mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-11-03 00:31:36 +08:00
Use new param yaml format
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@@ -39,6 +39,6 @@ px4_add_module(
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FixedwingWindEstimator.hpp
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FixedwingWindEstimator.hpp
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DEPENDS
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DEPENDS
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px4_work_queue
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px4_work_queue
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RateControl
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MODULE_CONFIG
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SlewRate
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module.yaml
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)
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)
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@@ -1,100 +0,0 @@
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/****************************************************************************
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*
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* Copyright (c) 2025 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* AS IS AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file fw_wind_estimator_params.c
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*
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* Parameters defined by the fixed-wing wind estimator
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*
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* @author Jaeyoung Lim <jaeyounglim@berkeley.edu>
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*/
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/**
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* Vehicle Mass
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*
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* @unit %/rad/s
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* @min 0.0
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* @max 25
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* @decimal 3
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* @increment 0.01
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* @group FW Wind Estimator
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*/
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PARAM_DEFINE_FLOAT(FW_W_MASS, 1.00f);
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/**
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* Vehicle Mass
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*
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* @unit %/rad/s
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* @min 0.0
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* @max 25
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* @decimal 3
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* @increment 0.01
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* @group FW Wind Estimator
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*/
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PARAM_DEFINE_FLOAT(FW_W_AREA, 0.34f);
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/**
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* Vehicle Aerodynamic coefficient
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*
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* @unit %/rad/s
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* @min 0.0
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* @max 4
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* @decimal 3
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* @increment 0.01
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* @group FW Wind Estimator
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*/
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PARAM_DEFINE_FLOAT(FW_W_C_B1, 1.0f);
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/**
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* Vehicle Aerodynamic coefficient
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*
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* @unit %/rad/s
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* @min 0.0
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* @max 4
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* @decimal 3
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* @increment 0.01
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* @group FW Wind Estimator
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*/
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PARAM_DEFINE_FLOAT(FW_W_C_A0, 0.15188f);
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/**
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* Vehicle Aerodynamic coefficient
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*
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* @unit %/rad/s
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* @min 0.0
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* @max 10
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* @decimal 3
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* @increment 0.01
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* @group FW Wind Estimator
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*/
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PARAM_DEFINE_FLOAT(FW_W_C_A1, 5.015f);
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@@ -0,0 +1,54 @@
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module_name: fw_wind_estimator
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parameters:
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- group: FW Wind Estimator
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definitions:
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FW_W_MASS:
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description:
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short: Vehicle Mass
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type: float
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default: 1.0
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unit: '%/rad/s'
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min: 0.0
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max: 25
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decimal: 3
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increment: 0.01
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FW_W_AREA:
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description:
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short: Vehicle Mass
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type: float
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default: 0.34
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unit: '%/rad/s'
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min: 0.0
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max: 25
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decimal: 3
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increment: 0.01
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FW_W_C_B1:
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description:
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short: Vehicle Aerodynamic coefficient
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type: float
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default: 1.0
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unit: '%/rad/s'
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min: 0.0
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max: 4
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decimal: 3
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increment: 0.01
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FW_W_C_A0:
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description:
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short: Vehicle Aerodynamic coefficient
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type: float
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default: 0.15188
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unit: '%/rad/s'
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min: 0.0
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max: 4
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decimal: 3
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increment: 0.01
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FW_W_C_A1:
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description:
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short: Vehicle Aerodynamic coefficient
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type: float
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default: 5.015
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unit: '%/rad/s'
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min: 0.0
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max: 10
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decimal: 3
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increment: 0.01
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