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https://bitbucket.org/librepilot/librepilot.git
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Merge remote-tracking branch 'origin/laurent/OP-1063_Multi_config_Hexa_fixes' into rel-14.06
This commit is contained in:
commit
25c54ac16d
@ -265,7 +265,9 @@ FrameType_t GetCurrentFrameType()
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case SYSTEMSETTINGS_AIRFRAMETYPE_QUADP:
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case SYSTEMSETTINGS_AIRFRAMETYPE_HEXA:
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case SYSTEMSETTINGS_AIRFRAMETYPE_OCTO:
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case SYSTEMSETTINGS_AIRFRAMETYPE_OCTOX:
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case SYSTEMSETTINGS_AIRFRAMETYPE_HEXAX:
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case SYSTEMSETTINGS_AIRFRAMETYPE_HEXAH:
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case SYSTEMSETTINGS_AIRFRAMETYPE_OCTOV:
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case SYSTEMSETTINGS_AIRFRAMETYPE_OCTOCOAXP:
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case SYSTEMSETTINGS_AIRFRAMETYPE_HEXACOAX:
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@ -190,7 +190,8 @@ static void vtolPathFollowerTask(__attribute__((unused)) void *parameters)
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&& (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_HEXA) && (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_HEXAX)
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&& (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_HEXACOAX) && (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_OCTO)
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&& (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_OCTOV) && (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_OCTOCOAXP)
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&& (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_TRI)) {
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&& (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_TRI) && (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_HEXAH)
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&& (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_OCTOX)) {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_WARNING);
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vTaskDelay(1000);
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continue;
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@ -56,6 +56,33 @@ QStringList ConfigMultiRotorWidget::getChannelDescriptions()
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GUIConfigDataUnion configData = getConfigData();
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multiGUISettingsStruct multi = configData.multi;
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// Octocopter X motor definition
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if (multi.VTOLMotorNNE > 0 && multi.VTOLMotorNNE <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorNNE - 1] = QString("VTOLMotorNNE");
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}
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if (multi.VTOLMotorENE > 0 && multi.VTOLMotorENE <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorENE - 1] = QString("VTOLMotorENE");
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}
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if (multi.VTOLMotorESE > 0 && multi.VTOLMotorESE <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorESE - 1] = QString("VTOLMotorESE");
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}
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if (multi.VTOLMotorSSE > 0 && multi.VTOLMotorSSE <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorSSE - 1] = QString("VTOLMotorSSE");
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}
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if (multi.VTOLMotorSSW > 0 && multi.VTOLMotorSSW <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorSSW - 1] = QString("VTOLMotorSSW");
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}
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if (multi.VTOLMotorWSW > 0 && multi.VTOLMotorWSW <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorWSW - 1] = QString("VTOLMotorWSW");
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}
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if (multi.VTOLMotorWNW > 0 && multi.VTOLMotorWNW <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorWNW - 1] = QString("VTOLMotorWNW");
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}
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if (multi.VTOLMotorNNW > 0 && multi.VTOLMotorNNW <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorNNW - 1] = QString("VTOLMotorNNW");
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}
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// End OctocopterX
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if (multi.VTOLMotorN > 0 && multi.VTOLMotorN <= ConfigMultiRotorWidget::CHANNEL_NUMELEM) {
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channelDesc[multi.VTOLMotorN - 1] = QString("VTOLMotorN");
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}
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@ -110,8 +137,8 @@ ConfigMultiRotorWidget::ConfigMultiRotorWidget(QWidget *parent) :
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m_aircraft->quadShape->setScene(scene);
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QStringList multiRotorTypes;
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multiRotorTypes << "Tricopter Y" << "Quad +" << "Quad X" << "Hexacopter" << "Hexacopter X" << "Hexacopter Y6"
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<< "Octocopter" << "Octocopter V" << "Octo Coax +" << "Octo Coax X";
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multiRotorTypes << "Tricopter Y" << "Quad +" << "Quad X" << "Hexacopter" << "Hexacopter X" << "Hexacopter H" << "Hexacopter Y6"
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<< "Octocopter" << "Octocopter X" << "Octocopter V" << "Octo Coax +" << "Octo Coax X";
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m_aircraft->multirotorFrameType->addItems(multiRotorTypes);
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// Set default model to "Quad X"
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@ -158,16 +185,23 @@ void ConfigMultiRotorWidget::setupUI(QString frameType)
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} else if (frameType == "Hexa" || frameType == "Hexacopter") {
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setComboCurrentIndex(m_aircraft->multirotorFrameType, m_aircraft->multirotorFrameType->findText("Hexacopter"));
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m_aircraft->mrRollMixLevel->setValue(50);
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m_aircraft->mrPitchMixLevel->setValue(33);
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setYawMixLevel(33);
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m_aircraft->mrRollMixLevel->setValue(100); // Old Roll 50 - Pitch 33 - Yaw 33
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m_aircraft->mrPitchMixLevel->setValue(100); // Do not alter mixer matrix
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setYawMixLevel(100);
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} else if (frameType == "HexaX" || frameType == "Hexacopter X") {
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setComboCurrentIndex(m_aircraft->multirotorFrameType,
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m_aircraft->multirotorFrameType->findText("Hexacopter X"));
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m_aircraft->mrRollMixLevel->setValue(33);
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m_aircraft->mrPitchMixLevel->setValue(50);
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setYawMixLevel(33);
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m_aircraft->mrRollMixLevel->setValue(100); // Old: Roll 33 - Pitch 50 - Yaw 33
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m_aircraft->mrPitchMixLevel->setValue(100); // Do not alter mixer matrix
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setYawMixLevel(100);
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} else if (frameType == "HexaH" || frameType == "Hexacopter H") {
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setComboCurrentIndex(m_aircraft->multirotorFrameType,
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m_aircraft->multirotorFrameType->findText("Hexacopter H"));
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m_aircraft->mrRollMixLevel->setValue(100); // Do not alter mixer matrix
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m_aircraft->mrPitchMixLevel->setValue(100); // All mixers RPY levels = 100%
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setYawMixLevel(100);
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} else if (frameType == "HexaCoax" || frameType == "Hexacopter Y6") {
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setComboCurrentIndex(m_aircraft->multirotorFrameType,
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m_aircraft->multirotorFrameType->findText("Hexacopter Y6"));
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@ -178,9 +212,15 @@ void ConfigMultiRotorWidget::setupUI(QString frameType)
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} else if (frameType == "Octo" || frameType == "Octocopter") {
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setComboCurrentIndex(m_aircraft->multirotorFrameType, m_aircraft->multirotorFrameType->findText("Octocopter"));
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m_aircraft->mrRollMixLevel->setValue(33);
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m_aircraft->mrPitchMixLevel->setValue(33);
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setYawMixLevel(25);
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m_aircraft->mrRollMixLevel->setValue(100); // Do not alter mixer matrix
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m_aircraft->mrPitchMixLevel->setValue(100); // All mixers RPY levels = 100%
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setYawMixLevel(100);
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} else if (frameType == "OctoX" || frameType == "Octocopter X") {
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setComboCurrentIndex(m_aircraft->multirotorFrameType, m_aircraft->multirotorFrameType->findText("Octocopter X"));
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m_aircraft->mrRollMixLevel->setValue(100); // Do not alter mixer matrix
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m_aircraft->mrPitchMixLevel->setValue(100); // All mixers RPY levels = 100%
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setYawMixLevel(100);
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} else if (frameType == "OctoV" || frameType == "Octocopter V") {
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setComboCurrentIndex(m_aircraft->multirotorFrameType,
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m_aircraft->multirotorFrameType->findText("Octocopter V"));
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@ -235,10 +275,14 @@ void ConfigMultiRotorWidget::setupEnabledControls(QString frameType)
