Merge branch 'next' of http://git.gitorious.org/fg/flightgear into next
This commit is contained in:
commit
031ed14fb2
70 changed files with 97 additions and 104 deletions
0
package/Win32-Inno/FlightGear-1.9.iss
Executable file → Normal file
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package/Win32-Inno/FlightGear-1.9.iss
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projects/VC8/FGJS.vcproj
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projects/VC8/FGJS.vcproj
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projects/VC8/FlightGear.sln
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projects/VC8/FlightGear.sln
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projects/VC8/FlightGear.vcproj
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projects/VC8/FlightGear.vcproj
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projects/VC8/FlightGearLib.vcproj
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projects/VC8/FlightGearLib.vcproj
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projects/VC90/flightgear.ico
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projects/VC90/flightgear.ico
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Before Width: | Height: | Size: 13 KiB After Width: | Height: | Size: 13 KiB |
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projects/VC90/flightgear.rc
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projects/VC90/flightgear.rc
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|
@ -335,35 +335,13 @@ void FGAIMultiplayer::update(double dt)
|
|||
if (prevIt != mMotionInfo.begin())
|
||||
{
|
||||
--prevIt;
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||||
|
||||
MotionInfo::iterator delIt;
|
||||
delIt = mMotionInfo.begin();
|
||||
|
||||
while (delIt != prevIt)
|
||||
{
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||||
std::vector<FGPropertyData*>::const_iterator propIt;
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||||
std::vector<FGPropertyData*>::const_iterator propItEnd;
|
||||
propIt = delIt->second.properties.begin();
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||||
propItEnd = delIt->second.properties.end();
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||||
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||||
//cout << "Deleting data\n";
|
||||
|
||||
while (propIt != propItEnd)
|
||||
{
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||||
delete *propIt;
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||||
propIt++;
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||||
}
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||||
|
||||
delIt++;
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||||
}
|
||||
|
||||
mMotionInfo.erase(mMotionInfo.begin(), prevIt);
|
||||
}
|
||||
}
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||||
} else {
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||||
// Ok, we need to predict the future, so, take the best data we can have
|
||||
// and do some eom computation to guess that for now.
|
||||
FGExternalMotionData motionInfo = it->second;
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||||
FGExternalMotionData& motionInfo = it->second;
|
||||
|
||||
// The time to predict, limit to 5 seconds
|
||||
double t = tInterp - motionInfo.time;
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||||
|
@ -488,7 +466,7 @@ void FGAIMultiplayer::update(double dt)
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|||
}
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||||
|
||||
void
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||||
FGAIMultiplayer::addMotionInfo(const FGExternalMotionData& motionInfo,
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||||
FGAIMultiplayer::addMotionInfo(FGExternalMotionData& motionInfo,
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||||
long stamp)
|
||||
{
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||||
mLastTimestamp = stamp;
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||||
|
@ -505,6 +483,9 @@ FGAIMultiplayer::addMotionInfo(const FGExternalMotionData& motionInfo,
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|||
return;
|
||||
}
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||||
mMotionInfo[motionInfo.time] = motionInfo;
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||||
// We just copied the property (pointer) list - they are ours now. Clear the
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||||
// properties list in given/returned object, so former owner won't deallocate them.
