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0db9a9bf8d
for example: EKFStateVariancePSet(EKFStateVariancePData *NewP); EKFStateVariancePGet(EKFStateVariancePData *NewP); Also in this case array accessors are renamed as xxxArrayGet/Set: EKFStateVariancePArraySet(float *NewP); EKFStateVariancePArrayGet(float *NewP); Nothing changes for anonymous items as default functions continues to deal with arrays +review OPReview-552
357 lines
13 KiB
C
357 lines
13 KiB
C
/**
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******************************************************************************
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* @addtogroup OpenPilotModules OpenPilot Modules
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* @{
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* @addtogroup CameraStab Camera Stabilization Module
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* @brief Camera stabilization module
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* Updates accessory outputs with values appropriate for camera stabilization
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* @{
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*
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* @file camerastab.c
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
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* @brief Stabilize camera against the roll pitch and yaw of aircraft
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*
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* @see The GNU Public License (GPL) Version 3
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*
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*****************************************************************************/
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/*
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 3 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
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* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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* for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program; if not, write to the Free Software Foundation, Inc.,
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* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
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*/
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/**
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* Output object: Accessory
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*
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* This module will periodically calculate the output values for stabilizing the camera
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*
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* UAVObjects are automatically generated by the UAVObjectGenerator from
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* the object definition XML file.
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*
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* Modules have no API, all communication to other modules is done through UAVObjects.
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* However modules may use the API exposed by shared libraries.
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* See the OpenPilot wiki for more details.
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* http://www.openpilot.org/OpenPilot_Application_Architecture
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*
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*/
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#include "openpilot.h"
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#include "accessorydesired.h"
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#include "attitudestate.h"
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#include "camerastabsettings.h"
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#include "cameradesired.h"
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#include "hwsettings.h"
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#include <pios_struct_helper.h>
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//
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// Configuration
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//
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#define SAMPLE_PERIOD_MS 10
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// Private types
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// Private variables
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static struct CameraStab_data {
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portTickType lastSysTime;
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float inputs[CAMERASTABSETTINGS_INPUT_NUMELEM];
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#ifdef USE_GIMBAL_LPF
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float attitudeFiltered[CAMERASTABSETTINGS_INPUT_NUMELEM];
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#endif
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#ifdef USE_GIMBAL_FF
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float ffLastAttitude[CAMERASTABSETTINGS_INPUT_NUMELEM];
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float ffLastAttitudeFiltered[CAMERASTABSETTINGS_INPUT_NUMELEM];
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float ffFilterAccumulator[CAMERASTABSETTINGS_INPUT_NUMELEM];
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#endif
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} *csd;
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// Private functions
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static void attitudeUpdated(UAVObjEvent *ev);
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static float bound(float val, float limit);
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#ifdef USE_GIMBAL_FF
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static void applyFeedForward(uint8_t index, float dT, float *attitude, CameraStabSettingsData *cameraStab);
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#endif
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/**
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* Initialise the module, called on startup
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* \returns 0 on success or -1 if initialisation failed
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*/
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int32_t CameraStabInitialize(void)
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{
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bool cameraStabEnabled;
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#ifdef MODULE_CAMERASTAB_BUILTIN
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cameraStabEnabled = true;
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#else
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HwSettingsOptionalModulesData optionalModules;
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HwSettingsInitialize();
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HwSettingsOptionalModulesGet(&optionalModules);
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if (optionalModules.CameraStab == HWSETTINGS_OPTIONALMODULES_ENABLED) {
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cameraStabEnabled = true;
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} else {
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cameraStabEnabled = false;
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}
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#endif
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if (cameraStabEnabled) {
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// allocate and initialize the static data storage only if module is enabled
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csd = (struct CameraStab_data *)pvPortMalloc(sizeof(struct CameraStab_data));
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if (!csd) {
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return -1;
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}
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// initialize camera state variables
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memset(csd, 0, sizeof(struct CameraStab_data));
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csd->lastSysTime = xTaskGetTickCount();
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AttitudeStateInitialize();
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CameraStabSettingsInitialize();
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CameraDesiredInitialize();
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UAVObjEvent ev = {
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.obj = AttitudeStateHandle(),
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.instId = 0,
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.event = 0,
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};
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EventPeriodicCallbackCreate(&ev, attitudeUpdated, SAMPLE_PERIOD_MS / portTICK_RATE_MS);
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return 0;
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}
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return -1;
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}
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/* stub: module has no module thread */
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int32_t CameraStabStart(void)
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{
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return 0;
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}
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MODULE_INITCALL(CameraStabInitialize, CameraStabStart);
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static void attitudeUpdated(UAVObjEvent *ev)
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{
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if (ev->obj != AttitudeStateHandle()) {
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return;
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}
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AccessoryDesiredData accessory;
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CameraStabSettingsData cameraStab;
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CameraStabSettingsGet(&cameraStab);
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// check how long since last update, time delta between calls in ms
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portTickType thisSysTime = xTaskGetTickCount();
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float dT_millis = (thisSysTime > csd->lastSysTime) ?