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enableComboBoxes(this, CHANNELBOXNAME, 6, true);
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} else if (frameType == "HexaX" || frameType == "Hexacopter X") {
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enableComboBoxes(this, CHANNELBOXNAME, 6, true);
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} else if (frameType == "HexaH" || frameType == "Hexacopter H") {
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enableComboBoxes(this, CHANNELBOXNAME, 6, true);
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} else if (frameType == "HexaCoax" || frameType == "Hexacopter Y6") {
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enableComboBoxes(this, CHANNELBOXNAME, 6, true);
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} else if (frameType == "Octo" || frameType == "Octocopter") {
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enableComboBoxes(this, CHANNELBOXNAME, 8, true);
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} else if (frameType == "OctoX" || frameType == "Octocopter X") {
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enableComboBoxes(this, CHANNELBOXNAME, 8, true);
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} else if (frameType == "OctoV" || frameType == "Octocopter V") {
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enableComboBoxes(this, CHANNELBOXNAME, 8, true);
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} else if (frameType == "OctoCoaxP" || frameType == "Octo Coax +") {
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@ -270,15 +314,23 @@ void ConfigMultiRotorWidget::registerWidgets(ConfigTaskWidget &parent)
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void ConfigMultiRotorWidget::resetActuators(GUIConfigDataUnion *configData)
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{
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configData->multi.VTOLMotorN = 0;
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configData->multi.VTOLMotorNE = 0;
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configData->multi.VTOLMotorE = 0;
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configData->multi.VTOLMotorSE = 0;
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configData->multi.VTOLMotorS = 0;
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configData->multi.VTOLMotorSW = 0;
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configData->multi.VTOLMotorW = 0;
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configData->multi.VTOLMotorNW = 0;
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configData->multi.VTOLMotorN = 0;
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configData->multi.VTOLMotorNE = 0;
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configData->multi.VTOLMotorE = 0;
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configData->multi.VTOLMotorSE = 0;
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configData->multi.VTOLMotorS = 0;
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configData->multi.VTOLMotorSW = 0;
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configData->multi.VTOLMotorW = 0;
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configData->multi.VTOLMotorNW = 0;
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configData->multi.TRIYaw = 0;
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configData->multi.VTOLMotorNNE = 0;
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configData->multi.VTOLMotorENE = 0;
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configData->multi.VTOLMotorESE = 0;
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configData->multi.VTOLMotorSSE = 0;
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configData->multi.VTOLMotorSSW = 0;
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configData->multi.VTOLMotorWSW = 0;
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configData->multi.VTOLMotorWNW = 0;
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configData->multi.VTOLMotorNNW = 0;
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}
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/**
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@ -366,10 +418,13 @@ void ConfigMultiRotorWidget::refreshWidgetsValues(QString frameType)
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int channel = m_aircraft->multiMotorChannelBox1->currentIndex() - 1;
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if (channel > -1) {
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// get motor 1 value for Pitch
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double value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_PITCH);
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m_aircraft->mrPitchMixLevel->setValue(qRound(value / 1.27));
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value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_YAW);
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// get motor 2 value for Yaw and Roll
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channel = m_aircraft->multiMotorChannelBox2->currentIndex() - 1;
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value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_YAW);
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setYawMixLevel(-qRound(value / 1.27));
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// change channels
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@ -392,9 +447,12 @@ void ConfigMultiRotorWidget::refreshWidgetsValues(QString frameType)
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int channel = m_aircraft->multiMotorChannelBox1->currentIndex() - 1;
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if (channel > -1) {
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// get motor 1 value for Pitch
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double value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_PITCH);
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m_aircraft->mrPitchMixLevel->setValue(qRound(value / 1.27));
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// get motor 2 value for Yaw and Roll
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channel = m_aircraft->multiMotorChannelBox2->currentIndex() - 1;
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value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_YAW);
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setYawMixLevel(-qRound(value / 1.27));
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@ -402,6 +460,34 @@ void ConfigMultiRotorWidget::refreshWidgetsValues(QString frameType)
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value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_ROLL);
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m_aircraft->mrRollMixLevel->setValue(-qRound(value / 1.27));
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}
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} else if (frameType == "HexaH") {
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// Motors 1/2/3 4/5/6 are: NE / E / SE / SW / W / NW
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setComboCurrentIndex(m_aircraft->multiMotorChannelBox1, multi.VTOLMotorNE);
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setComboCurrentIndex(m_aircraft->multiMotorChannelBox2, multi.VTOLMotorE);
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setComboCurrentIndex(m_aircraft->multiMotorChannelBox3, multi.VTOLMotorSE);
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setComboCurrentIndex(m_aircraft->multiMotorChannelBox4, multi.VTOLMotorSW);
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setComboCurrentIndex(m_aircraft->multiMotorChannelBox5, multi.VTOLMotorW);
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setComboCurrentIndex(m_aircraft->multiMotorChannelBox6, multi.VTOLMotorNW);
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|
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// Now, read the 1st mixer R/P/Y levels and initialize the mix sliders.
|
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// This assumes that all vectors are identical - if not, the user should use the
|
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// "custom" setting.
|
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|
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int channel = m_aircraft->multiMotorChannelBox1->currentIndex() - 1;
|
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if (channel > -1) {
|
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// get motor 1 value for Pitch
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double value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_PITCH);
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m_aircraft->mrPitchMixLevel->setValue(qRound(value / 1.27));
|
||||
|
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// get motor 2 value for Yaw and Roll
|
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channel += 1;
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value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_YAW);
|
||||
setYawMixLevel(-qRound(value / 1.27));
|
||||
|
||||
channel = m_aircraft->multiMotorChannelBox2->currentIndex() - 1;
|
||||
value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_ROLL);
|
||||
m_aircraft->mrRollMixLevel->setValue(-qRound(value / 1.27));
|
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}
|
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} else if (frameType == "HexaCoax") {
|
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// Motors 1/2/3 4/5/6 are: NW/W NE/E S/SE
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox1, multi.VTOLMotorNW);
|
||||
@ -449,8 +535,8 @@ void ConfigMultiRotorWidget::refreshWidgetsValues(QString frameType)
|
||||
value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_YAW);
|
||||
setYawMixLevel(-qRound(value / 1.27));
|
||||
|
||||
// change channels
|
||||
channel = m_aircraft->multiMotorChannelBox2->currentIndex() - 1;
|
||||
// Get M3 Roll value
|
||||
channel = m_aircraft->multiMotorChannelBox3->currentIndex() - 1;
|
||||
value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_ROLL);
|
||||
m_aircraft->mrRollMixLevel->setValue(-qRound(value / 1.27));
|
||||
} else if (frameType == "OctoV") {
|
||||
@ -477,6 +563,34 @@ void ConfigMultiRotorWidget::refreshWidgetsValues(QString frameType)
|
||||
m_aircraft->mrRollMixLevel->setValue(-qRound(value / 1.27));
|
||||
}
|
||||
}
|
||||
} else if (frameType == "OctoX") {
|
||||
// Motors 1 to 8 are NNE / ENE / ESE / etc
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox1, multi.VTOLMotorNNE);
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox2, multi.VTOLMotorENE);
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox3, multi.VTOLMotorESE);
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox4, multi.VTOLMotorSSE);
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox5, multi.VTOLMotorSSW);
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox6, multi.VTOLMotorWSW);
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox7, multi.VTOLMotorWNW);
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox8, multi.VTOLMotorNNW);
|
||||
|
||||
|
||||
// Now, read the 1st mixer R/P/Y levels and initialize the mix sliders.
|
||||
// This assumes that all vectors are identical - if not, the user should use the
|
||||
// "custom" setting.
