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Author SHA1 Message Date
ctzsnooze
7e3e5649e1 DTERM_CUT
This code cuts D by a specified percentage durning normal flight.

It lets D smoothly rise up to normal during rapid gyro moves like flips and rolls, and increase during prop wash events.

D should now be tuned to values the 'normal' 30-45 range.

If D is 40, a dterm_cut_percentage of 65 will cut D to 14 in normal flight, but the quad will still get full 40 of D to control bounce-back after flips and about 25 of D during strong prop wash.

The dterm_cut_percentage can be adjusted via the OSD, from the D filtering page.
Adding d_cut results in cooler motors, lower amounts of noise in motor traces and faster reactions to quick stick inputs.

Too high a dterm_cut_percentage may bring out P oscillation from lack of D.  Values of 70% are generally OK.

Input is gyro differential (delta).  Frequencies above 40hz (above propwash) are attenuated with a configurable (dterm_cut_range_hz) biquad filter.  Lower values for range can be used if the quad is very noisy or gets low frequency D resonant oscillation.  Up to 50 or 60hz may suit clean quads where prop wash control is the main priority.  Too high a range value results in D being boosted from noise in normal flight.

The boost signal is 'integrated, smoothed and delayed' with a 7hz PT1 'dterm_cut_lowpass_hz' filter.  The default of 7Hz gives about the right amount of smoothing and delay.  Higher numbers cause the boost to come on faster, with less delay. Lower values delay the boost effect and cause it to last longer.

The dterm_cut_gain amount controls the strength of the boost effect by amplifying the input to the boosting effect.  If the quad is flow gently, a higher gain value may be needed to gain full boost.

Logging with set debug_mode = D_CUT allows recording of realtime D values on roll and pitch into debug 2 and 3.  The reatime D value should reach its set maximum during rapid turns, ideally at about the time D itself peaks.  If it fails to reach the maximum, gain should be increased.

The D_Cut feature is not enabled on LUXV2RACE, OMNIBUS, SPRACINGF3NEO because there isn't enough flash space.
2019-01-12 21:09:03 -07:00
Thorsten Laux
ad253c146b add Thrust Linearization feature 2019-01-03 15:09:17 +01:00
Michael Keller
60118da63f
Merge pull request #6432 from joelucid/integrated_yaw
For discussion: Integrated yaw control
2018-12-15 18:40:00 +13:00
Thorsten Laux
b0af988a75 unit test bugs 2018-12-10 19:28:18 +01:00
Thorsten Laux
56181a87c8 change pid.h for unit test 2018-12-10 13:57:35 +01:00
Thorsten Laux
17a995e03e fix abs control refactor, make abs control cutoff configurable 2018-12-10 09:05:20 +01:00
Thorsten Laux
52e2ad2301 eliminate extra newlines 2018-12-09 20:38:15 +01:00
Thorsten Laux
d4512672fe Move to pid.c, add relax to offset drag based component, make configurable 2018-12-09 14:21:44 +01:00
Kenneth Mitchell
233ac7fb3f
Allow width=0 to select single notch. Restore dyn lpf mins. 2018-12-02 10:01:51 -05:00
Kenneth Mitchell
011eae93c6
Cascaded notch filters. 2018-12-02 09:52:02 -05:00
Bruce Luckcuck
b723d2976d Changes from review and add unit tests
Stylistic updates and add tests to the PID unit tests to verify launch control behavior
2018-10-30 18:14:49 -04:00
Bruce Luckcuck
e4dc93b128 Launch Control
Adds a race start assistance system that allows the pilot to pitch forward and then release the sticks with the quad holding position for the race start.
2018-10-27 11:50:37 -04:00
Kenneth Mitchell
ca460e842b
Implement throttle based dynamic gyro and dterm filters. 2018-10-25 19:23:14 -04:00
Kenneth Mitchell
641d0a2e54 Implement biquad on 2nd dterm lowpass filter. 2018-10-14 13:34:11 -04:00
borisbstyle
87b2eeb2fd More isolated pid_unittests
Refactor iterm_relax to iterm_relax_axis

