:00
51d987a890
Copter: removed unusued variable
2013-01-02 09:55:55 +11:00
677b38a48e
ArduCopter: first implementation of surface tracking using sonar
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Note: not yet enabled as part of any flight mode
2013-01-02 09:55:37 +11:00
daac540e08
ArduCopter: get_throttle_althold - add check to avoid divide by zero
2013-01-02 09:55:37 +11:00
576af6d487
ArduCopter: bug fix to althold desired rate calculation. Fix from Jonathan.
2013-01-02 09:55:37 +11:00
ff40fa6aab
ArduCopter: alt hold bug fix - should use 2x linear distance when calculating the desired rate
...
Bug fix from Leonard.
2013-01-02 09:55:37 +11:00
393c893cdb
ArduCopter: bug fix (attempt #2 ) for accel based throttle controller
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Thanks to Jonathan for this.
2013-01-02 09:25:58 +11:00
e583ade62d
ArduCopter: bug fix to accel based throttle controller (was using m/s instead of cm/s)
2013-01-02 09:24:31 +11:00
e850ab7ccd
ArduCopter: add AUTO_VELZ_MIN, AUTO_VELZ_MAX and PILOT_VELZ_MAX to allow better control of climb/descent rate in auto and manual throttle modes
2013-01-02 09:24:31 +11:00
466097b383
ArduCopter: use inertial nav for current altitude and climb rate
2013-01-02 09:22:51 +11:00
7a5e4b8549
ArduCopter: stop unnecessary updates of target altitude and knock-on effect of too many EV message in dataflash log
2013-01-02 09:19:17 +11:00
ac8af9a53f
ArduCopter: Leonard Hall's changes to alt hold including adding low pass filter to climb rate
...
get_throttle_rate_stabilized changed to simply update the target altitude instead of talking directly to the rate controller.
get_throttle_althold changed to use sqrt of distance when calculating the desired rate towards the target altitude.
added reset of accel based throttle PID's I term.
unrelated small bug fix from Randy to allow CH6 tuning of throttle rate D term.
2013-01-02 09:19:17 +11:00
f4c50353b9
ArduCopter: allow tuning of the Throttle Rate D term
2013-01-02 09:16:48 +11:00
7ea34d4fb7
ArduCopter: updated accel based throttle to use ahrs's get_accel_ef method
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Also removed slow low pass filter meant to correct for accelerometer calibration. This is no longer required now that we have the improved calibration method.
2013-01-02 09:11:25 +11:00
7af03127f6
ArduCopter: more work
2012-12-20 14:52:28 +11:00
af77425636
ArduCopter: fix Failed to Init Optflow message at startup
2012-12-11 00:09:45 +09:00
2f1b2b70e6
ArduCopter: added ACRO_TRAINER parameter to allow enabling/disabling the acro training function which will bring the roll back to within +- 45 degrees
2012-12-10 22:27:46 +09:00
154e3c33f7
ArduCopter, AP_InertialNav: consolidated ThirdOrderComplementaryFilter into AP_InertialNav to save about 200bytes of RAM
2012-12-10 00:43:11 +09:00
0eb57bf93d
ACM: TradHeli
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Fix to make update_throttle_cruise work with stab_throttle scaling.
2012-12-08 15:12:39 -05:00
1b97a92098
ACM: Code Cleanup
2012-12-08 14:49:38 -05:00
9dd978576b
ArduCopter: auto yaw changes to allow pilot override of yaw during missions
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Added set_yaw_mode to better control of yaw controller changes and variable initialisation.
Replaced AUTO_YAW mode with separate yaw controllers YAW_LOOK_AT_NEXT_WP, YAW_LOOK_AT_LOCATION, YAW_LOOK_AT_HEADING.
Pilot manual override of yaw causes yaw to change to YAW_HOLD (i.e. manual yaw) until next waypoint is reached.
Added get_yaw_slew function to control how quickly autopilot turns copter
Changed YAW_LOOK_AHEAD to use GPS heading and moved to new get_look_ahead_yaw function in Attitude.pde
Renamed variables: target_bearing->wp_bearing, original_target_bearing->original_wp_bearing.
Removed auto_yaw_tracking and auto_yaw variables and update_auto_yaw function as they are no longer needed.
Simplified MAV_CMD_CONDITION_YAW handling (do_yaw). We lose ability to control direction of turn and ability to do long panorama shots but it now works between waypoints and save 20bytes.