|
||||
int channel = m_aircraft->multiMotorChannelBox1->currentIndex() - 1;
|
||||
if (channel > -1) {
|
||||
double value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_PITCH);
|
||||
m_aircraft->mrPitchMixLevel->setValue(qRound(value / 1.27));
|
||||
|
||||
value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_YAW);
|
||||
setYawMixLevel(-qRound(value / 1.27));
|
||||
|
||||
// Get M2 Roll value
|
||||
channel = m_aircraft->multiMotorChannelBox2->currentIndex() - 1;
|
||||
value = getMixerVectorValue(mixer, channel, VehicleConfig::MIXERVECTOR_ROLL);
|
||||
m_aircraft->mrRollMixLevel->setValue(-qRound(value / 1.27));
|
||||
}
|
||||
} else if (frameType == "OctoCoaxX") {
|
||||
// Motors 1 to 8 are N / NE / E / etc
|
||||
setComboCurrentIndex(m_aircraft->multiMotorChannelBox1, multi.VTOLMotorNW);
|
||||
@ -549,6 +663,37 @@ QString ConfigMultiRotorWidget::updateConfigObjectsFromWidgets()
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Hexacopter X") {
|
||||
airframeType = "HexaX";
|
||||
setupHexa(false);
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Hexacopter H") {
|
||||
airframeType = "HexaH";
|
||||
|
||||
// Show any config errors in GUI
|
||||
if (throwConfigError(6)) {
|
||||
return airframeType;
|
||||
}
|
||||
motorList << "VTOLMotorNE" << "VTOLMotorE" << "VTOLMotorSE" << "VTOLMotorSW" << "VTOLMotorW" << "VTOLMotorNW";
|
||||
setupMotors(motorList);
|
||||
|
||||
// Motor 1 to 6, H layout
|
||||
// ---------------------------------------------
|
||||
// Motor: 1 2 3 4 5 6
|
||||
// ROLL {-0.50, -1.00, -0.50, 0.50, 1.00, 0.50}
|
||||
// PITCH {1.00, 0.00, -1.00, -1.00, -0.00, 1.00}
|
||||
// YAW {-0.50, 1.00, -0.50, 0.50, -1.00, 0.50}
|
||||
// ---------------------------------------------
|
||||
// http://wiki.paparazziuav.org/wiki/RotorcraftMixing
|
||||
// pitch roll yaw
|
||||
double hMixer[8][3] = {
|
||||
{ 1, -0.5, -0.5 },
|
||||
{ 0, -1, 1 },
|
||||
{ -1, -0.5, -0.5 },
|
||||
{ -1, 0.5, 0.5 },
|
||||
{ 0, 1, -1 },
|
||||
{ 1, 0.5, 0.5 },
|
||||
{ 0, 0, 0 },
|
||||
{ 0, 0, 0 }
|
||||
};
|
||||
setupMultiRotorMixer(hMixer);
|
||||
m_aircraft->mrStatusLabel->setText(tr("Configuration OK"));
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Hexacopter Y6") {
|
||||
airframeType = "HexaCoax";
|
||||
|
||||
@ -572,7 +717,7 @@ QString ConfigMultiRotorWidget::updateConfigObjectsFromWidgets()
|
||||
{ 0, 0, 0 }
|
||||
};
|
||||
setupMultiRotorMixer(mixerMatrix);
|
||||
m_aircraft->mrStatusLabel->setText("Configuration OK");
|
||||
m_aircraft->mrStatusLabel->setText(tr("Configuration OK"));
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Octocopter") {
|
||||
airframeType = "Octo";
|
||||
|
||||
@ -583,20 +728,58 @@ QString ConfigMultiRotorWidget::updateConfigObjectsFromWidgets()
|
||||
motorList << "VTOLMotorN" << "VTOLMotorNE" << "VTOLMotorE" << "VTOLMotorSE" << "VTOLMotorS" << "VTOLMotorSW"
|
||||
<< "VTOLMotorW" << "VTOLMotorNW";
|
||||
setupMotors(motorList);
|
||||
// Motor 1 to 8:
|
||||
// Motor 1 to 8, OctoP
|
||||
// -------------------------------------------------------
|
||||
// Motor: 1 2 3 4 5 6 7 8
|
||||
// ROLL {0.00, -0.71, -1.00, -0.71, 0.00, 0.71, 1.00, 0.71}
|
||||
// PITCH {1.00, 0.71, -0.00, -0.71,-1.00,-0.71,-0.00, 0.71}
|
||||
// YAW {-1.00, 1.00, -1.00, 1.00, -1.00, 1.00,-1.00, 1.00}
|
||||
// -------------------------------------------------------
|
||||
// http://wiki.paparazziuav.org/wiki/RotorcraftMixing
|
||||
// pitch roll yaw
|
||||
double mixerMatrix[8][3] = {
|
||||
{ 1, 0, -1 },
|
||||
{ 1, -1, 1 },
|
||||
{ 0, -1, -1 },
|
||||
{ -1, -1, 1 },
|
||||
{ -1, 0, -1 },
|
||||
{ -1, 1, 1 },
|
||||
{ 0, 1, -1 },
|
||||
{ 1, 1, 1 }
|
||||
{ 1, 0, -1 },
|
||||
{ 0.71, -0.71, 1 },
|
||||
{ 0, -1, -1 },
|
||||
{ -0.71, -0.71, 1 },
|
||||
{ -1, 0, -1 },
|
||||
{ -0.71, 0.71, 1 },
|
||||
{ 0, 1, -1 },
|
||||
{ 0.71, 0.71, 1 }
|
||||
};
|
||||
setupMultiRotorMixer(mixerMatrix);
|
||||
m_aircraft->mrStatusLabel->setText("Configuration OK");
|
||||
m_aircraft->mrStatusLabel->setText(tr("Configuration OK"));
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Octocopter X") {
|
||||
airframeType = "OctoX";
|
||||
|
||||
// Show any config errors in GUI
|
||||
if (throwConfigError(8)) {
|
||||
return airframeType;
|
||||
}
|
||||
motorList << "VTOLMotorNNE" << "VTOLMotorENE" << "VTOLMotorESE" << "VTOLMotorSSE" << "VTOLMotorSSW" << "VTOLMotorWSW"
|
||||
<< "VTOLMotorWNW" << "VTOLMotorNNW";
|
||||
setupMotors(motorList);
|
||||
// Motor 1 to 8, OctoX
|
||||
// --------------------------------------------------------
|
||||
// Motor: 1 2 3 4 5 6 7 8
|
||||
// ROLL {-0.41, -1.00, -1.00, -0.41, 0.41, 1.00, 1.00, 0.41}
|
||||
// PITCH {1.00, 0.41, -0.41, -1.00, -1.00, -0.41, 0.41, 1.00}
|
||||
// YAW {-1.00, 1.00, -1.00, 1.00, -1.00, 1.00, -1.00, 1.00}
|
||||
// --------------------------------------------------------
|
||||
// http://wiki.paparazziuav.org/wiki/RotorcraftMixing
|
||||
// pitch roll yaw
|
||||
double mixerMatrix[8][3] = {
|
||||
{ 1, -0.41, -1 },
|
||||
{ 0.41, -1, 1 },
|
||||
{ -0.41, -1, -1 },
|
||||
{ -1, -0.41, 1 },
|
||||
{ -1, 0.41, -1 },
|
||||
{ -0.41, 1, 1 },
|
||||
{ 0.41, 1, -1 },
|
||||
{ 1, 0.41, 1 }
|
||||
};
|
||||
setupMultiRotorMixer(mixerMatrix);
|
||||
m_aircraft->mrStatusLabel->setText(tr("Configuration OK"));
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Octocopter V") {
|
||||
airframeType = "OctoV";
|
||||
|
||||
@ -621,7 +804,7 @@ QString ConfigMultiRotorWidget::updateConfigObjectsFromWidgets()
|
||||
{ 0.33, 1, 1 }
|
||||
};
|
||||
setupMultiRotorMixer(mixerMatrix);
|
||||
m_aircraft->mrStatusLabel->setText("Configuration OK");
|
||||