Isolate pidLevel test

Isolate pidHorizon tests

remove if UNIT_TEST

revert to iterm_relax from iterm_relax_axis
2018-09-19 08:15:32 +02:00
ctzsnooze
37da70c555 rebase and recheck 2018-09-15 12:19:53 +10:00
ctzsnooze
80608f5f1c camelCase fix, else added, getMotorMixRange directly 2018-09-15 11:57:47 +10:00
borisbstyle
afccf50d96 Add Iterm Relax unittest // refactor
Refactor PID code Iterm Relax and Absolute control

Move defines for unittest to Makefile

Fix unittest isAirmodeActivated()

Absolute control unittests + optimizations

Fix dead code absolute control // unittests

Further optimizations to absolute control switch logic
2018-09-12 08:09:21 +02:00
mikeller
6a77c5f576 Removed OSD_SLAVE defines. 2018-08-23 23:03:22 +12:00
mikeller
ec06575203 Removed unused PID settings. 2018-07-22 11:41:22 +12:00
Bruce Luckcuck
17e76e48f6 PID controller feedforward
Restructures the PID controller to decouple feedforward from D.

Cleaned up the structure of the PID controller; moved some feature-based enhancements out of the main structure.

Feedforward becomes a separate component of the PID controller and there is now:
f_pitch
f_roll
f_yaw

The default values of 60 for pitch and roll matches the default setpoint weight used in BF3.4.  Yaw previously had no setpoint weight capability so the default here needs to be discussed.  Currently it's also set to 60 and flight testing seems positive.  Feedforward on yaw adds a lot of value so I don't think we want to default to 0.  Instead we need decide on the default.

All occurences of setpoint weight have been replaced by feedforward. "setpoint_relax_ratio" has been renamed to "feedforward_transition".

The pidSum now consists of P + I + D + F.

D has been added back for yaw (disabled by default with d_yaw = 0). We've found little need for D for normal quads but it may have value for other configurations - particularly tricopters.

Updated CMS menus to support adjusting the feedforward for each axis.

Changed the default for "rc_interp_ch" to be "RPYT".  Need yaw to be smoothed to support feedforward.

Open issues:

Needs BFC support
- Need to add support for the axis "F" gains.
- Remove "setpoint weight" slider.
- Rename "D Setpoint transition" to "Feedforward transition"

Needs BBE support
- Header "setpoint_relaxation_ratio" has been renamed "feedforward_transition"
- Header "dterm_setpoint_weight" has been replaced with an array named "feed_forward_weight".
  example: H feed_forward_weight:65,60,60    (R,P,Y)
- PID component "AXISF" has been added for all axes. Should be handled like P, I and D values.
- PidSum calculation needs to include F.

Needs LUA script support
- Support the renamed "setpoint_relax_ratio".
- Support for feedforward weight on all 3 axes.

Open code issues:
- rc_adjustments.c - support for adjusting feedforward weight for all axes. Currently only supporting roll - needs coordination with BFC.
2018-07-21 10:26:23 -04:00
ctzsnooze
94c7109a4c Changes, thanks mikeller and jirif 2018-07-21 23:49:41 +12:00
ctzsnooze
4c917efa50 Smooth anti gravity 2018-07-21 23:49:41 +12:00
Michael Keller
5371350150
Merge pull request #6129 from McGiverGim/iterm_relax_decreasing_I
Add Iterm Relax INC modes
2018-07-09 22:43:33 +12:00
Bruce Luckcuck
1982c94780 RC smoothing retraining update - adds full support for CRSF
Adds in flight monitoring of the rx frame rate and adapts the filters if the frame rate changes. Primarily to add support for Crossfire with its ability to switch from 150hz to 50hz (and back) under some circumstances. Will work with any protocol - not CRSF specific.   So if future receivers add the ability to switch frame rates dynamically the logic should support them.

If the current rx frame rate is more than +-20% from the previously detected rate, then the process will retrain for the next 50 samples as long as the rate continues to be outside the 20% tolerance. Once 50 samples are collected the new frame rate is updated and the filter cutoffs are adjusted. Only filters set with their cutoffs = 0 (auto) will be adjusted. There is a 2 second guard time after a successful update before retraining can start again to prevent rapid switching back and forth.

