mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-06-07 09:13:32 +08:00
Remove unused estimator
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@@ -88,7 +88,6 @@ MODULES += examples/px4_simple_app
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#
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# Drivers / modules to test build, but not useful for test environment
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#
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MODULES += modules/attitude_estimator_so3
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MODULES += drivers/pca8574
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#
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@@ -1,3 +0,0 @@
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Synopsis
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nsh> attitude_estimator_so3_comp start
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File diff suppressed because it is too large
Load Diff
@@ -1,86 +0,0 @@
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/****************************************************************************
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*
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* Copyright (C) 2013 PX4 Development Team. All rights reserved.
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* Author: Hyon Lim <limhyon@gmail.com>
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* Anton Babushkin <anton.babushkin@me.com>
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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 attitude_estimator_so3_params.c
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*
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* Parameters for nonlinear complementary filters on the SO(3).
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*/
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#include "attitude_estimator_so3_params.h"
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/* This is filter gain for nonlinear SO3 complementary filter */
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/* NOTE : How to tune the gain? First of all, stick with this default gain. And let the quad in stable place.
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Log the steady state reponse of filter. If it is too slow, increase SO3_COMP_KP.
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If you are flying from ground to high altitude in short amount of time, please increase SO3_COMP_KI which
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will compensate gyro bias which depends on temperature and vibration of your vehicle */
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PARAM_DEFINE_FLOAT(SO3_COMP_KP, 1.0f); //! This parameter will give you about 15 seconds convergence time.
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//! You can set this gain higher if you want more fast response.
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//! But note that higher gain will give you also higher overshoot.
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PARAM_DEFINE_FLOAT(SO3_COMP_KI, 0.05f); //! This gain will incorporate slow time-varying bias (e.g., temperature change)
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//! This gain is depend on your vehicle status.
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/* offsets in roll, pitch and yaw of sensor plane and body */
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PARAM_DEFINE_FLOAT(SO3_ROLL_OFFS, 0.0f);
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PARAM_DEFINE_FLOAT(SO3_PITCH_OFFS, 0.0f);
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PARAM_DEFINE_FLOAT(SO3_YAW_OFFS, 0.0f);
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int parameters_init(struct attitude_estimator_so3_param_handles *h)
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{
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/* Filter gain parameters */
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h->Kp = param_find("SO3_COMP_KP");
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h->Ki = param_find("SO3_COMP_KI");
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/* Attitude offset (WARNING: Do not change if you do not know what exactly this variable wil lchange) */
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h->roll_off = param_find("SO3_ROLL_OFFS");
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h->pitch_off = param_find("SO3_PITCH_OFFS");
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h->yaw_off = param_find("SO3_YAW_OFFS");
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return OK;
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}
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int parameters_update(const struct attitude_estimator_so3_param_handles *h, struct attitude_estimator_so3_params *p)
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{
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/* Update filter gain */
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param_get(h->Kp, &(p->Kp));
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param_get(h->Ki, &(p->Ki));
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/* Update attitude offset */
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param_get(h->roll_off, &(p->roll_off));
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param_get(h->pitch_off, &(p->pitch_off));
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param_get(h->yaw_off, &(p->yaw_off));
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return OK;
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}
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@@ -1,67 +0,0 @@
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/****************************************************************************
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*
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* Copyright (C) 2013 PX4 Development Team. All rights reserved.
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* Author: Hyon Lim <limhyon@gmail.com>
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* Anton Babushkin <anton.babushkin@me.com>
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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 attitude_estimator_so3_params.h
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*
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* Parameters for nonlinear complementary filters on the SO(3).
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*/
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#include <systemlib/param/param.h>
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struct attitude_estimator_so3_params {
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float Kp;
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float Ki;
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float roll_off;
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float pitch_off;
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float yaw_off;
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};
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struct attitude_estimator_so3_param_handles {
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param_t Kp, Ki;
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param_t roll_off, pitch_off, yaw_off;
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};
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/**
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* Initialize all parameter handles and values
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*
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*/
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int parameters_init(struct attitude_estimator_so3_param_handles *h);
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/**
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* Update all parameters
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*
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*/
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int parameters_update(const struct attitude_estimator_so3_param_handles *h, struct attitude_estimator_so3_params *p);
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@@ -1,12 +0,0 @@
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#
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# Attitude estimator (Nonlinear SO(3) complementary Filter)
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#
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MODULE_COMMAND = attitude_estimator_so3
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SRCS = attitude_estimator_so3_main.cpp \
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attitude_estimator_so3_params.c
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MODULE_STACKSIZE = 1200
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EXTRACXXFLAGS = -Wno-float-equal
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