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(float)((thisSysTime - csd->lastSysTime) * portTICK_RATE_MS) :
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(float)SAMPLE_PERIOD_MS;
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csd->lastSysTime = thisSysTime;
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// storage for elevon roll component before the pitch component has been generated
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// we are guaranteed that the iteration order of i is roll pitch yaw
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// that guarnteees this won't be used uninited, but the compiler doesn't know that
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// so we init it or turn the warning/error off for each compiler
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float elevon_roll = 0.0f;
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// process axes
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for (uint8_t i = 0; i < CAMERASTABSETTINGS_INPUT_NUMELEM; i++) {
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// read and process control input
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if (cast_struct_to_array(cameraStab.Input, cameraStab.Input.Roll)[i] != CAMERASTABSETTINGS_INPUT_NONE) {
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if (AccessoryDesiredInstGet(cast_struct_to_array(cameraStab.Input, cameraStab.Input.Roll)[i] -
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CAMERASTABSETTINGS_INPUT_ACCESSORY0, &accessory) == 0) {
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float input_rate;
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switch (cast_struct_to_array(cameraStab.StabilizationMode, cameraStab.StabilizationMode.Roll)[i]) {
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case CAMERASTABSETTINGS_STABILIZATIONMODE_ATTITUDE:
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csd->inputs[i] = accessory.AccessoryVal *
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cast_struct_to_array(cameraStab.InputRange, cameraStab.InputRange.Roll)[i];
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break;
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case CAMERASTABSETTINGS_STABILIZATIONMODE_AXISLOCK:
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input_rate = accessory.AccessoryVal *
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cast_struct_to_array(cameraStab.InputRate, cameraStab.InputRate.Roll)[i];
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if (fabsf(input_rate) > cameraStab.MaxAxisLockRate) {
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csd->inputs[i] = bound(csd->inputs[i] + input_rate * 0.001f * dT_millis,
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cast_struct_to_array(cameraStab.InputRange, cameraStab.InputRange.Roll)[i]);
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}
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break;
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default:
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PIOS_Assert(0);
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}
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}
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}
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// calculate servo output
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float attitude;
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switch (i) {
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case CAMERASTABSETTINGS_INPUT_ROLL:
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AttitudeStateRollGet(&attitude);
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break;
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case CAMERASTABSETTINGS_INPUT_PITCH:
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AttitudeStatePitchGet(&attitude);
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break;
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case CAMERASTABSETTINGS_INPUT_YAW:
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AttitudeStateYawGet(&attitude);
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break;
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default:
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PIOS_Assert(0);
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}
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#ifdef USE_GIMBAL_LPF
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if (cast_struct_to_array(cameraStab.ResponseTime, cameraStab.ResponseTime.Roll)[i]) {
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float rt = (float)cast_struct_to_array(cameraStab.ResponseTime, cameraStab.ResponseTime.Roll)[i];
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attitude = csd->attitudeFiltered[i] = ((rt * csd->attitudeFiltered[i]) + (dT_millis * attitude)) / (rt + dT_millis);
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}
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#endif
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#ifdef USE_GIMBAL_FF
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if (cast_struct_to_array(cameraStab.FeedForward, cameraStab.FeedForward.Roll)[i]) {
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applyFeedForward(i, dT_millis, &attitude, &cameraStab);
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}
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#endif
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// bounding for elevon mixing occurs on the unmixed output
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// to limit the range of the mixed output you must limit the range
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// of both the unmixed pitch and unmixed roll
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float output = bound((attitude + csd->inputs[i]) / cast_struct_to_array(cameraStab.OutputRange, cameraStab.OutputRange.Roll)[i], 1.0f);
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// set output channels
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switch (i) {
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case CAMERASTABSETTINGS_INPUT_ROLL:
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// we are guaranteed that the iteration order of i is roll pitch yaw
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// for elevon mixing we simply grab the value for later use
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if (cameraStab.GimbalType == CAMERASTABSETTINGS_GIMBALTYPE_ROLLPITCHMIXED) {
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elevon_roll = output;
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} else {
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CameraDesiredRollOrServo1Set(&output);
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}
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break;
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case CAMERASTABSETTINGS_INPUT_PITCH:
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// we are guaranteed that the iteration order of i is roll pitch yaw
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// for elevon mixing we use the value we previously grabbed and set both s1 and s2
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if (cameraStab.GimbalType == CAMERASTABSETTINGS_GIMBALTYPE_ROLLPITCHMIXED) {
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float elevon_pitch = output;
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// elevon reversing works like this:
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// first use the normal reversing facilities to get servo 1 roll working in the correct direction
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// then use the normal reversing facilities to get servo 2 roll working in the correct direction
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// then use these new reversing switches to reverse servo 1 and/or 2 pitch as needed