The logic is optimized to not perform any training if the filters are set to manual cutoffs. So there is an opportunity for advanced users to choose specific cutoffs and reduce the PID loop load slightly. However this is not recommended for Crossfire or other protocols that might change their rx frame rate.

Updated the output of the `rc_smoothing_info` cli command to match the revised logic.
2018-06-22 20:10:06 -04:00
Miguel Angel Mulero Martinez
d63eecffaa Add Iterm Relax INC modes 2018-06-15 15:08:09 +02:00
Michael Keller
db3c0d1447 Some fixes. 2018-06-08 21:18:54 +12:00
Thorsten Laux
fefedbd686 attempts to improve relax
attempts to improve relax fix

attempts to improve relax fix

bug fixes

spaces

changed settings and added isAirmodeActive()

fix rebase error
2018-06-08 21:01:46 +12:00
Bruce Luckcuck
7e18d7c1b9 Make filter type selectable and add BIQUAD
Adds options to select the filter type for both input and derivative.
rc_smoothing_input_type = PT1 | BIQUAD (default is BIQUAD)
rc_smoothing_derivative_type = OFF | PT1 | BIQUAD (default is OFF)
2018-06-03 21:52:15 -04:00
Bruce Luckcuck
826609e703 Experimental filter-based rc channel smoothing
Adds an additional rc channel smoothing algorithm that can be used in place of the default rc interpolation. Utilizing a filter-based approach the smoothing has lower latency and is immune to loop time jitter that can introduce artifacts.  Additionally a smoothing filter is added to the setpoint derivative used to produce D-term setpoint weight resulting in a smoother effect on D.

The default setting is to use the previous interpolation logic and there are no changes unless the optional method is selected.

Configuration:

rc_smoothing_type: (INTERPOLATION | FILTER) - defaults to INTERPOLATION

rc_smoothing_input_hz: (0-255) - sets the rc channel input filter cutoff in Hz. Default value of 0 will enable auto calculation based on received RX frame rate.

rc_smoothing_derivative_hz: (0-255) - sets the setpoint weight derivative filter cutoff in Hz. Default value of 0 will enable auto calculation based on received RX frame rate.

rc_smoothing_debug_axis: (ROLL | PITCH | YAW | THROTTLE) - determines which axis is logged in the debug fields

Debug logging:

set debug_mode = RC_SMOOTHING

debug(0) = raw un-smoothed rc channel data
debug(1) = raw un-smoothed setpoint derivative
debug(2) = filtered setpoint derivative before applied to setpoint weight
debug(3) = auto-calculated filter cutoff frequency base after sampling the rx frame rate

Notes:

Currently only enabled for F4/F7 due to flash size limitations

Uses the rc_inter_ch parameter to determine which channels are smoothed (same as default interpolation logic)

The auto filter cutoff calculation will set a cutoff frequency of 30Hz for typical SBUS frames (9ms).  11ms Spektrum will calculate to approximately 25Hz. The user can manually enter the filter cutoffs to be used instead of the auto calculation.  The current default calculation was chosen as a good starting point but may be adjusted in the future.

Setting a lower cutoff frequency will result in more smoothing, but also more delay.

There currently isn't any support for receivers that change their rx frame rate dynamically.  So for CRSF users wishing to use this alternate smoothing method should change their settings to lock the rx frame rate for now. Support for auto-adjusting to new frame rates in flight will likely be added.
2018-06-03 21:52:01 -04:00
mikeller
a9b3911e03 Made new PID loop improvements conditional, disabled some for F3 to save flash space. 2018-06-03 17:07:10 +12:00
mikeller
c666fcfa17 Reordered and optimised pidProfile parameter group. 2018-05-31 23:51:31 +12:00
Thorsten Laux
bd289121fc absolute control feature 2018-05-30 23:04:26 +02:00
Bruce Luckcuck
2384088855 Requested changes, cleanup and control logic updates
Also added a new parameter acro_trainer_gain to allow adjustments to the limiting strength.
2018-05-29 21:08:19 -04:00
Bruce Luckcuck
9b43839052 Acro trainer
Adds a new angle limiting mode for pilots who are learning to fly in acro mode. Primarily targeted at new LOS acro pilots, but can be used with FPV as well.