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||||
motionInfo.properties.clear();
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||||
}
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||||
void
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|
|
|
@ -37,7 +37,7 @@ public:
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|||
virtual void unbind();
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virtual void update(double dt);
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||||
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||||
void addMotionInfo(const FGExternalMotionData& motionInfo, long stamp);
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||||
void addMotionInfo(FGExternalMotionData& motionInfo, long stamp);
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||||
void setDoubleProperty(const std::string& prop, double val);
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||||
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||||
long getLastTimestamp(void) const
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||||
|
|
0
src/Airports/pavement.cxx
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src/Airports/pavement.cxx
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src/Airports/pavement.hxx
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src/Airports/pavement.hxx
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src/Environment/presets.cxx
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src/Environment/presets.cxx
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src/Environment/presets.hxx
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src/Environment/presets.hxx
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|
@ -36,25 +36,12 @@
|
|||
#include <Scenery/scenery.hxx>
|
||||
#include <string>
|
||||
#include <math.h>
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||||
|
||||
#include <simgear/sg_inlines.h>
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||||
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||||
using std::string;
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||||
|
||||
#include "ridge_lift.hxx"
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||||
|
||||
static string CreateIndexedPropertyName(string Property, int index)
|
||||
{
|
||||
std::stringstream str;
|
||||
str << index;
|
||||
string tmp;
|
||||
str >> tmp;
|
||||
return Property + "[" + tmp + "]";
|
||||
}
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||||
|
||||
static inline double sign(double x) {
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||||
return x == 0 ? 0 : x > 0 ? 1.0 : -1.0;
|
||||
}
|
||||
|
||||
static const double BOUNDARY1_m = 40.0;
|
||||
|
||||
const double FGRidgeLift::dist_probe_m[] = { // in meters
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||||
|
@ -172,7 +159,7 @@ void FGRidgeLift::update(double dt) {
|
|||
slope[3] = (probe_elev_m[4] - probe_elev_m[0]) / -dist_probe_m[4];
|
||||
|
||||
for (unsigned i = 0; i < sizeof(slope)/sizeof(slope[0]); i++)
|
||||
adj_slope[i] = sin(atan(5.0 * pow ( (fabs(slope[i])),1.7) ) ) *sign(slope[i]);
|
||||
adj_slope[i] = sin(atan(5.0 * pow ( (fabs(slope[i])),1.7) ) ) *SG_SIGN<double>(slope[i]);
|
||||
|
||||
//adjustment
|
||||
adj_slope[0] *= 0.2;
|
||||
|
|
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src/FDM/JSBSim/input_output/FGPropertyManager.cpp
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src/FDM/JSBSim/input_output/FGPropertyManager.cpp
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src/FDM/JSBSim/input_output/FGScript.cpp
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src/FDM/JSBSim/input_output/FGScript.cpp
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src/FDM/JSBSim/input_output/FGXMLElement.cpp
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src/FDM/JSBSim/input_output/FGXMLElement.cpp
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src/FDM/JSBSim/input_output/FGXMLElement.h
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src/FDM/JSBSim/input_output/FGXMLElement.h
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src/FDM/JSBSim/input_output/FGXMLFileRead.h
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src/FDM/JSBSim/input_output/FGXMLFileRead.h
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src/FDM/JSBSim/input_output/FGXMLParse.cpp
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src/FDM/JSBSim/input_output/FGXMLParse.cpp
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src/FDM/JSBSim/input_output/FGXMLParse.h
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src/FDM/JSBSim/input_output/FGXMLParse.h
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src/FDM/JSBSim/math/FGFunction.cpp
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src/FDM/JSBSim/math/FGFunction.cpp
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src/FDM/JSBSim/math/FGFunction.h
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src/FDM/JSBSim/math/FGFunction.h
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src/FDM/JSBSim/math/FGModelFunctions.cpp
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src/FDM/JSBSim/math/FGModelFunctions.cpp
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src/FDM/JSBSim/math/FGModelFunctions.h
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src/FDM/JSBSim/math/FGModelFunctions.h
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src/FDM/JSBSim/math/FGParameter.h
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src/FDM/JSBSim/math/FGParameter.h
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src/FDM/JSBSim/math/FGPropertyValue.cpp
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src/FDM/JSBSim/math/FGPropertyValue.cpp
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src/FDM/JSBSim/math/FGPropertyValue.h
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src/FDM/JSBSim/math/FGPropertyValue.h
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src/FDM/JSBSim/math/FGRealValue.cpp
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src/FDM/JSBSim/math/FGRealValue.cpp
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src/FDM/JSBSim/math/FGRealValue.h
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src/FDM/JSBSim/math/FGRealValue.h
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src/FDM/JSBSim/models/FGAuxiliary.cpp
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src/FDM/JSBSim/models/FGAuxiliary.cpp