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// if servo 1 pitch is reversed
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if (cameraStab.Servo1PitchReverse == CAMERASTABSETTINGS_SERVO1PITCHREVERSE_TRUE) {
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// use (reversed pitch) + roll
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output = ((1.0f - elevon_pitch) + elevon_roll) / 2.0f;
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} else {
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// use pitch + roll
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output = (elevon_pitch + elevon_roll) / 2.0f;
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}
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CameraDesiredRollOrServo1Set(&output);
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// if servo 2 pitch is reversed
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if (cameraStab.Servo2PitchReverse == CAMERASTABSETTINGS_SERVO2PITCHREVERSE_TRUE) {
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// use (reversed pitch) - roll
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output = ((1.0f - elevon_pitch) - elevon_roll) / 2.0f;
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} else {
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// use pitch - roll
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output = (elevon_pitch - elevon_roll) / 2.0f;
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}
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CameraDesiredPitchOrServo2Set(&output);
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} else {
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CameraDesiredPitchOrServo2Set(&output);
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}
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break;
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case CAMERASTABSETTINGS_INPUT_YAW:
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CameraDesiredYawSet(&output);
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break;
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default:
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PIOS_Assert(0);
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}
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}
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}
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float bound(float val, float limit)
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{
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return (val > limit) ? limit :
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(val < -limit) ? -limit :
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val;
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}
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#ifdef USE_GIMBAL_FF
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void applyFeedForward(uint8_t index, float dT_millis, float *attitude, CameraStabSettingsData *cameraStab)
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{
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// compensate high feed forward values depending on gimbal type
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float gimbalTypeCorrection = 1.0f;
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switch (cameraStab->GimbalType) {
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case CAMERASTABSETTINGS_GIMBALTYPE_GENERIC:
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case CAMERASTABSETTINGS_GIMBALTYPE_ROLLPITCHMIXED:
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// no correction
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break;
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case CAMERASTABSETTINGS_GIMBALTYPE_YAWROLLPITCH:
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if (index == CAMERASTABSETTINGS_INPUT_ROLL) {
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float pitch;
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AttitudeStatePitchGet(&pitch);
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gimbalTypeCorrection = (cameraStab->OutputRange.Pitch - fabsf(pitch))
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/ cameraStab->OutputRange.Pitch;
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}
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break;
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case CAMERASTABSETTINGS_GIMBALTYPE_YAWPITCHROLL:
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if (index == CAMERASTABSETTINGS_INPUT_PITCH) {
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float roll;
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AttitudeStateRollGet(&roll);
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gimbalTypeCorrection = (cameraStab->OutputRange.Roll - fabsf(roll))
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/ cameraStab->OutputRange.Roll;
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}
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break;
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default:
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PIOS_Assert(0);
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}
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// apply feed forward
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float accumulator = csd->ffFilterAccumulator[index];
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accumulator += (*attitude - csd->ffLastAttitude[index]) *
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(float)cast_struct_to_array(cameraStab->FeedForward, cameraStab->FeedForward.Roll)[index] * gimbalTypeCorrection;
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csd->ffLastAttitude[index] = *attitude;
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*attitude += accumulator;
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float filter = (float)((accumulator > 0.0f) ? cast_struct_to_array(cameraStab->AccelTime, cameraStab->AccelTime.Roll)[index] :
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cast_struct_to_array(cameraStab->DecelTime, cameraStab->DecelTime.Roll)[index]) / dT_millis;
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if (filter < 1.0f) {
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filter = 1.0f;
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}
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accumulator -= accumulator / filter;
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csd->ffFilterAccumulator[index] = accumulator;
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*attitude += accumulator;
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// apply acceleration limit
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float delta = *attitude - csd->ffLastAttitudeFiltered[index];
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float maxDelta = (float)cameraStab->MaxAccel * 0.001f * dT_millis;
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if (fabsf(delta) > maxDelta) {
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// we are accelerating too hard
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*attitude = csd->ffLastAttitudeFiltered[index] + ((delta > 0.0f) ? maxDelta : -maxDelta);
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}
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csd->ffLastAttitudeFiltered[index] = *attitude;
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}
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#endif // USE_GIMBAL_FF
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/**
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* @}
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*/
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/**
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* @}
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*/
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