m_aircraft->mrStatusLabel->setText(tr("Configuration OK"));
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Octo Coax +") {
|
||||
airframeType = "OctoCoaxP";
|
||||
|
||||
@ -645,7 +828,7 @@ QString ConfigMultiRotorWidget::updateConfigObjectsFromWidgets()
|
||||
{ 0, 1, 1 }
|
||||
};
|
||||
setupMultiRotorMixer(mixerMatrix);
|
||||
m_aircraft->mrStatusLabel->setText("Configuration OK");
|
||||
m_aircraft->mrStatusLabel->setText(tr("Configuration OK"));
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Octo Coax X") {
|
||||
airframeType = "OctoCoaxX";
|
||||
|
||||
@ -669,7 +852,7 @@ QString ConfigMultiRotorWidget::updateConfigObjectsFromWidgets()
|
||||
{ -1, 1, 1 }
|
||||
};
|
||||
setupMultiRotorMixer(mixerMatrix);
|
||||
m_aircraft->mrStatusLabel->setText("Configuration OK");
|
||||
m_aircraft->mrStatusLabel->setText(tr("Configuration OK"));
|
||||
} else if (m_aircraft->multirotorFrameType->currentText() == "Tricopter Y") {
|
||||
airframeType = "Tri";
|
||||
|
||||
@ -678,7 +861,7 @@ QString ConfigMultiRotorWidget::updateConfigObjectsFromWidgets()
|
||||
return airframeType;
|
||||
}
|
||||
if (m_aircraft->triYawChannelBox->currentText() == "None") {
|
||||
m_aircraft->mrStatusLabel->setText("<font color='red'>Error: Assign a Yaw channel</font>");
|
||||
m_aircraft->mrStatusLabel->setText(tr("<font color='red'>ERROR: Assign a Yaw channel</font>"));
|
||||
return airframeType;
|
||||
}
|
||||
motorList << "VTOLMotorNW" << "VTOLMotorNE" << "VTOLMotorS";
|
||||
@ -688,7 +871,7 @@ QString ConfigMultiRotorWidget::updateConfigObjectsFromWidgets()
|
||||
config.multi.TRIYaw = m_aircraft->triYawChannelBox->currentIndex();
|
||||
setConfigData(config);
|
||||
|
||||
// Motor 1 to 6, Y6 Layout:
|
||||
// Motor 1 to 3, Tricopter Y Layout:
|
||||
// pitch roll yaw
|
||||
double mixerMatrix[8][3] = {
|
||||
{ 0.5, 1, 0 },
|
||||
@ -748,11 +931,15 @@ void ConfigMultiRotorWidget::updateAirframe(QString frameType)
|
||||
} else if (frameType == "Hexa" || frameType == "Hexacopter") {
|
||||
elementId = "quad-hexa";
|
||||
} else if (frameType == "HexaX" || frameType == "Hexacopter X") {
|
||||
elementId = "quad-hexa-X";
|
||||
} else if (frameType == "HexaH" || frameType == "Hexacopter H") {
|
||||
elementId = "quad-hexa-H";
|
||||
} else if (frameType == "HexaCoax" || frameType == "Hexacopter Y6") {
|
||||
elementId = "hexa-coax";
|
||||
} else if (frameType == "Octo" || frameType == "Octocopter") {
|
||||
elementId = "quad-octo";
|
||||
} else if (frameType == "OctoX" || frameType == "Octocopter X") {
|
||||
elementId = "quad-octo-X";
|
||||
} else if (frameType == "OctoV" || frameType == "Octocopter V") {
|
||||
elementId = "quad-octo-v";
|
||||
} else if (frameType == "OctoCoaxP" || frameType == "Octo Coax +") {
|
||||
@ -824,6 +1011,23 @@ void ConfigMultiRotorWidget::setupMotors(QList<QString> motorList)
|
||||
configData.multi.VTOLMotorW = index;
|
||||
} else if (motor == QString("VTOLMotorNW")) {
|
||||
configData.multi.VTOLMotorNW = index;
|
||||
// OctoX
|
||||
} else if (motor == QString("VTOLMotorNNE")) {
|
||||
configData.multi.VTOLMotorNNE = index;
|
||||
} else if (motor == QString("VTOLMotorENE")) {
|
||||
configData.multi.VTOLMotorENE = index;
|
||||
} else if (motor == QString("VTOLMotorESE")) {
|
||||
configData.multi.VTOLMotorESE = index;
|
||||
} else if (motor == QString("VTOLMotorSSE")) {
|
||||
configData.multi.VTOLMotorSSE = index;
|
||||
} else if (motor == QString("VTOLMotorSSW")) {
|
||||
configData.multi.VTOLMotorSSW = index;
|
||||
} else if (motor == QString("VTOLMotorWSW")) {
|
||||
configData.multi.VTOLMotorWSW = index;
|
||||
} else if (motor == QString("VTOLMotorWNW")) {
|
||||
configData.multi.VTOLMotorWNW = index;
|
||||
} else if (motor == QString("VTOLMotorNNW")) {
|
||||
configData.multi.VTOLMotorNNW = index;
|
||||
}
|
||||
}
|
||||
setConfigData(configData);
|
||||
@ -914,41 +1118,44 @@ bool ConfigMultiRotorWidget::setupHexa(bool pLayout)
|
||||
|
||||
// and set only the relevant channels:
|
||||
|
||||
// Motor 1 to 6, P Layout:
|
||||
// Motor 1 to 6, HexaP Layout
|
||||
// ---------------------------------------------
|
||||
// Motor: 1 2 3 4 5 6
|
||||
// ROLL {0.00, -1.00, -1.00, 0.00, 1.00, 1.00}
|
||||
// PITCH {1.00, 0.50, -0.50, -1.00, -0.50, 0.50}
|
||||
// YAW {-1.00, 1.00, -1.00, 1.00, -1.00, 1.00}
|
||||
// ---------------------------------------------
|
||||
// http://wiki.paparazziuav.org/wiki/RotorcraftMixing
|
||||
// pitch roll yaw
|
||||
// 1 { 0.3 , 0 ,-0.3 // N CW
|
||||
// 2 { 0.3 ,-0.5 , 0.3 // NE CCW
|
||||
// 3 {-0.3 ,-0.5 ,-0.3 // SE CW
|
||||
// 4 {-0.3 , 0 , 0.3 // S CCW
|
||||
// 5 {-0.3 , 0.5 ,-0.3 // SW CW
|
||||
// 6 { 0.3 , 0.5 , 0.3 // NW CCW
|
||||
double pMixer[8][3] = {
|
||||
{ 1, 0, -1 },
|
||||
{ 1, -1, 1 },
|
||||
{ -1, -1, -1 },
|
||||
{ -1, 0, 1 },
|
||||
{ -1, 1, -1 },
|
||||
{ 1, 1, 1 },
|
||||
{ 0, 0, 0 },
|
||||
{ 0, 0, 0 }
|
||||
{ 1, 0, -1 },
|
||||
{ 0.5, -1, 1 },
|
||||
{ -0.5, -1, -1 },
|
||||
{ -1, 0, 1 },
|
||||
{ -0.5, 1, -1 },
|
||||
{ 0.5, 1, 1 },
|
||||
{ 0, 0, 0 },
|
||||
{ 0, 0, 0 }
|
||||
};
|
||||
|
||||
// Motor 1 to 6, X Layout:
|
||||
// 1 [ 0.5, -0.3, -0.3 ] NE
|
||||
// 2 [ 0 , -0.3, 0.3 ] E
|
||||
// 3 [ -0.5, -0.3, -0.3 ] SE
|
||||
// 4 [ -0.5, 0.3, 0.3 ] SW
|
||||
// 5 [ 0 , 0.3, -0.3 ] W
|
||||
// 6 [ 0.5, 0.3, 0.3 ] NW
|
||||
// Motor 1 to 6, HexaX Layout
|
||||
// ---------------------------------------------
|
||||
// Motor: 1 2 3 4 5 6
|
||||
// ROLL {-0.50, -1.00, -0.50, 0.50, 1.00, 0.50}
|
||||
// PITCH {1.00, 0.00, -1.00, -1.00, -0.00, 1.00}
|
||||
// YAW {-1.00, 1.00, -1.00, 1.00, -1.00, 1.00}
|
||||
// ---------------------------------------------