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src/FDM/JSBSim/models/FGExternalForce.cpp
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src/FDM/JSBSim/models/FGExternalForce.cpp
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src/FDM/JSBSim/models/FGExternalForce.h
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src/FDM/JSBSim/models/FGExternalForce.h
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src/FDM/JSBSim/models/FGExternalReactions.cpp
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src/FDM/JSBSim/models/FGExternalReactions.cpp
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src/FDM/JSBSim/models/FGExternalReactions.h
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src/FDM/JSBSim/models/FGExternalReactions.h
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src/FDM/JSBSim/models/FGInput.cpp
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src/FDM/JSBSim/models/FGInput.cpp
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src/FDM/JSBSim/models/FGInput.h
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src/FDM/JSBSim/models/FGInput.h
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src/FDM/JSBSim/models/atmosphere/FGMSIS.cpp
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src/FDM/JSBSim/models/atmosphere/FGMSIS.cpp
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src/FDM/JSBSim/models/atmosphere/FGMSIS.h
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src/FDM/JSBSim/models/atmosphere/FGMSIS.h
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src/FDM/JSBSim/models/atmosphere/FGMSISData.cpp
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src/FDM/JSBSim/models/atmosphere/FGMSISData.cpp
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src/FDM/JSBSim/models/atmosphere/FGMars.cpp
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src/FDM/JSBSim/models/atmosphere/FGMars.cpp
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src/FDM/JSBSim/models/atmosphere/FGMars.h
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src/FDM/JSBSim/models/atmosphere/FGMars.h
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src/FDM/JSBSim/models/flight_control/FGAccelerometer.cpp
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src/FDM/JSBSim/models/flight_control/FGAccelerometer.cpp
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src/FDM/JSBSim/models/flight_control/FGAccelerometer.h
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src/FDM/JSBSim/models/flight_control/FGAccelerometer.h
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src/FDM/JSBSim/models/flight_control/FGFCSFunction.cpp
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src/FDM/JSBSim/models/flight_control/FGFCSFunction.cpp
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src/FDM/JSBSim/models/flight_control/FGFCSFunction.h
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src/FDM/JSBSim/models/flight_control/FGFCSFunction.h
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src/FDM/JSBSim/models/flight_control/FGGyro.cpp
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src/FDM/JSBSim/models/flight_control/FGGyro.cpp
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src/FDM/JSBSim/models/flight_control/FGGyro.h
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src/FDM/JSBSim/models/flight_control/FGGyro.h
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src/FDM/JSBSim/models/flight_control/FGMagnetometer.cpp
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src/FDM/JSBSim/models/flight_control/FGMagnetometer.cpp
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src/FDM/JSBSim/models/flight_control/FGMagnetometer.h
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src/FDM/JSBSim/models/flight_control/FGMagnetometer.h
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src/FDM/JSBSim/models/flight_control/FGPID.cpp
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src/FDM/JSBSim/models/flight_control/FGPID.cpp
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src/FDM/JSBSim/models/flight_control/FGPID.h
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src/FDM/JSBSim/models/flight_control/FGPID.h
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src/FDM/JSBSim/models/flight_control/FGSensor.cpp
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src/FDM/JSBSim/models/flight_control/FGSensor.cpp
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src/FDM/JSBSim/models/flight_control/FGSensor.h
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src/FDM/JSBSim/models/flight_control/FGSensor.h
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src/FDM/JSBSim/models/flight_control/FGSensorOrientation.h
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src/FDM/JSBSim/models/flight_control/FGSensorOrientation.h
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src/FDM/JSBSim/models/propulsion/FGTurboProp.cpp
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src/FDM/JSBSim/models/propulsion/FGTurboProp.cpp
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src/FDM/JSBSim/models/propulsion/FGTurboProp.h
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src/FDM/JSBSim/models/propulsion/FGTurboProp.h
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src/FDM/YASim/Hitch.cpp
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src/FDM/YASim/Hitch.cpp
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src/FDM/YASim/Hitch.hpp
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src/FDM/YASim/Hitch.hpp
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src/Instrumentation/mk_viii.cxx
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src/Instrumentation/mk_viii.cxx
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src/Instrumentation/mk_viii.hxx
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src/Instrumentation/mk_viii.hxx
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|
@ -61,28 +61,37 @@ static double sawtooth(double xx)
|
|||
return 4.0 * fabs(xx/4.0 + 0.25 - floor(xx/4.0 + 0.75)) - 1.0;
|
||||
}
|
||||
|
||||
// Calculate a unit vector in the horizontal tangent plane
|
||||
// starting at the given "tail" of the vector and going off
|
||||
// with the given heading.
|
||||
static SGVec3d tangentVector(const SGGeod& tail, const SGVec3d& tail_xyz,
|
||||
const double heading)
|
||||
// Calculate a Cartesian unit vector in the
|
||||
// local horizontal plane, i.e. tangent to the
|
||||
// surface of the earth at the local ground zero.
