mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-28 19:32:36 +08:00
refactor(lib/mixer_module): convert params.c to module.yaml
Convert 2 parameter file(s) from legacy C format to YAML module configuration.
This commit is contained in:
@@ -60,6 +60,8 @@ px4_add_library(mixer_module
|
|||||||
mixer_module.cpp
|
mixer_module.cpp
|
||||||
mixer_module.hpp
|
mixer_module.hpp
|
||||||
)
|
)
|
||||||
|
set_property(GLOBAL APPEND PROPERTY PX4_MODULE_CONFIG_FILES ${CMAKE_CURRENT_SOURCE_DIR}/motor_params.yaml)
|
||||||
|
set_property(GLOBAL APPEND PROPERTY PX4_MODULE_CONFIG_FILES ${CMAKE_CURRENT_SOURCE_DIR}/params.yaml)
|
||||||
|
|
||||||
add_dependencies(mixer_module output_functions_header)
|
add_dependencies(mixer_module output_functions_header)
|
||||||
target_compile_options(mixer_module PRIVATE ${MAX_CUSTOM_OPT_LEVEL})
|
target_compile_options(mixer_module PRIVATE ${MAX_CUSTOM_OPT_LEVEL})
|
||||||
|
|||||||
@@ -1,57 +0,0 @@
|
|||||||
/****************************************************************************
|
|
||||||
*
|
|
||||||
* Copyright (c) 2018 PX4 Development Team. All rights reserved.
|
|
||||||
*
|
|
||||||
* Redistribution and use in source and binary forms, with or without
|
|
||||||
* modification, are permitted provided that the following conditions
|
|
||||||
* are met:
|
|
||||||
*
|
|
||||||
* 1. Redistributions of source code must retain the above copyright
|
|
||||||
* notice, this list of conditions and the following disclaimer.
|
|
||||||
* 2. Redistributions in binary form must reproduce the above copyright
|
|
||||||
* notice, this list of conditions and the following disclaimer in
|
|
||||||
* the documentation and/or other materials provided with the
|
|
||||||
* distribution.
|
|
||||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
|
||||||
* used to endorse or promote products derived from this software
|
|
||||||
* without specific prior written permission.
|
|
||||||
*
|
|
||||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
|
||||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
|
||||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
|
||||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
|
||||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
|
||||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
|
||||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
|
||||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
|
||||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
|
||||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
|
||||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
|
||||||
* POSSIBILITY OF SUCH DAMAGE.
|
|
||||||
*
|
|
||||||
****************************************************************************/
|
|
||||||
|
|
||||||
/**
|
|
||||||
* @file motor_params.c
|
|
||||||
*
|
|
||||||
* Parameters for motors.
|
|
||||||
*
|
|
||||||
*/
|
|
||||||
|
|
||||||
/**
|
|
||||||
* Thrust to motor control signal model parameter
|
|
||||||
*
|
|
||||||
* Parameter used to model the nonlinear relationship between
|
|
||||||
* motor control signal (e.g. PWM) and static thrust.
|
|
||||||
*
|
|
||||||
* The model is: rel_thrust = factor * rel_signal^2 + (1-factor) * rel_signal,
|
|
||||||
* where rel_thrust is the normalized thrust between 0 and 1, and
|
|
||||||
* rel_signal is the relative motor control signal between 0 and 1.
|
|
||||||
*
|
|
||||||
* @min 0.0
|
|
||||||
* @max 1.0
|
|
||||||
* @decimal 1
|
|
||||||
* @increment 0.1
|
|
||||||
* @group PWM Outputs
|
|
||||||
*/
|
|
||||||
PARAM_DEFINE_FLOAT(THR_MDL_FAC, 0.0f);
|
|
||||||
@@ -0,0 +1,20 @@
|
|||||||
|
module_name: mixer_module
|
||||||
|
parameters:
|
||||||
|
- group: PWM Outputs
|
||||||
|
definitions:
|
||||||
|
THR_MDL_FAC:
|
||||||
|
description:
|
||||||
|
short: Thrust to motor control signal model parameter
|
||||||
|
long: |-
|
||||||
|
Parameter used to model the nonlinear relationship between
|
||||||
|
motor control signal (e.g. PWM) and static thrust.
|
||||||
|
|
||||||
|
The model is: rel_thrust = factor * rel_signal^2 + (1-factor) * rel_signal,
|
||||||
|
where rel_thrust is the normalized thrust between 0 and 1, and
|
||||||
|
rel_signal is the relative motor control signal between 0 and 1.
|
||||||
|
type: float
|
||||||
|
default: 0.0
|
||||||
|
min: 0.0
|
||||||
|
max: 1.0
|
||||||
|
decimal: 1
|
||||||
|
increment: 0.1
|
||||||
@@ -1,18 +0,0 @@
|
|||||||
|
|
||||||
/**
|
|
||||||
* Multicopter air-mode
|
|
||||||
*
|
|
||||||
* The air-mode enables the mixer to increase the total thrust of the multirotor
|
|
||||||
* in order to keep attitude and rate control even at low and high throttle.
|
|
||||||
*
|
|
||||||
* This function should be disabled during tuning as it will help the controller
|
|
||||||
* to diverge if the closed-loop is unstable (i.e. the vehicle is not tuned yet).
|
|
||||||
*
|
|
||||||
* Enabling air-mode for yaw requires the use of an arming switch.
|
|
||||||
*
|
|
||||||
* @value 0 Disabled
|
|
||||||
* @value 1 Roll/Pitch
|
|
||||||
* @value 2 Roll/Pitch/Yaw
|
|
||||||
* @group Mixer Output
|
|
||||||
*/
|
|
||||||
PARAM_DEFINE_INT32(MC_AIRMODE, 0);
|
|
||||||
@@ -0,0 +1,21 @@
|
|||||||
|
module_name: mixer_module
|
||||||
|
parameters:
|
||||||
|
- group: Mixer Output
|
||||||
|
definitions:
|
||||||
|
MC_AIRMODE:
|
||||||
|
description:
|
||||||
|
short: Multicopter air-mode
|
||||||
|
long: |-
|
||||||
|
The air-mode enables the mixer to increase the total thrust of the multirotor
|
||||||
|
in order to keep attitude and rate control even at low and high throttle.
|
||||||
|
|
||||||
|
This function should be disabled during tuning as it will help the controller
|
||||||
|
to diverge if the closed-loop is unstable (i.e. the vehicle is not tuned yet).
|
||||||
|
|
||||||
|
Enabling air-mode for yaw requires the use of an arming switch.
|
||||||
|
type: enum
|
||||||
|
values:
|
||||||
|
0: Disabled
|
||||||
|
1: Roll/Pitch
|
||||||
|
2: Roll/Pitch/Yaw
|
||||||
|
default: 0
|
||||||
Reference in New Issue
Block a user