|
||||
// http://wiki.paparazziuav.org/wiki/RotorcraftMixing
|
||||
// pitch roll yaw
|
||||
double xMixer[8][3] = {
|
||||
{ 1, -1, -1 },
|
||||
{ 0, -1, 1 },
|
||||
{ -1, -1, -1 },
|
||||
{ -1, 1, 1 },
|
||||
{ 0, 1, -1 },
|
||||
{ 1, 1, 1 },
|
||||
{ 0, 0, 0 },
|
||||
{ 0, 0, 0 }
|
||||
{ 1, -0.5, -1 },
|
||||
{ 0, -1, 1 },
|
||||
{ -1, -0.5, -1 },
|
||||
{ -1, 0.5, 1 },
|
||||
{ 0, 1, -1 },
|
||||
{ 1, 0.5, 1 },
|
||||
{ 0, 0, 0 },
|
||||
{ 0, 0, 0 }
|
||||
};
|
||||
|
||||
if (pLayout) {
|
||||
@ -956,7 +1163,7 @@ bool ConfigMultiRotorWidget::setupHexa(bool pLayout)
|
||||
} else {
|
||||
setupMultiRotorMixer(xMixer);
|
||||
}
|
||||
m_aircraft->mrStatusLabel->setText("Configuration OK");
|
||||
m_aircraft->mrStatusLabel->setText(tr("Configuration OK"));
|
||||
return true;
|
||||
}
|
||||
|
||||
@ -1021,7 +1228,7 @@ bool ConfigMultiRotorWidget::throwConfigError(int numMotors)
|
||||
|
||||
if (error) {
|
||||
m_aircraft->mrStatusLabel->setText(
|
||||
QString("<font color='red'>ERROR: Assign all %1 motor channels</font>").arg(numMotors));
|
||||
QString(tr("<font color='red'>ERROR: Assign all %1 motor channels</font>")).arg(numMotors));
|
||||
}
|
||||
return error;
|
||||
}
|
||||
|
@ -42,6 +42,15 @@ typedef struct {
|
||||
uint VTOLMotorNE : 4;
|
||||
uint VTOLMotorSW : 4;
|
||||
uint VTOLMotorSE : 4; // 32 bits
|
||||
// OctoX
|
||||
uint VTOLMotorNNE : 4;
|
||||
uint VTOLMotorENE : 4;
|
||||
uint VTOLMotorESE : 4;
|
||||
uint VTOLMotorSSE : 4;
|
||||
uint VTOLMotorSSW : 4;
|
||||
uint VTOLMotorWSW : 4;
|
||||
uint VTOLMotorWNW : 4;
|
||||
uint VTOLMotorNNW : 4; // 32 bits
|
||||
uint TRIYaw : 4;
|
||||
quint32 padding : 28; // 64 bits
|
||||
quint32 padding1;
|
||||
|
@ -85,6 +85,7 @@ QStringList ConfigVehicleTypeWidget::getChannelDescriptions()
|
||||
case SystemSettings::AIRFRAMETYPE_OCTOCOAXX:
|
||||
case SystemSettings::AIRFRAMETYPE_OCTOCOAXP:
|
||||
case SystemSettings::AIRFRAMETYPE_OCTO:
|
||||
case SystemSettings::AIRFRAMETYPE_OCTOX:
|
||||
case SystemSettings::AIRFRAMETYPE_HEXAX:
|
||||
case SystemSettings::AIRFRAMETYPE_HEXACOAX:
|
||||
case SystemSettings::AIRFRAMETYPE_HEXA:
|
||||
@ -263,8 +264,11 @@ int ConfigVehicleTypeWidget::frameCategory(QString frameType)
|
||||
} else if (frameType == "Tri" || frameType == "Tricopter Y" || frameType == "QuadX" || frameType == "Quad X"
|
||||
|| frameType == "QuadP" || frameType == "Quad +" || frameType == "Hexa" || frameType == "Hexacopter"
|
||||
|| frameType == "HexaX" || frameType == "Hexacopter X" || frameType == "HexaCoax"
|
||||
|| frameType == "Hexacopter Y6" || frameType == "Octo" || frameType == "Octocopter" || frameType == "OctoV"
|
||||
|| frameType == "Octocopter V" || frameType == "OctoCoaxP" || frameType == "Octo Coax +"
|
||||
|| frameType == "HexaH" || frameType == "Hexacopter H" || frameType == "Hexacopter Y6"
|
||||
|| frameType == "Octo" || frameType == "Octocopter"
|
||||
|| frameType == "OctoX" || frameType == "Octocopter X"
|
||||
|| frameType == "OctoV" || frameType == "Octocopter V"
|
||||
|| frameType == "OctoCoaxP" || frameType == "Octo Coax +"
|
||||
|| frameType == "OctoCoaxX" || frameType == "Octo Coax X") {
|
||||
return ConfigVehicleTypeWidget::MULTIROTOR;
|
||||
} else if (frameType == "HeliCP") {
|
||||
|
File diff suppressed because one or more lines are too long
Before Width: | Height: | Size: 758 KiB After Width: | Height: | Size: 898 KiB |
@ -107,6 +107,9 @@ void ConnectionDiagram::setupGraphicsScene()
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA:
|
||||
elementsToShow << "hexa";
|
||||
break;
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_X:
|
||||
elementsToShow << "hexa-x";
|
||||
break;
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_COAX_Y:
|
||||
elementsToShow << "hexa-y";
|
||||
break;
|
||||
|
@ -101,11 +101,15 @@ void MultiPage::setupMultiTypesCombo()
|
||||
ui->typeCombo->addItem(tr("Hexacopter"), SetupWizard::MULTI_ROTOR_HEXA);
|
||||
m_descriptions << tr("Hexacopter");
|
||||
|
||||
ui->typeCombo->addItem(tr("Hexacopter X"), SetupWizard::MULTI_ROTOR_HEXA_X);
|
||||
m_descriptions << tr("Hexacopter X");
|
||||
|
||||
ui->typeCombo->addItem(tr("Hexacopter H"), SetupWizard::MULTI_ROTOR_HEXA_H);
|
||||
m_descriptions << tr("Hexacopter H");
|
||||
|
||||
ui->typeCombo->addItem(tr("Hexacopter Coax (Y6)"), SetupWizard::MULTI_ROTOR_HEXA_COAX_Y);
|
||||
m_descriptions << tr("Hexacopter Coax (Y6)");
|
||||
|
||||
ui->typeCombo->addItem(tr("Hexacopter X"), SetupWizard::MULTI_ROTOR_HEXA_H);
|
||||
m_descriptions << tr("Hexacopter H");
|
||||
|
||||
// Fredrik Arvidsson(m_thread) 2012-08-26 Disable Octos until further notice
|
||||
/*
|
||||
@ -159,6 +163,9 @@ void MultiPage::updateImageAndDescription()
|
||||
case SetupWizard::MULTI_ROTOR_HEXA_H:
|
||||
elementId = "quad-hexa-H";
|
||||
break;
|
||||
case SetupWizard::MULTI_ROTOR_HEXA_X:
|
||||
elementId = "quad-hexa-X";
|
||||
break;
|
||||
case SetupWizard::MULTI_ROTOR_OCTO:
|
||||
elementId = "quad-octo";
|
||||
break;
|
||||
|
@ -104,6 +104,12 @@ void OutputCalibrationPage::setupVehicle()
|
||||
m_vehicleHighlightElementIndexes << 0 << 1 << 2 << 3 << 4 << 5 << 6;
|
||||
m_channelIndex << 0 << 0 << 1 << 2 << 3 << 4 << 5;
|
||||
break;
|
||||
case SetupWizard::MULTI_ROTOR_HEXA_X:
|
||||
m_wizardIndexes << 0 << 1 << 1 << 1 << 1 << 1 << 1;
|
||||
m_vehicleElementIds << "hexa-x" << "hexa-x-frame" << "hexa-x-m1" << "hexa-x-m2" << "hexa-x-m3" << "hexa-x-m4" << "hexa-x-m5" << "hexa-x-m6";
|
||||
m_vehicleHighlightElementIndexes << 0 << 1 << 2 << 3 << 4 << 5 << 6;
|
||||
m_channelIndex << 0 << 0 << 1 << 2 << 3 << 4 << 5;
|
||||
break;
|
||||
default:
|
||||
break;
|
||||
}
|
||||