2012-12-08 14:23:32 +09:00
2dd4694eef
ArduCopter: adjusted pid_throttle_accel dt to 0.01 (100hz)
2012-12-06 10:32:12 +09:00
39d524212f
ArduCopter: allow accel based throttle controller to be enabled/disabled with the new THR_ACC_ENABLE parameter.
...
When disabled the original velocity based throttle controller is used.
2012-12-06 10:31:57 +09:00
a5bb54e36e
ArduCopter: RTL clean-up and slightly improved landing sensor
...
Consolidated RTL state to be captured by rtl_state variable.
Combined update_RTL_Nav and verify_RTL functions which performed the same function but one was for missions, the other for the RTL flight mode.
Renamed some RTL parameters and global variables to have RTL at the front.
Landing detector now checks accel-throttle's I term and/or a very low throttle value
2012-12-06 10:31:52 +09:00
072ffec493
ArduCopter: allow INERTIAL_NAV to be enabled separately for horizontal and vertical position
2012-12-06 10:31:41 +09:00
bdb47c449a
ArduCopter: pass linear altitude error to throttle rate controllers.
...
Previously the requested rate used the square root of the altitude error.
Scale pilot's desired vertical rate and acceleration based on ACCELERATION_MAX_Z and VELOCITY_MAX_Z #defines
2012-12-06 10:31:31 +09:00
7b4ed2d227
ArduCopter: restored landing detector to landing throttle mode.
...
Added LAND_SPEED parameter to control the rate of descent for the last 10m of a landing.
Added CH6 tuning for accel based throttle controller.
2012-12-06 10:31:20 +09:00
a94826f182
ArduCopter: add set_throttle_mode to better control initialisation of variables
2012-12-06 10:31:04 +09:00
1036b35128
ArduCopter: added back in angle boost and recombined for heli and multicopter
2012-12-06 10:30:55 +09:00
3cbef57c64
ArduCopter: first merge of leonard's accel based altitude controller plus other changes from Randy
...
Changes include:
New low-level get_throttle_accel function takes target acceleration and compares vs earth-frame Z accelerometer values to produce output to motors.
Higher level throttle controllers modified to call new get_throttle_accel controller
Throttle_rate_stabilized controller added which maintains a desired climb/descent rate
Throttle_land controller added - descends using normal auto throttle controller to 10m then descends at 50cm/s
Multiple throttle modes added including landing mode
Land flight mode no longer needs GPS
Throttle cruise maintenance moved to update_throttle_cruise function
2012-12-06 10:30:49 +09:00
1d589c0b7d
ACM: TradHeli
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Fixes for Attitude rate controllers.
2012-12-04 14:42:04 -05:00
07d7d90882
ACM: TradHeli
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Bringing in Low Pass Filter for Rate Controllers
2012-11-26 21:51:23 -05:00
3f0e8dd358
ACM: TradHeli
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Bringing in Low Pas Filter
Commented out because it does not build.
Needs updates to Low Pass Filter Lib
2012-11-26 21:21:12 -05:00
e8d619acad
ACM: Begin creation of TradHeli rate control.
...
May affect Multi-Rotors.
2012-11-26 21:02:41 -05:00
95eeda7cf7
ACM: TradHeli
...
Removing Angle Boost function.
Does not make sense for helis due to aerodynamics. Can cause more problems than it solves.
2012-11-26 18:58:21 -05:00
6ffc115236
Changes to get_throttle_rate()
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Commented out a bit of code that is not used currently
Change the output constrains to #defines so they can be easily changed, particularly for use in TradHeli.
2012-11-21 17:11:38 -05:00
07a7a1acd8
ArduCopter: replaced digitalRead and digitalWrite with faster calls
...
improved performance logging to dataflash
2012-11-19 01:16:07 +09:00
5f57678a9c
ACM Nav_throttle- removed sign inversion
2012-11-16 17:38:57 -08:00
ac5dcc8d49
ArduCopter: remove last remanants of rate_d to resolve compiler warning of unused variables
2012-11-12 12:35:58 +09:00
69db678252
ACM: attitude.pde - adjusted the FF of the alt hold algorithm, the old way was pretty crap. increased the output range of rate controller.