The feature is activated with a new mode named "ACRO TRAINER". When the feature is active, the craft will fly in normal acro mode but will limit roll/pitch axes so that they don't exceed the configured angle limit. New pilots can start with a small angle limit and progressively increase as their skills improve.

The accelerometer must be enabled for the feature to be configured and function.

Also the feature will only be active while in acro flight and will disable if ANGLE or HORIZON modes are selected.

For most users all they need to do is simply configure the new mode to be active as desired on the "Modes" tab in the configurator and configure the desired angle limit in the cli.

Configuration parameters:

acro_trainer_angle_limit: (range 10-80) Angle limit in degrees.

acro_trainer_lookahead_ms: (range 10-200) Time in milliseconds that the logic will "look ahead" to help minimize overshoot and bounce-back if the limit is approached at high gyro rates. The default value of 50 should be good for most users. For low powered or unresponsive craft (micros or brushed) it may be helpful to increase this setting if you're seeing substantial overshoot.

acro_trainer_debug_axis: (ROLL, PITCH) The axis that will log information if debugging is active.

To enable debugging:
set debug_mode = ACRO_TRAINER

debug(0) - Current angle
debug(1) - The internal logic state
debug(2) - Modified setpoint
debug(3) - Projected angle based gyro rate and lookahead period
2018-05-29 21:08:16 -04:00
Thorsten Laux
dc929baf75 make itermRelax into enum 2018-05-29 16:40:23 +02:00
Thorsten Laux
32748a328a ITerm relax feature 2018-05-28 16:37:41 +02:00
Thorsten Laux
03b5c3c872 add description 2018-05-27 08:04:27 +02:00
Thorsten Laux
5aad57c3a7 add smart_feedforward config setting 2018-05-24 21:55:49 +02:00
supiiik
76e3e7aded dterm_setpoint_weight to uint16_t
dterm_setpoint_weight changet to uint16 with limit 0-2000
2018-05-23 08:39:45 +02:00
Mark Hale
b2e43abf2d Display anti-gravity activity in OSD.
Signed-off-by: Mark Hale <mark.hale@physics.org>
2018-05-05 19:56:56 +01:00
blckmn
a9f74cd6df Removed excess trailing spaces before new lines on licenses. 2018-04-25 20:58:00 +10:00
Bruce Luckcuck
0a0add8c56 Yaw spin recovery optimize (#3)
* PID controller unittest

* Clean code for yaw spin recovery

* Yaw spin recovery optimizations

* Flash size optimizations, use 50% throttle when airmode is off, and override pidsum_limit_yaw

Also rebasing from betaflight/master
2018-04-24 14:02:36 +12:00
blckmn
46fe22b4bd Direct license replacement 2018-04-22 09:22:46 +10:00
Miroslav Drbal [ApoC]
045557561d Optimized the PID loop a little bit (#5661)
* * Put PID variables into the structure
* Precalculate DTerm gyro filter outside the axis loop
* Removed unused variables PIDweight[3], airmodeWasActivated
* If zero throttle or gyro overflow, we can just set values and exit, this saves checks and jumps in axis loop
* Compute PIDSUM after the axis loop, this saves branching inside the loop because of Yaw has no D term

* * Incorporated review changes from DieHertz and fujin

* * Incorporated another review requests from DieHertz
  - PidSum renamed to Sum
  - pidData[3] redone to pidData[XYZ_AXIS_COUNT]
2018-04-11 08:22:51 +12:00
Andrey Mironov
9cf0eca620
Fixed missing extern on throttleBoost (#5549) 2018-03-26 23:01:25 +03:00
joelucid
ee8daac41d ITerm rotation (#5469)
* ITerm rotation

* address requested changes

* now counting up

* scale errors according to Ki while rotating

* iterm_rotation profile setting

* revert to non scaled version, style related fixes

* Triggering a CI build.
2018-03-26 10:50:21 +13:00
joelucid
efda704ee5 Throttle boost (#5508)
* throttle boost which temporarily boosts throttle in both directions to improve response

* fix comment and use pt1FilterGain

* incorporate review suggestions

* incorporate review suggestions

* use float constant to avoid double promotion

* formatting changes

* formatting change

* hopefully last style changes
2018-03-25 11:33:22 +13:00
ctzsnooze
ab231b7c84 Second dterm pt1 (#5458)
* Second PT1 on DTerm

This PR replaces the default biquad filter with a second PT1 set to
200Hz.