|
||||
// The tangent vector passes through the given <midpoint>
|
||||
// and points forward along the given <heading>.
|
||||
// The <heading> is given in degrees.
|
||||
static SGVec3d tangentVector(const SGGeod& midpoint, const double heading)
|
||||
{
|
||||
// The fudge factor here is presumably intended to improve
|
||||
// numerical stability. I don't know if it is necessary.
|
||||
// It gets divided out later.
|
||||
double fudge(100.0);
|
||||
SGGeod head;
|
||||
// The size of the delta is presumably chosen to give
|
||||
// numerical stability. I don't know how the value was chosen.
|
||||
// It probably doesn't matter much. It gets divided out.
|
||||
double delta(100.0); // in meters
|
||||
SGGeod head, tail;
|
||||
double az2; // ignored
|
||||
SGGeodesy::direct(tail, heading, fudge, head, az2);
|
||||
head.setElevationM(tail.getElevationM());
|
||||
SGGeodesy::direct(midpoint, heading, delta, head, az2);
|
||||
SGGeodesy::direct(midpoint, 180+heading, delta, tail, az2);
|
||||
head.setElevationM(midpoint.getElevationM());
|
||||
tail.setElevationM(midpoint.getElevationM());
|
||||
SGVec3d head_xyz = SGVec3d::fromGeod(head);
|
||||
return (head_xyz - tail_xyz) * (1.0/fudge);
|
||||
SGVec3d tail_xyz = SGVec3d::fromGeod(tail);
|
||||
// Awkward formula here, needed because vector-by-scalar
|
||||
// multiplication is defined, but not vector-by-scalar division.
|
||||
return (head_xyz - tail_xyz) * (0.5/delta);
|
||||
}
|
||||
|
||||
// Create a "serviceable" node with a default value of "true"
|
||||
SGPropertyNode_ptr createServiceableProp(SGPropertyNode* aParent, const char* aName)
|
||||
SGPropertyNode_ptr createServiceableProp(SGPropertyNode* aParent,
|
||||
const char* aName)
|
||||
{
|
||||
SGPropertyNode_ptr n = (aParent->getChild(aName, 0, true)->getChild("serviceable", 0, true));
|
||||
SGPropertyNode_ptr n =
|
||||
aParent->getChild(aName, 0, true)->getChild("serviceable", 0, true);
|
||||
simgear::props::Type typ = n->getType();
|
||||
if ((typ == simgear::props::NONE) || (typ == simgear::props::UNSPECIFIED)) {
|
||||
n->setBoolValue(true);
|
||||
|
@ -231,6 +240,7 @@ FGNavRadio::init ()
|
|||
gs_deflection_node = node->getChild("gs-needle-deflection", 0, true);
|
||||
gs_deflection_deg_node = node->getChild("gs-needle-deflection-deg", 0, true);
|
||||
gs_deflection_norm_node = node->getChild("gs-needle-deflection-norm", 0, true);
|
||||
gs_direct_node = node->getChild("gs-direct-deg", 0, true);
|
||||
gs_rate_of_climb_node = node->getChild("gs-rate-of-climb", 0, true);
|
||||
gs_rate_of_climb_fpm_node = node->getChild("gs-rate-of-climb-fpm", 0, true);
|
||||
gs_dist_node = node->getChild("gs-distance", 0, true);
|
||||
|
@ -393,6 +403,7 @@ void FGNavRadio::clearOutputs()
|
|||
gs_deflection_node->setDoubleValue( 0.0 );
|
||||
gs_deflection_deg_node->setDoubleValue(0.0);
|
||||
gs_deflection_norm_node->setDoubleValue(0.0);
|
||||
gs_direct_node->setDoubleValue(0.0);
|
||||
gs_inrange_node->setBoolValue( false );
|
||||
loc_node->setBoolValue( false );
|
||||
has_gs_node->setBoolValue(false);
|
||||
|
@ -592,19 +603,27 @@ void FGNavRadio::updateGlideSlope(double dt, const SGVec3d& aircraft, double sig
|
|||
bool gsInRange = (gsDist < (_gs->get_range() * SG_NM_TO_METER));
|
||||
gs_inrange_node->setBoolValue(gsInRange);
|
||||
|
||||
if (!gsInRange) {
|
||||
_gsNeedleDeflection = 0.0;
|
||||
_gsNeedleDeflectionNorm = 0.0;
|
||||
return;
|
||||
}
|
||||
if (!gsInRange) return;
|
||||
|
||||
SGVec3d pos = aircraft - _gsCart; // relative vector from gs antenna to aircraft
|
||||
// The positive GS axis points along the runway in the landing direction,
|
||||
// toward the far end, not toward the approach area, so we need a - sign here:
|
||||
double dot_h = -dot(pos, _gsAxis);
|
||||
double dot_v = dot(pos, _gsVertical);
|
||||
double angle = atan2(dot_v, dot_h) * SGD_RADIANS_TO_DEGREES;
|
||||
double deflectionAngle = target_gs - angle;
|
||||
double comp_h = -dot(pos, _gsAxis); // component in horiz direction
|
||||
double comp_v = dot(pos, _gsVertical); // component in vertical direction
|
||||
//double comp_b = dot(pos, _gsBaseline); // component in baseline direction
|
||||
//if (comp_b) {} // ... (useful for debugging)
|
||||
|
||||
// _gsDirect represents the angle of elevation of the aircraft
|
||||
// as seen by the GS transmitter.