2012-11-11 18:22:54 -08:00
5ad38a32bf
ACM : Attitude : added nav param reset
2012-11-09 22:15:15 -08:00
3c78c4a7a3
ACM : Attitude.pde added ap bitfield for failsafe bit
2012-11-09 22:15:15 -08:00
a42c6bb609
ACM : Attitude.pde removed stabilize D
2012-11-09 22:15:15 -08:00
14cbe37d3e
ArduCopter: remove unused get_stabilize_rate_yaw
2012-11-07 23:28:25 +09:00
1f801714e8
ArduCopter: incorporate new version of inertial navigation
...
Moved several navigation functions from ArduCopter.pde to navigation.pde
2012-11-07 19:21:31 +09:00
a1b4ec6d0e
ArduCopter: move to use new INS library instead of IMU library
2012-11-07 19:21:09 +09:00
8a8ed7a711
ACM : Formatting
2012-10-28 12:12:38 -07:00
4877348c49
ArduCopter: remove some unhelpful constraints on nav_lat and nav_lon.
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Increase other constraints from 3200 to 32000. These constraints are there to ensure int32_t do not cause an overflow when added to an int16_t.
2012-10-24 22:04:35 +09:00
5e8043fd9c
ArduCopter: changed ACRO_ROLL_STABILIZE and ACRO_PITCH_STABILIZE to parameters
...
Changes on behalf of Leonard Hall
2012-10-23 21:30:50 +09:00
a0752dc7dc
ACM Acceleration management
...
removed unused waypoint_radius var
removed slow_wp
updated speed management system to maintain a constant acceleration or deceleration of 1m/s
changed version to 2.8.1a
2012-10-21 14:32:39 -07:00
583f2e49a3
ArduCopter: integrated Leonard Hall's improved ACRO mode
2012-10-18 23:24:34 +09:00
b944d9df26
ArduCopter: bug fix in earthframe->body frame translation.
...
Provided by Leonard Hall.
Also removed large unnecessary comments.
2012-10-17 19:15:25 +09:00
5fbe53a84d
ArduCopter: bug fix for get_yaw_rate_stabilized_ef
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Provided by Leonard Hall
2012-10-17 10:18:24 +09:00
d7b7e1cefa
New Yaw controller using rate feed forward and stabilize.
...
Signed-off-by: LeonardTHall <LeonardTHall@gmail.com>
2012-10-15 11:37:49 +09:00
997fe85880
ArduCopter: fixed acro mode
...
Changes included:
Removing earth frame roll_rate_trim, pitch_rate_trim and yaw_rate_trim.
Switch ACRO mode to use YAW_ACRO instead of YAW_HOLD.
Changed YAW_ACRO to use stabilize yaw when axis_enabled.
Reset ACRO roll, pitch and yaw targets to current attitude when first entering ACRO.
2012-10-14 17:47:46 +09:00
2848bb8ee6
ArduCopter: freeze I terms if motor limits breached
2012-10-11 17:20:00 +09:00
7cf60e61b4
ArduCopter: bug fix in earth-frame to body-frame conversion for roll
2012-10-07 19:14:40 +09:00
05fd04134a
ArduCopter: fix heli build
2012-10-06 13:46:19 +09:00
e375a27058
ArduCopter: prioritise rate controllers, rate controller targets converted to body frame
2012-10-03 14:10:31 +09:00
361ff0c08f
ArduCopter: allow PID logging of throttle. Make get_angle_boost actually use parameter passed in.
2012-09-18 23:19:23 +09:00
f783ace0de
uncrustify ArduCopter/Attitude.pde
2012-08-21 19:19:50 -07:00
0a25a189eb
ACM | Attitude.pde - removed next_wp.alt reset.
2012-08-18 12:25:48 -07:00
bc631b656e
ACM: Added a more sane limit to Angle boost
2012-08-18 09:04:21 -07:00
87d5b5944d
ArduCopter: commented out get_acro_yaw2 function to reduce compiler warnings
2012-08-18 16:03:49 +09:00
92688a793a
ArduCopter: fixed compiler warning related to shadowing of control_roll and control_pitch in get_of_roll and get_of_pitch.
2012-08-18 11:48:12 +09:00
9cee1b2fa0
ACM : Upped Yaw Limit to 2200
2012-08-16 15:38:46 -07:00
36f947acb9
ArduCopter: changed all "int" to "int16_t" and a few "long"s to "int32_t".
...
Also moved "simple_counter" variable from global scope to the "update_simple_mode" function which is the only place that it's actually used.
2012-08-16 20:04:46 +09:00
a72bf6ef57
ArduCopter: replaced abs with labs as required in a few places.
...