Basically allows the user to enable a second, set point configurable,
PT1 type first order low-pass filter on DTerm.

This is useful because most noise in most logs arises from D, not P.

The default is set to on, at twice the normal Dterm setpoint.  This
provides greater Dterm cut than a single PT1, and twice the steepness
of cut above the second setpoint.  Modelling shows significant
reductions in higher frequency Dterm noise with only minor additional
delay.

The improvement in noise performance will be less than for biquad, but
the delay is considerably less.

If with the default settings the overall noise improves a lot, it may
be possible bring D both filtering set points to higher numbers (e.g.
140/280), or alternatively remove other filters such as the notch
filters, while maintaining an adequate level of control over noise.

* Update names, old defaults, fix whitespace

Defaults restored to biquad with second PT1 off.  ‘lpf’ retained as
abbreviation for values, otherwise generally remove ‘Filter’ where
redundant, replace ‘FilterLpf’ with ‘Lowpass’, etc, thanks Fujin and
DieHertz

* Remove underscore in lowpass_2, add hz to setpoint for lowpass

Thanks DieHertz

* completed replacing lpf with lowpass, added _hz to all lowpass set points in profile

Thanks DieHertz

* fix whitespace

fixed whitespace in settings.c

* whitespace attempt #57

* change lpf to lowpass where appropriate elsewhere

Note did not change OSD abbreviations, they are still LPF, and did not
change gyro_lpf anywhere.

* second attempt at a simple PT1 implementation

Basically copied from the DtermNotch implementation

* Second PT1 on DTerm

This PR replaces the default biquad filter with a second PT1 set to
200Hz.

Basically allows the user to enable a second, set point configurable,
PT1 type first order low-pass filter on DTerm.

This is useful because most noise in most logs arises from D, not P.

The default is set to on, at twice the normal Dterm setpoint.  This
provides greater Dterm cut than a single PT1, and twice the steepness
of cut above the second setpoint.  Modelling shows significant
reductions in higher frequency Dterm noise with only minor additional
delay.

The improvement in noise performance will be less than for biquad, but
the delay is considerably less.

If with the default settings the overall noise improves a lot, it may
be possible bring D both filtering set points to higher numbers (e.g.
140/280), or alternatively remove other filters such as the notch
filters, while maintaining an adequate level of control over noise.

* Rebase

* Remove underscore in lowpass_2, add hz to setpoint for lowpass

Thanks DieHertz

* completed replacing lpf with lowpass, added _hz to all lowpass set points in profile

Thanks DieHertz

* fix whitespace

fixed whitespace in settings.c

* whitespace attempt #57

* change lpf to lowpass where appropriate elsewhere

Note did not change OSD abbreviations, they are still LPF, and did not
change gyro_lpf anywhere.

* second attempt at a simple PT1 implementation

Basically copied from the DtermNotch implementation

* Whitespace fix - thanks, Ledvinap

* Fix PG issue

by moving added dterm_lowpass2_hz to bottom of struct

* Got rid of redundant indirection

* Fixed indentantion shifts
2018-03-21 01:40:23 +13:00
Bruce Luckcuck
449f5f2f5c Runaway Takeoff remove unneeded parameters and enhance deactivate logic
Removed parameters runaway_takeoff_threshold (hardcode to 60) and runaway_takeoff_activate_delay (hardcode to 75).  The previous default values worked well and required no tuning.

Enhance the deactivate logic to remove the R/P/Y stick activity condition once throttle reaches 2X runaway_takeoff_deactivate_throttle_percent.  Additionally reduce the runaway_takeoff_deactivate_delay by 50% when throttle exceeds 75%.
2018-02-27 19:22:33 -05:00