|
File diff suppressed because one or more lines are too long
Before Width: | Height: | Size: 483 KiB After Width: | Height: | Size: 524 KiB |
File diff suppressed because one or more lines are too long
Before Width: | Height: | Size: 431 KiB After Width: | Height: | Size: 432 KiB |
@ -204,6 +204,9 @@ QString SetupWizard::getSummaryText()
|
||||
summary.append(tr("Hexacopter Coax (Y6)"));
|
||||
break;
|
||||
case SetupWizard::MULTI_ROTOR_HEXA_H:
|
||||
summary.append(tr("Hexacopter H"));
|
||||
break;
|
||||
case SetupWizard::MULTI_ROTOR_HEXA_X:
|
||||
summary.append(tr("Hexacopter X"));
|
||||
break;
|
||||
case SetupWizard::MULTI_ROTOR_OCTO:
|
||||
|
@ -202,9 +202,11 @@ void VehicleConfigurationHelper::applyVehicleConfiguration()
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_COAX_Y:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_H:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_X:
|
||||
setupHexaCopter();
|
||||
break;
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_X:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_COAX_X:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_COAX_PLUS:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_V:
|
||||
@ -279,7 +281,9 @@ void VehicleConfigurationHelper::applyActuatorConfiguration()
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_COAX_Y:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_H:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_X:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_X:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_COAX_X:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_COAX_PLUS:
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_V:
|
||||
@ -633,8 +637,9 @@ void VehicleConfigurationHelper::resetVehicleConfig()
|
||||
for (int i = 1; i <= 2; i++) {
|
||||
UAVObjectField *field = mSettings->getField(throttlePattern.arg(i));
|
||||
Q_ASSERT(field);
|
||||
// Wizard support only Multirotors - Set default curve with 90% max
|
||||
for (quint32 i = 0; i < field->getNumElements(); i++) {
|
||||
field->setValue(i * (1.0f / (field->getNumElements() - 1)), i);
|
||||
field->setValue(i * (0.9f / (field->getNumElements() - 1)), i);
|
||||
}
|
||||
}
|
||||
|
||||
@ -831,48 +836,55 @@ void VehicleConfigurationHelper::setupHexaCopter()
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA:
|
||||
{
|
||||
frame = SystemSettings::AIRFRAMETYPE_HEXA;
|
||||
|
||||
// HexaPlus according to new mixer table and pitch-roll-yaw mixing at 100%
|
||||
// Pitch Roll Yaw
|
||||
// M1 { 1 , 0 , -1 },
|
||||
// M2 { 0.5, -1, 1 },
|
||||
// M3 { -0.5, -1, -1 },
|
||||
// M4 { -1 , 0 , 1 },
|
||||
// M5 { -0.5, 1 , -1 },
|
||||
// M6 { 0.5, 1 , 1 },
|
||||
channels[0].type = MIXER_TYPE_MOTOR;
|
||||
channels[0].throttle1 = 100;
|
||||
channels[0].throttle2 = 0;
|
||||
channels[0].roll = 0;
|
||||
channels[0].pitch = 33;
|
||||
channels[0].yaw = -33;
|
||||
channels[0].pitch = 100;
|
||||
channels[0].yaw = -100;
|
||||
|
||||
channels[1].type = MIXER_TYPE_MOTOR;
|
||||
channels[1].throttle1 = 100;
|
||||
channels[1].throttle2 = 0;
|
||||
channels[1].roll = -50;
|
||||
channels[1].pitch = 33;
|
||||
channels[1].yaw = 33;
|
||||
channels[1].roll = -100;
|
||||
channels[1].pitch = 50;
|
||||
channels[1].yaw = 100;
|
||||
|
||||
channels[2].type = MIXER_TYPE_MOTOR;
|
||||
channels[2].throttle1 = 100;
|
||||
channels[2].throttle2 = 0;
|
||||
channels[2].roll = -50;
|
||||
channels[2].pitch = -33;
|
||||
channels[2].yaw = -33;
|
||||
channels[2].roll = -100;
|
||||
channels[2].pitch = -50;
|
||||
channels[2].yaw = -100;
|
||||
|
||||
channels[3].type = MIXER_TYPE_MOTOR;
|
||||
channels[3].throttle1 = 100;
|
||||
channels[3].throttle2 = 0;
|
||||
channels[3].roll = 0;
|
||||
channels[3].pitch = -33;
|
||||
channels[3].yaw = 33;
|
||||
channels[3].pitch = -100;
|
||||
channels[3].yaw = 100;
|
||||
|
||||
channels[4].type = MIXER_TYPE_MOTOR;
|
||||
channels[4].throttle1 = 100;
|
||||
channels[4].throttle2 = 0;
|
||||
channels[4].roll = 50;
|
||||
channels[4].pitch = -33;
|
||||
channels[4].yaw = -33;
|
||||
channels[4].roll = 100;
|
||||
channels[4].pitch = -50;
|
||||
channels[4].yaw = -100;
|
||||
|
||||
channels[5].type = MIXER_TYPE_MOTOR;
|
||||
channels[5].throttle1 = 100;
|
||||
channels[5].throttle2 = 0;
|
||||
channels[5].roll = 50;
|
||||
channels[5].pitch = 33;
|
||||
channels[5].yaw = 33;
|
||||
channels[5].roll = 100;
|
||||
channels[5].pitch = 50;
|
||||
channels[5].yaw = 100;
|
||||
|
||||
guiSettings.multi.VTOLMotorN = 1;
|
||||
guiSettings.multi.VTOLMotorNE = 2;
|
||||
@ -940,49 +952,118 @@ void VehicleConfigurationHelper::setupHexaCopter()
|
||||
}
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_H:
|
||||
{
|
||||
frame = SystemSettings::AIRFRAMETYPE_HEXAX;
|
||||
|
||||
frame = SystemSettings::AIRFRAMETYPE_HEXAH;
|
||||
// HexaH according to new mixer table and pitch-roll-yaw mixing at 100%
|
||||
// Pitch Roll Yaw
|
||||
// M1 { 1 , -0.5, -0.5 },
|
||||
// M2 { 0 , -1 , 1 },
|
||||
// M3 { -1 , -0.5, -0.5 },
|
||||
// M4 { -1 , 0.5, 0.5 },
|
||||
// M5 { 0 , 1 , -1 },
|
||||
// M6 { 1 , 0.5, 0.5 },
|
||||
channels[0].type = MIXER_TYPE_MOTOR;
|
||||
channels[0].throttle1 = 100;
|
||||
channels[0].throttle2 = 0;
|
||||
channels[0].roll = -33;
|
||||
channels[0].pitch = 50;
|
||||
channels[0].yaw = -33;
|
||||
channels[0].roll = -50;
|
||||
channels[0].pitch = 100;
|
||||
channels[0].yaw = -50;
|
||||
|
||||
channels[1].type = MIXER_TYPE_MOTOR;
|
||||
channels[1].throttle1 = 100;
|
||||
channels[1].throttle2 = 0;
|
||||
channels[1].roll = -33;
|
||||
channels[1].roll = -100;
|
||||
channels[1].pitch = 0;
|
||||
channels[1].yaw = 33;