Also fixed a small bug in the get_stabilize_pitch function in which it was using the roll (instead of pitch) to decide whether it should let the i term build-up or not.
2012-08-16 17:51:09 +09:00
3ad08b7ffc
ACM : Added larger WP radius for fast waypoints so we don't loose speed angling in on the WP at the last second.
2012-08-10 10:02:32 -07:00
132ac7d412
ACM : attitude.pde - removed unused function
2012-08-09 17:04:12 -07:00
5d756decd2
ACM : Attitude.pde
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yaw limit, moved toy code out of att to it's own pre
2012-08-09 16:59:43 -07:00
8c47b0c087
ACM: Toy mode fix - Pitch flipped the sign on roll/Yaw coupling.
2012-07-30 15:43:05 -07:00
613849a8df
Arducopter: Force nav_yaw to match auto_yaw when starting a mission
2012-07-19 22:59:03 -07:00
610d1d1795
Arducopter: deprecated the get_nav_yaw_offset function.
...
Small Toy mode updates
2012-07-19 17:41:52 -07:00
aa645afe2b
Arducopter: Altitude change nav
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Split altitude hold into two controls to parallel navigation.
2012-07-18 22:57:10 -07:00
584e7dcda4
Arducopter: Removed Yaw Limit for Quads
2012-07-14 14:06:34 -07:00
44b16b7b61
Arducopter: Temp reversion to old Yaw controller.
2012-07-14 12:26:13 -07:00
59e133235f
Implementing Yaw Fix. Tried to blend with Jason's changes.
2012-07-14 00:24:22 -04:00
6f9e2bf3a8
Arducopter: Toy mode update
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Removed debugging printfs,
lowered roll response - was too high in test flights
made roll limit 2500 for testing
2012-07-11 17:46:06 -07:00
1feaaa4655
Arducopter: Toy mode refinements
2012-07-10 21:53:38 -07:00
226bba48a6
Toy Mode Yaw Rate fix
2012-07-09 13:13:32 -07:00
c62706ad06
Toy Mode: Yaw performance update.
2012-07-03 17:14:54 -07:00
16b25a26c2
Toy Mode: removed virtual WP, copter now just goes into auto_loiter when not holding the sticks.
2012-07-02 17:52:38 -07:00
e0b3309500
Yaw mode:
...
Improved hybrid Yaw mode:
- uses rate controller rather than as fast as possible
- waits 1.5 seconds before entering hold
- bounce free
2012-07-01 13:40:12 -07:00
3ce867508b
Attitude.pde: Toy mode logic
2012-06-29 21:20:27 -07:00
eeab4c5363
Attitude.pde: Turned off boost_p for nav_throttle based on Testing feedback from Marco.
2012-06-26 10:39:42 -07:00
812bf7d874
Attitude.pde - Added small boost to alt hold for takeoff.
2012-06-25 23:12:19 -07:00
1064dcbd34
Open up constraint on Rate Yaw Output for all copters.
2012-06-22 10:06:01 -04:00
27e0aee03f
Small fix to angle boost - increases by about 20% to deal with inefficiencies of non-downward thrust
2012-06-20 08:47:47 -07:00
c42f9ece43
Inertial Control
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I added inertial navigation based on the simulator data. This is an option only available if you compile with Arduino and set
#define INERTIAL_NAV ENABLED
in the APM_Config.h file.
This has been tested for one real flight and did not crash my quad, but consider it very alpha. The quad may be unpredictable at first until the error correction fixes poorly calibrated accels. Be Careful.
Most of the real work is in the inertia file, but the error correction, new variable defines and calibration calls are sprinkled throughout.
The Log should record RAW messages with special debugging values.
2012-06-13 22:34:45 -07:00
65050775e1
ArduCopter: made Robert's new yaw method optional (off by default).
...
Add this line to APM_Config.h to enable Robert's yaw
#define ALTERNATIVE_YAW_MODE ENABLED
2012-06-13 21:50:16 +09:00
c5916a8b4d
Opening up the Yaw Rate constraint for Trad Heli.
2012-06-07 22:40:25 -04:00
e2496181ff
Yaw Fix
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Modified Nav_Yaw controller to better track intended heading changes.
2012-06-07 17:15:33 -04:00
a9610a0761
Stabilization patches
...
removed Angle error limit for stabilization
constricted Iterm to +- 5° error and limited the implementation to when the quad is +- 5° from center
doubled the output limit for Rate controller.
increased default Rate_P gain to .18 with matching Rate_D of .004
Tested in the SIM and in backyard. dramatically increases performance and quad no longer overshoots and flips when pushed hard.