|
||||
_gsDirect = atan2(comp_v, comp_h) * SGD_RADIANS_TO_DEGREES;
|
||||
// At this point, if the aircraft is centered on the glide slope,
|
||||
// _gsDirect will be a small positive number, e.g. 3.0 degrees
|
||||
|
||||
// Aim the branch cut straight down
|
||||
// into the ground below the GS transmitter:
|
||||
if (_gsDirect < -90.0) _gsDirect += 360.0;
|
||||
|
||||
double deflectionAngle = target_gs - _gsDirect;
|
||||
|
||||
if (falseCoursesEnabledNode->getBoolValue()) {
|
||||
// Construct false glideslopes. The scale factor of 1.5
|
||||
|
@ -624,20 +643,27 @@ void FGNavRadio::updateGlideSlope(double dt, const SGVec3d& aircraft, double sig
|
|||
}
|
||||
}
|
||||
|
||||
// GS is documented to be 1.4 degrees thick,
|
||||
// i.e. plus or minus 0.7 degrees from the midline:
|
||||
SG_CLAMP_RANGE(deflectionAngle, -0.7, 0.7);
|
||||
|
||||
// Many older instrument xml frontends depend on
|
||||
// the un-normalized gs-needle-deflection.
|
||||
// Apparently the interface standard is plus or minus 3.5 "volts"
|
||||
// for a full-scale deflection:
|
||||
_gsNeedleDeflection = deflectionAngle * 5.0;
|
||||
_gsNeedleDeflection *= signal_quality_norm;
|
||||
|
||||
SG_CLAMP_RANGE(deflectionAngle, -0.7, 0.7);
|
||||
_gsNeedleDeflectionNorm = (deflectionAngle / 0.7) * signal_quality_norm;
|
||||
|
||||
//////////////////////////////////////////////////////////
|
||||
// Calculate desired rate of climb for intercepting the GS
|
||||
//////////////////////////////////////////////////////////
|
||||
double gs_diff = target_gs - angle;
|
||||
double gs_diff = target_gs - _gsDirect;
|
||||
// convert desired vertical path angle into a climb rate
|
||||
double des_angle = angle - 10 * gs_diff;
|
||||
double des_angle = _gsDirect - 10 * gs_diff;
|
||||
/* printf("target_gs=%.1f angle=%.1f gs_diff=%.1f des_angle=%.1f\n",
|
||||
target_gs, angle, gs_diff, des_angle); */
|
||||
target_gs, _gsDirect, gs_diff, des_angle); */
|
||||
|
||||
// estimate horizontal speed towards ILS in meters per minute
|
||||
double elapsedDistance = last_x - gsDist;
|
||||
|
@ -798,7 +824,7 @@ void FGNavRadio::updateCDI(double dt)
|
|||
|
||||
//////////////////////////////////////////////////////////
|
||||
// compute the time to intercept selected radial (based on
|
||||
// current and last cross track errors and dt
|
||||
// current and last cross track errors and dt)
|
||||
//////////////////////////////////////////////////////////
|
||||
double t = 0.0;
|
||||
if ( inrange && cdi_serviceable ) {
|
||||
|
@ -819,6 +845,7 @@ void FGNavRadio::updateCDI(double dt)
|
|||
gs_deflection_node->setDoubleValue(_gsNeedleDeflection);
|
||||
gs_deflection_deg_node->setDoubleValue(_gsNeedleDeflectionNorm * 0.7);
|
||||
gs_deflection_norm_node->setDoubleValue(_gsNeedleDeflectionNorm);
|
||||
gs_direct_node->setDoubleValue(_gsDirect);
|
||||
|
||||
last_xtrack_error = _cdiCrossTrackErrorM;
|
||||
}
|
||||
|
@ -940,23 +967,18 @@ void FGNavRadio::search()
|
|||
int tmp = (int)(_gs->get_multiuse() / 1000.0);
|
||||
target_gs = (double)tmp / 100.0;
|
||||
|
||||
// until penaltyForNav goes away, we cannot assume we always pick
|
||||
// paired LOC/GS trasmsitters. As we pass over a runway threshold, we
|
||||
// often end up picking the 'wrong' LOC, but the correct GS. To avoid
|
||||
// breaking the basis computation, ensure we use the GS radial and not
|
||||
// the (potentially reversed) LOC radial.
