refactor(mc_autotune_attitude_control): convert params.c to module.yaml

Convert 1 parameter file(s) from legacy C format to YAML
module configuration.
This commit is contained in:
Jacob Dahl 2026-03-17 21:55:34 -08:00 committed by Jacob Dahl
parent 89e5b41722
commit ff4eed3604
3 changed files with 45 additions and 88 deletions

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@ -39,6 +39,8 @@ px4_add_module(
SRCS
mc_autotune_attitude_control.cpp
mc_autotune_attitude_control.hpp
MODULE_CONFIG
mc_autotune_attitude_control_params.yaml
DEPENDS
hysteresis
mathlib

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@ -1,88 +0,0 @@
/****************************************************************************
*
* Copyright (c) 2020-2021 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 mc_autotune_attitude_control_params.c
*
* Parameters used by the attitude auto-tuner
*
* @author Mathieu Bresciani <mathieu@auterion.com>
*/
/**
* Multicopter autotune module enable
*
* @boolean
* @group Autotune
*/
PARAM_DEFINE_INT32(MC_AT_EN, 0);
/**
* Amplitude of the injected signal
*
* @min 0.1
* @max 6.0
* @decimal 1
* @group Autotune
*/
PARAM_DEFINE_FLOAT(MC_AT_SYSID_AMP, 0.7);
/**
* Controls when to apply the new gains
*
* After the auto-tuning sequence is completed,
* a new set of gains is available and can be applied
* immediately or after landing.
*
* WARNING Applying the gains in air is dangerous as there is no
* guarantee that those new gains will be able to stabilize
* the drone properly.
*
* @value 0 Do not apply the new gains (logging only)
* @value 1 Apply the new gains after disarm
* @value 2 WARNING Apply the new gains in air
* @group Autotune
*/
PARAM_DEFINE_INT32(MC_AT_APPLY, 1);
/**
* Desired angular rate closed-loop rise time
*
* @min 0.01
* @max 0.5
* @decimal 2
* @unit s
* @group Autotune
*/
PARAM_DEFINE_FLOAT(MC_AT_RISE_TIME, 0.14);

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@ -0,0 +1,43 @@
module_name: mc_autotune_attitude_control
parameters:
- group: Autotune
definitions:
MC_AT_EN:
description:
short: Multicopter autotune module enable
type: boolean
default: 0
MC_AT_SYSID_AMP:
description:
short: Amplitude of the injected signal
type: float
default: 0.7
min: 0.1
max: 6.0
decimal: 1
MC_AT_APPLY:
description:
short: Controls when to apply the new gains
long: |-
After the auto-tuning sequence is completed,
a new set of gains is available and can be applied
immediately or after landing.
WARNING Applying the gains in air is dangerous as there is no
guarantee that those new gains will be able to stabilize
the drone properly.
type: enum
values:
0: Do not apply the new gains (logging only)
1: Apply the new gains after disarm
2: WARNING Apply the new gains in air
default: 1
MC_AT_RISE_TIME:
description:
short: Desired angular rate closed-loop rise time
type: float
default: 0.14
min: 0.01
max: 0.5
decimal: 2
unit: s