|
||||
channels[1].yaw = 100;
|
||||
|
||||
channels[2].type = MIXER_TYPE_MOTOR;
|
||||
channels[2].throttle1 = 100;
|
||||
channels[2].throttle2 = 0;
|
||||
channels[2].roll = -33;
|
||||
channels[2].pitch = -50;
|
||||
channels[2].yaw = -33;
|
||||
channels[2].roll = -50;
|
||||
channels[2].pitch = -100;
|
||||
channels[2].yaw = -50;
|
||||
|
||||
channels[3].type = MIXER_TYPE_MOTOR;
|
||||
channels[3].throttle1 = 100;
|
||||
channels[3].throttle2 = 0;
|
||||
channels[3].roll = -33;
|
||||
channels[3].pitch = -50;
|
||||
channels[3].yaw = 33;
|
||||
channels[3].roll = 50;
|
||||
channels[3].pitch = -100;
|
||||
channels[3].yaw = 50;
|
||||
|
||||
channels[4].type = MIXER_TYPE_MOTOR;
|
||||
channels[4].throttle1 = 100;
|
||||
channels[4].throttle2 = 0;
|
||||
channels[4].roll = 33;
|
||||
channels[4].roll = 100;
|
||||
channels[4].pitch = 0;
|
||||
channels[4].yaw = -33;
|
||||
channels[4].yaw = -100;
|
||||
|
||||
channels[5].type = MIXER_TYPE_MOTOR;
|
||||
channels[5].throttle1 = 100;
|
||||
channels[5].throttle2 = 0;
|
||||
channels[5].roll = 33;
|
||||
channels[5].pitch = 50;
|
||||
channels[5].yaw = -33;
|
||||
channels[5].roll = 50;
|
||||
channels[5].pitch = 100;
|
||||
channels[5].yaw = 50;
|
||||
|
||||
guiSettings.multi.VTOLMotorNE = 1;
|
||||
guiSettings.multi.VTOLMotorE = 2;
|
||||
guiSettings.multi.VTOLMotorSE = 3;
|
||||
guiSettings.multi.VTOLMotorSW = 4;
|
||||
guiSettings.multi.VTOLMotorW = 5;
|
||||
guiSettings.multi.VTOLMotorNW = 6;
|
||||
|
||||
break;
|
||||
}
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_HEXA_X:
|
||||
{
|
||||
frame = SystemSettings::AIRFRAMETYPE_HEXAH;
|
||||
// HexaX according to new mixer table and pitch-roll-yaw mixing at 100%
|
||||
// Pitch Roll Yaw
|
||||
// M1 { 1, -0.5, -1 },
|
||||
// M2 { 0, -1 , 1 },
|
||||
// M3 { -1, -0.5, -1 },
|
||||
// M4 { -1, 0.5, 1 },
|
||||
// M5 { 0, 1 , -1 },
|
||||
// M6 { 1, 0.5, 1 },
|
||||
channels[0].type = MIXER_TYPE_MOTOR;
|
||||
channels[0].throttle1 = 100;
|
||||
channels[0].throttle2 = 0;
|
||||
channels[0].roll = -50;
|
||||
channels[0].pitch = 100;
|
||||
channels[0].yaw = -100;
|
||||
|
||||
channels[1].type = MIXER_TYPE_MOTOR;
|
||||
channels[1].throttle1 = 100;
|
||||
channels[1].throttle2 = 0;
|
||||
channels[1].roll = -100;
|
||||
channels[1].pitch = 0;
|
||||
channels[1].yaw = 100;
|
||||
|
||||
channels[2].type = MIXER_TYPE_MOTOR;
|
||||
channels[2].throttle1 = 100;
|
||||
channels[2].throttle2 = 0;
|
||||
channels[2].roll = -50;
|
||||
channels[2].pitch = -100;
|
||||
channels[2].yaw = -100;
|
||||
|
||||
channels[3].type = MIXER_TYPE_MOTOR;
|
||||
channels[3].throttle1 = 100;
|
||||
channels[3].throttle2 = 0;
|
||||
channels[3].roll = 50;
|
||||
channels[3].pitch = -100;
|
||||
channels[3].yaw = 100;
|
||||
|
||||
channels[4].type = MIXER_TYPE_MOTOR;
|
||||
channels[4].throttle1 = 100;
|
||||
channels[4].throttle2 = 0;
|
||||
channels[4].roll = 100;
|
||||
channels[4].pitch = 0;
|
||||
channels[4].yaw = -100;
|
||||
|
||||
channels[5].type = MIXER_TYPE_MOTOR;
|
||||
channels[5].throttle1 = 100;
|
||||
channels[5].throttle2 = 0;
|
||||
channels[5].roll = 50;
|
||||
channels[5].pitch = 100;
|
||||
channels[5].yaw = 100;
|
||||
|
||||
guiSettings.multi.VTOLMotorNE = 1;
|
||||
guiSettings.multi.VTOLMotorE = 2;
|
||||
@ -1010,62 +1091,71 @@ void VehicleConfigurationHelper::setupOctoCopter()
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO:
|
||||
{
|
||||
frame = SystemSettings::AIRFRAMETYPE_OCTO;
|
||||
|
||||
// OctoP according to new mixer table and pitch-roll-yaw mixing at 100%
|
||||
// Pitch Roll Yaw
|
||||
// M1{ 1 , 0 , -1 },
|
||||
// M2{ 0.71,-0.71, 1 },
|
||||
// M3{ 0 ,-1 , -1 },
|
||||
// M4{ -0.71,-0.71, 1 },
|
||||
// M5{ -1 , 0 , -1 },
|
||||
// M6{ -0.71, 0.71, 1 },
|
||||
// M7{ 0 , 1 , -1 },
|
||||
// M8{ 0.71, 0.71, 1 }
|
||||
channels[0].type = MIXER_TYPE_MOTOR;
|
||||
channels[0].throttle1 = 100;
|
||||
channels[0].throttle2 = 0;
|
||||
channels[0].roll = 0;
|
||||
channels[0].pitch = 33;
|
||||
channels[0].yaw = -25;
|
||||
channels[0].pitch = 100;
|
||||
channels[0].yaw = -100;
|
||||
|
||||
channels[1].type = MIXER_TYPE_MOTOR;
|
||||
channels[1].throttle1 = 100;
|
||||
channels[1].throttle2 = 0;
|
||||
channels[1].roll = -33;
|
||||
channels[1].pitch = 33;
|
||||
channels[1].yaw = 25;
|
||||
channels[1].roll = -71;
|
||||
channels[1].pitch = 71;
|
||||
channels[1].yaw = 100;
|
||||
|
||||
channels[2].type = MIXER_TYPE_MOTOR;
|
||||
channels[2].throttle1 = 100;
|
||||
channels[2].throttle2 = 0;
|
||||
channels[2].roll = -33;
|
||||
channels[2].roll = -71;
|
||||
channels[2].pitch = 0;
|
||||
channels[2].yaw = -25;
|
||||
channels[2].yaw = -100;
|
||||
|
||||
channels[3].type = MIXER_TYPE_MOTOR;
|
||||
channels[3].throttle1 = 100;
|
||||
channels[3].throttle2 = 0;
|
||||
channels[3].roll = -33;
|
||||
channels[3].pitch = -33;
|
||||
channels[3].yaw = 25;
|
||||
channels[3].roll = -71;
|
||||
channels[3].pitch = -71;
|
||||
channels[3].yaw = 100;
|
||||
|
||||
channels[4].type = MIXER_TYPE_MOTOR;
|
||||
channels[4].throttle1 = 100;
|
||||
channels[4].throttle2 = 0;
|
||||
channels[4].roll = 0;
|
||||
channels[4].pitch = -33;
|
||||
channels[4].yaw = -25;
|
||||
channels[4].pitch = -100;
|
||||
channels[4].yaw = -100;
|
||||
|
||||
channels[5].type = MIXER_TYPE_MOTOR;
|
||||
channels[5].throttle1 = 100;
|
||||
channels[5].throttle2 = 0;
|
||||
channels[5].roll = 33;
|
||||
channels[5].pitch = -33;
|
||||
channels[5].yaw = 25;
|
||||
channels[5].roll = 71;
|
||||
channels[5].pitch = -71;
|
||||
channels[5].yaw = 100;
|
||||
|
||||
channels[6].type = MIXER_TYPE_MOTOR;
|
||||
channels[6].throttle1 = 100;
|
||||