2012-06-05 16:41:44 -07:00
9ab06c5542
Moved PID logging counter into define
2012-06-03 11:13:50 -07:00
2311d52d37
Renamed some variables to clarify functionality.
2012-05-29 12:42:37 -07:00
1a5e2f4e37
Attitude.pde - Removed rate limit based on SIM flights. These should never have been in place and seriously detriment Acro flight.
2012-05-21 09:58:23 -07:00
533772339e
ArduCopter - Attitude.pde - added logging of optical flow pid controller
2012-04-21 20:17:12 +09:00
df85051574
ArduCopter - added dataflash logging of roll and pitch rate controllers
2012-04-08 10:19:20 +09:00
aa4085183c
ArduCopter - Attitude.pde - moved heli_get_angle_boost from heli.pde (which will be removed) to Attitude.pde. In fact we should combine heli_get_angle_boost and the regular get_angle_boost.
2012-04-04 22:51:39 +09:00
e0c9ab5a29
ACM: fixed heli build
2012-03-27 15:37:25 +11:00
47f9dfd125
ACM: fixed the build on the 1280
2012-03-27 15:37:24 +11:00
1f4cfb9333
ArduCopter - added PID log type. Implemented for Yaw stabilize and rate controllers.
2012-03-25 16:09:08 +09:00
547b4ed55b
AHRS: adapt ArduCopter for new AHRS framework
2012-03-19 17:29:02 +11:00
a0717f082e
ACM: Attitude.pde - consolidated wind I term resets
2012-03-18 22:31:21 -07:00
fc32da0d2e
ACM: increased the available rate error constrain, it was too low
2012-03-10 12:39:16 -08:00
bd4835a1b2
ACM: removed the experiment for rate error.
2012-03-10 12:38:29 -08:00
730476fdfd
ACM -
...
Implemented automatic ranging of Alt Hold gains. Works well in simulator and testing.
- alt hold estimation moved to 50 hz
- simple fixed observer calc for smooth and accurate climb rates useful for derivative calcs
- auto-reset of the I term by moving I value into throttle value. This recalcs the gain every 20seconds for battery drainage compensation in long flights.
- remove filtering for Nav_throttle
- added a way to lower the gain on nav_throttle for descents by / climb_rate error by 2 - seems to work OK and keeps copter from dropping like a rock when the Baro drifts quickly lower.
- removed old throttle hold set point code
- made throttle override for alt hold +- 200 vs 250
2012-03-06 22:22:14 -08:00
a387956814
added stab_d gain scheduling
2012-02-28 20:16:40 -08:00
744e5b8c60
ArduCopter - made rate controller filters globals to fix compiler error on Arduino 022 (Arduino 1.0 was fine)
2012-02-28 22:56:26 +09:00
4a0989f95d
ArduCopter - Attitude.pde - updated get_rate_roll and get_rate_pitch to use new average filter.
...
modified all int to int16_t in Attitude.pde
2012-02-28 21:26:37 +09:00
1ce267f904
increased the rate error for more responsive alt hold
2012-02-25 13:31:21 -08:00
57e5eee8c8
TradHeli - increase max yaw input to 45 degrees
2012-02-24 20:18:40 +09:00
364afe8da0
added a constraint to D term
2012-02-23 09:14:44 -08:00
265c5255a3
Added slow_wp default in AP mode
2012-02-19 13:15:40 -08:00
5218220f0f
re-implemented WII Dampening filter for Marco.
2012-02-16 22:38:23 -08:00
632cc783a1
cast D term to float just in case
2012-02-16 22:09:21 -08:00
3d63bb6cd4
Added acro_p to the params
2012-02-15 11:29:25 -08:00
fcb24ee17d
Added Acro_P
2012-02-15 09:10:14 -08:00
3b4cae3cc3
adapted main ACM code for AP_Param
2012-02-13 16:22:52 +11:00
c64d781dce
get_acro_yaw added
2012-02-10 22:32:55 -08:00
f40d40b0f9
Acro fix - we had lost the scaling of Acro mode in 2.1. This restores that.
2012-02-09 22:22:00 -08:00
Randy Mackay
Andrew Tridgell
James Bielman
Pat Hickey
Robert Lefebvre
Jason Short
Jason Short
LeonardTHall
uncrustify