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Code Issues Releases Activity

Merge remote-tracking branch 'remotes/origin/next' into sambas/diffnext

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Conflicts:
	flight/modules/VtolPathFollower/vtolpathfollower.c
This commit is contained in:
sambas 2013-04-28 09:46:14 +03:00
commit 38d9d5dde3
4 changed files with 2887 additions and 2886 deletions
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18
flight/modules/VtolPathFollower/vtolpathfollower.c
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@ -481,12 +481,12 @@ void updateEndpointVelocity()
HomeLocationGet(&homeLocation); HomeLocationGet(&homeLocation);
float lat = DEG2RAD(homeLocation.Latitude / 10.0e6f); float lat = DEG2RAD(homeLocation.Latitude / 10.0e6f);
float alt = homeLocation.Altitude; float alt = homeLocation.Altitude;
float T[3] = float T[3] = { alt+6.378137E6f,
{ alt + 6.378137E6f, cosf(lat) * (alt + 6.378137E6f), -1.0f }; cosf(lat)*(alt+6.378137E6f),
float NED[3] = -1.0f};
{ T[0] * (DEG2RAD((gpsPosition.Latitude - homeLocation.Latitude) / 10.0e6f)), T[1] float NED[3] = {T[0] * (DEG2RAD((gpsPosition.Latitude - homeLocation.Latitude) / 10.0e6f)),
* (DEG2RAD((gpsPosition.Longitude - homeLocation.Longitude) / 10.0e6f)), T[2] T[1] * (DEG2RAD((gpsPosition.Longitude - homeLocation.Longitude) / 10.0e6f)),
* ((gpsPosition.Altitude + gpsPosition.GeoidSeparation - homeLocation.Altitude)) }; T[2] * ((gpsPosition.Altitude + gpsPosition.GeoidSeparation - homeLocation.Altitude))};
northPos = NED[0]; northPos = NED[0];
eastPos = NED[1]; eastPos = NED[1];
@ -654,9 +654,11 @@ static void updateVtolDesiredAttitude(bool yaw_attitude)
// Project the north and east command signals into the pitch and roll based on yaw. For this to behave well the // Project the north and east command signals into the pitch and roll based on yaw. For this to behave well the
// craft should move similarly for 5 deg roll versus 5 deg pitch // craft should move similarly for 5 deg roll versus 5 deg pitch
stabDesired.Pitch = bound(-northCommand * cosf(DEG2RAD(attitudeActual.Yaw)) + -eastCommand * sinf(DEG2RAD(attitudeActual.Yaw)), stabDesired.Pitch = bound(-northCommand * cosf(DEG2RAD(attitudeActual.Yaw)) +
-eastCommand * sinf(DEG2RAD(attitudeActual.Yaw)),
-vtolpathfollowerSettings.MaxRollPitch, vtolpathfollowerSettings.MaxRollPitch); -vtolpathfollowerSettings.MaxRollPitch, vtolpathfollowerSettings.MaxRollPitch);
stabDesired.Roll = bound(-northCommand * sinf(DEG2RAD(attitudeActual.Yaw)) + eastCommand * cosf(DEG2RAD(attitudeActual.Yaw)), stabDesired.Roll = bound(-northCommand * sinf(DEG2RAD(attitudeActual.Yaw)) +
eastCommand * cosf(DEG2RAD(attitudeActual.Yaw)),
-vtolpathfollowerSettings.MaxRollPitch, vtolpathfollowerSettings.MaxRollPitch); -vtolpathfollowerSettings.MaxRollPitch, vtolpathfollowerSettings.MaxRollPitch);
if (vtolpathfollowerSettings.ThrottleControl == VTOLPATHFOLLOWERSETTINGS_THROTTLECONTROL_FALSE) { if (vtolpathfollowerSettings.ThrottleControl == VTOLPATHFOLLOWERSETTINGS_THROTTLECONTROL_FALSE) {

1
ground/openpilotgcs/share/openpilotgcs/default_configurations/OpenPilotGCS.xml
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@ -2744,7 +2744,6 @@
<Mode5> <Mode5>
<showToolbars>false</showToolbars> <showToolbars>false</showToolbars>
<splitter> <splitter>
<side0>
<side0> <side0>
<classId>HITL</classId> <classId>HITL</classId>
<gadget> <gadget>

2
ground/openpilotgcs/src/plugins/config/revosensors.ui
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@ -51,7 +51,7 @@
</font> </font>
</property> </property>
<property name="text"> <property name="text">
<string>#1: Magnetometer calibrtion</string> <string>#1: Magnetometer calibration</string>
</property> </property>
</widget> </widget>
</item> </item>

2
shared/uavobjectdefinition/stabilizationsettings.xml
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@ -5,7 +5,7 @@
<field name="PitchMax" units="degrees" type="uint8" elements="1" defaultvalue="40" limits="%BE:0:180"/> <field name="PitchMax" units="degrees" type="uint8" elements="1" defaultvalue="40" limits="%BE:0:180"/>
<field name="YawMax" units="degrees" type="uint8" elements="1" defaultvalue="40" limits="%BE:0:180"/> <field name="YawMax" units="degrees" type="uint8" elements="1" defaultvalue="40" limits="%BE:0:180"/>
<field name="ManualRate" units="degrees/sec" type="float" elementnames="Roll,Pitch,Yaw" defaultvalue="150,150,175" limits="%BE:0:500; %BE:0:500; %BE:0:500"/> <field name="ManualRate" units="degrees/sec" type="float" elementnames="Roll,Pitch,Yaw" defaultvalue="150,150,175" limits="%BE:0:500; %BE:0:500; %BE:0:500"/>
<field name="MaximumRate" units="degrees/sec" type="float" elementnames="Roll,Pitch,Yaw" defaultvalue="300,300,300" limits="%BE:0:500; %BE:0:500; %BE:0:500"/> <field name="MaximumRate" units="degrees/sec" type="float" elementnames="Roll,Pitch,Yaw" defaultvalue="300,300,50" limits="%BE:0:500; %BE:0:500; %BE:0:500"/>
<field name="RollRatePID" units="" type="float" elementnames="Kp,Ki,Kd,ILimit" defaultvalue="0.003,0.003,0.00002,0.3" limits="%BE:0:0.01; %BE:0:0.01; ; "/> <field name="RollRatePID" units="" type="float" elementnames="Kp,Ki,Kd,ILimit" defaultvalue="0.003,0.003,0.00002,0.3" limits="%BE:0:0.01; %BE:0:0.01; ; "/>
<field name="PitchRatePID" units="" type="float" elementnames="Kp,Ki,Kd,ILimit" defaultvalue="0.003,0.003,0.00002,0.3" limits="%BE:0:0.01; %BE:0:0.01; ; "/> <field name="PitchRatePID" units="" type="float" elementnames="Kp,Ki,Kd,ILimit" defaultvalue="0.003,0.003,0.00002,0.3" limits="%BE:0:0.01; %BE:0:0.01; ; "/>