channels[6].throttle2 = 0;
|
||||
channels[6].roll = 33;
|
||||
channels[6].roll = 100;
|
||||
channels[6].pitch = 0;
|
||||
channels[6].yaw = -25;
|
||||
channels[6].yaw = -100;
|
||||
|
||||
channels[7].type = MIXER_TYPE_MOTOR;
|
||||
channels[7].throttle1 = 100;
|
||||
channels[7].throttle2 = 0;
|
||||
channels[7].roll = 33;
|
||||
channels[7].pitch = 33;
|
||||
channels[7].yaw = 25;
|
||||
channels[7].roll = 71;
|
||||
channels[7].pitch = 71;
|
||||
channels[7].yaw = 100;
|
||||
|
||||
guiSettings.multi.VTOLMotorN = 1;
|
||||
guiSettings.multi.VTOLMotorNE = 2;
|
||||
@ -1078,6 +1168,86 @@ void VehicleConfigurationHelper::setupOctoCopter()
|
||||
|
||||
break;
|
||||
}
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_X:
|
||||
{
|
||||
frame = SystemSettings::AIRFRAMETYPE_OCTOX;
|
||||
// OctoX according to new mixer table and pitch-roll-yaw mixing at 100%
|
||||
// Pitch Roll Yaw
|
||||
// M1{ 1 ,-0.41, -1 },
|
||||
// M2{ 0.41, -1 , 1 },
|
||||
// M3{ -0.41, -1 , -1 },
|
||||
// M4{ -1 ,-0.41, 1 },
|
||||
// M5{ -1 , 0.41, -1 },
|
||||
// M6{ -0.41, 1 , 1 },
|
||||
// M7{ 0.41, 1 , -1 },
|
||||
// M8{ 1 , 0.41, 1 }
|
||||
channels[0].type = MIXER_TYPE_MOTOR;
|
||||
channels[0].throttle1 = 100;
|
||||
channels[0].throttle2 = 0;
|
||||
channels[0].roll = -41;
|
||||
channels[0].pitch = 100;
|
||||
channels[0].yaw = -100;
|
||||
|
||||
channels[1].type = MIXER_TYPE_MOTOR;
|
||||
channels[1].throttle1 = 100;
|
||||
channels[1].throttle2 = 0;
|
||||
channels[1].roll = -100;
|
||||
channels[1].pitch = 41;
|
||||
channels[1].yaw = 100;
|
||||
|
||||
channels[2].type = MIXER_TYPE_MOTOR;
|
||||
channels[2].throttle1 = 100;
|
||||
channels[2].throttle2 = 0;
|
||||
channels[2].roll = -100;
|
||||
channels[2].pitch = -41;
|
||||
channels[2].yaw = -100;
|
||||
|
||||
channels[3].type = MIXER_TYPE_MOTOR;
|
||||
channels[3].throttle1 = 100;
|
||||
channels[3].throttle2 = 0;
|
||||
channels[3].roll = -41;
|
||||
channels[3].pitch = -100;
|
||||
channels[3].yaw = 100;
|
||||
|
||||
channels[4].type = MIXER_TYPE_MOTOR;
|
||||
channels[4].throttle1 = 100;
|
||||
channels[4].throttle2 = 0;
|
||||
channels[4].roll = 41;
|
||||
channels[4].pitch = -100;
|
||||
channels[4].yaw = -100;
|
||||
|
||||
channels[5].type = MIXER_TYPE_MOTOR;
|
||||
channels[5].throttle1 = 100;
|
||||
channels[5].throttle2 = 0;
|
||||
channels[5].roll = 100;
|
||||
channels[5].pitch = -41;
|
||||
channels[5].yaw = 100;
|
||||
|
||||
channels[6].type = MIXER_TYPE_MOTOR;
|
||||
channels[6].throttle1 = 100;
|
||||
channels[6].throttle2 = 0;
|
||||
channels[6].roll = 100;
|
||||
channels[6].pitch = 41;
|
||||
channels[6].yaw = -100;
|
||||
|
||||
channels[7].type = MIXER_TYPE_MOTOR;
|
||||
channels[7].throttle1 = 100;
|
||||
channels[7].throttle2 = 0;
|
||||
channels[7].roll = 41;
|
||||
channels[7].pitch = 100;
|
||||
channels[7].yaw = 100;
|
||||
|
||||
guiSettings.multi.VTOLMotorNNE = 1;
|
||||
guiSettings.multi.VTOLMotorENE = 2;
|
||||
guiSettings.multi.VTOLMotorESE = 3;
|
||||
guiSettings.multi.VTOLMotorSSE = 4;
|
||||
guiSettings.multi.VTOLMotorSSW = 5;
|
||||
guiSettings.multi.VTOLMotorWSW = 6;
|
||||
guiSettings.multi.VTOLMotorWNW = 7;
|
||||
guiSettings.multi.VTOLMotorNNW = 8;
|
||||
|
||||
break;
|
||||
}
|
||||
case VehicleConfigurationSource::MULTI_ROTOR_OCTO_COAX_X:
|
||||
{
|
||||
frame = SystemSettings::AIRFRAMETYPE_OCTOCOAXX;
|
||||
|
@ -58,9 +58,9 @@ public:
|
||||
enum CONTROLLER_TYPE { CONTROLLER_UNKNOWN, CONTROLLER_CC, CONTROLLER_CC3D, CONTROLLER_REVO, CONTROLLER_OPLINK };
|
||||
enum VEHICLE_TYPE { VEHICLE_UNKNOWN, VEHICLE_MULTI, VEHICLE_FIXEDWING, VEHICLE_HELI, VEHICLE_SURFACE };
|
||||
enum VEHICLE_SUB_TYPE { MULTI_ROTOR_UNKNOWN, MULTI_ROTOR_TRI_Y, MULTI_ROTOR_QUAD_X, MULTI_ROTOR_QUAD_PLUS,
|
||||
MULTI_ROTOR_HEXA, MULTI_ROTOR_HEXA_H, MULTI_ROTOR_HEXA_COAX_Y, MULTI_ROTOR_OCTO,
|
||||
MULTI_ROTOR_OCTO_V, MULTI_ROTOR_OCTO_COAX_X, MULTI_ROTOR_OCTO_COAX_PLUS, FIXED_WING_AILERON,
|
||||
FIXED_WING_VTAIL, HELI_CCPM };
|
||||
MULTI_ROTOR_HEXA, MULTI_ROTOR_HEXA_H, MULTI_ROTOR_HEXA_X, MULTI_ROTOR_HEXA_COAX_Y, MULTI_ROTOR_OCTO,
|
||||
MULTI_ROTOR_OCTO_X, MULTI_ROTOR_OCTO_V, MULTI_ROTOR_OCTO_COAX_X, MULTI_ROTOR_OCTO_COAX_PLUS,
|
||||
FIXED_WING_AILERON, FIXED_WING_VTAIL, HELI_CCPM };
|
||||
enum ESC_TYPE { ESC_RAPID, ESC_LEGACY, ESC_UNKNOWN };
|
||||
enum INPUT_TYPE { INPUT_PWM, INPUT_PPM, INPUT_SBUS, INPUT_DSMX10, INPUT_DSMX11, INPUT_DSM2, INPUT_UNKNOWN };
|
||||
|
||||
|
@ -1,7 +1,7 @@
|
||||
<xml>
|
||||
<object name="SystemSettings" singleinstance="true" settings="true" category="System">
|
||||
<description>Select airframe type. Currently used by @ref ActuatorModule to choose mixing from @ref ActuatorDesired to @ref ActuatorCommand</description>
|
||||
<field name="AirframeType" units="" type="enum" elements="1" options="FixedWing,FixedWingElevon,FixedWingVtail,VTOL,HeliCP,QuadX,QuadP,Hexa,Octo,Custom,HexaX,OctoV,OctoCoaxP,OctoCoaxX,HexaCoax,Tri,GroundVehicleCar,GroundVehicleDifferential,GroundVehicleMotorcycle" defaultvalue="QuadX"/>
|
||||
<field name="AirframeType" units="" type="enum" elements="1" options="FixedWing,FixedWingElevon,FixedWingVtail,VTOL,HeliCP,QuadX,QuadP,Hexa,Octo,Custom,HexaX,HexaH,OctoV,OctoCoaxP,OctoCoaxX,OctoX,HexaCoax,Tri,GroundVehicleCar,GroundVehicleDifferential,GroundVehicleMotorcycle" defaultvalue="QuadX"/>
|
||||
<field name="ThrustControl" units="" type="enum" elements="1" options="Throttle,Collective,None" defaultvalue="Throttle" />
|
||||
<!-- Which way the vehicle controls its thrust. Can be through
|
||||
"Throttle" (quadcopter, simple brushless planes,
|
||||
|
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Reference in New Issue
Block a user