Harmonized (and partly corrected) all occurancies of gpsSol.llh.alt and getEstimatedAltitude() to handle altiude sourced in cm resolution.
This was introduced by GSP_RESCUE/RTH.
Introduced a naming convention that include the unit into the variable/function names:
gpsSol.llh.alt -> gpsSol.llh.alt_cm
getEstimatedAltitude() -> getEstimatedAltitude_cm()
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All occurences of setpoint weight have been replaced by feedforward.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.
The vtx code doesn't have a lot of test coverage, so this adds a basic unit test that asserts vtx pit mode behavior
_Legal disclaimer: I am making my contributions/submissions to this project solely in my personal capacity and am not conveying any rights to any intellectual property of any third parties._
On bootup aux channels start out at default and allow sticky modes right away,
although they should only be allowed once they are actually not active.
_Legal disclaimer: I am making my contributions/submissions to this project solely in my personal capacity and am not conveying any rights to any intellectual property of any third parties._
This allows modes to be linked, for example to link vtx pit mode to paralyze. Whenever paralyze is activated, vtx pit mode is activated as well. Also the logic to prevent mode changes when enabling paralyze can be removed in favor of making paralyze sticky.
Modes can be linked in CLI by providing the mode id as the last parameter of the aux command. For example in order to link vtx pit mode to paralyze, replace the last 0 of the pit mode aux (39) with the mode id of paralyze (45):
```
aux 2 39 2 1700 2100 0 0
```
becomes
```
aux 2 39 2 1700 2100 0 45
```
_Legal disclaimer: I am making my contributions/submissions to this project solely in my personal capacity and am not conveying any rights to any intellectual property of any third parties._
Change the logic to not modify rcCommand directly and instead apply the additional throttle directly in the mixer.
Also move the logic to the attitude task instead of having it calculate in the PID loop. The logic relies on an angle that's only updated in the attitude task so there was no point in running the calculation every PID loop.
Provides a clear indication that arming is delayed for cases where DSHOT beacon is active.
Clears the OSD and displays "DISABLING BEACON" and "ARMING IN X.Y" with an active countdown in tenths of a second while arming is delayed due to DSHOT beacon. Once delay period is over the normal "ARMING" message appears.
If the DSHOT beacon is not active then this delay screen is not displayed.
Tries to prevent DSHOT beacon commands from interfering with commands to set the motor direction.
Adds a 2 second delay after disarming before DSHOT beacon commands will be sent. This attempts to prevent the beacon commands from interfering with the motor direction reset that happens after using crash flip mode.
During arming if a DSHOT beacon command has been sent within 2 seconds the arming will be delayed until the 2 seconds have passed. This attempts to prevent interference with the motor direction commands sent at arming.
The `failsafe_kill_switch` parameter has been renamed to
`failsafe_switch_mode` and it determines what happens
when the Failsafe mode is activated with an AUX switch.
It takes one of three values:
0 - simulates RC signal loss - thus activates Stage1 failsafe
(former behavior when kill switch option was OFF)
1 - disarms immediately
(former behavior when kill switch option was ON)
2 - activates the failsafe procedure (Stage2) immediately (new)
* through extensive testing prior to the beginning of the RC cycle, we have
discovered that the simplest combination of filters appears to be up to four
PT1 filters: two for gyro, and two for d-term.
* non-cascaded biquad filter plumbing is retained for noisy setups and the
dynamic notch bandpass, although gyro and d-term variants of the filtering may
eventually be removed in favor of pt1
* update all related unit tests