|
||||
double gs_radial = fmod(_gs->get_multiuse(), 1000.0);
|
||||
SG_NORMALIZE_RANGE(gs_radial, 0.0, 360.0);
|
||||
_gsCart = _gs->cart();
|
||||
|
||||
// GS axis unit tangent vector
|
||||
// (along the runway)
|
||||
_gsCart = _gs->cart();
|
||||
_gsAxis = tangentVector(_gs->geod(), _gsCart, gs_radial);
|
||||
// (along the runway):
|
||||
_gsAxis = tangentVector(_gs->geod(), gs_radial);
|
||||
|
||||
// GS baseline unit tangent vector
|
||||
// (perpendicular to the runay along the ground)
|
||||
SGVec3d baseline = tangentVector(_gs->geod(), _gsCart, gs_radial + 90.0);
|
||||
_gsVertical = cross(baseline, _gsAxis);
|
||||
// (transverse to the runay along the ground)
|
||||
_gsBaseline = tangentVector(_gs->geod(), gs_radial + 90.0);
|
||||
_gsVertical = cross(_gsBaseline, _gsAxis);
|
||||
} // of have glideslope
|
||||
} // of found LOC or ILS
|
||||
|
||||
|
|
|
@ -102,6 +102,7 @@ class FGNavRadio : public SGSubsystem, public SGPropertyChangeListener
|
|||
SGPropertyNode_ptr gs_deflection_node;
|
||||
SGPropertyNode_ptr gs_deflection_deg_node;
|
||||
SGPropertyNode_ptr gs_deflection_norm_node;
|
||||
SGPropertyNode_ptr gs_direct_node;
|
||||
SGPropertyNode_ptr gs_rate_of_climb_node;
|
||||
SGPropertyNode_ptr gs_rate_of_climb_fpm_node;
|
||||
SGPropertyNode_ptr gs_dist_node;
|
||||
|
@ -152,7 +153,7 @@ class FGNavRadio : public SGSubsystem, public SGPropertyChangeListener
|
|||
// internal periodic station search timer
|
||||
double _time_before_search_sec;
|
||||
|
||||
SGVec3d _gsCart, _gsAxis, _gsVertical;
|
||||
SGVec3d _gsCart, _gsAxis, _gsVertical, _gsBaseline;
|
||||
|
||||
FGNavRecordPtr _dme;
|
||||
bool _dmeInRange;
|
||||
|
@ -163,6 +164,7 @@ class FGNavRadio : public SGSubsystem, public SGPropertyChangeListener
|
|||
double _cdiCrossTrackErrorM;
|
||||
double _gsNeedleDeflection;
|
||||
double _gsNeedleDeflectionNorm;
|
||||
double _gsDirect;
|
||||
|
||||
SGSharedPtr<SGSampleGroup> _sgr;
|
||||
std::vector<SGPropertyNode_ptr> _tiedNodes;
|
||||
|
|
0
src/Instrumentation/tacan.cxx
Executable file → Normal file
0
src/Instrumentation/tacan.cxx
Executable file → Normal file
0
src/Instrumentation/tacan.hxx
Executable file → Normal file
0
src/Instrumentation/tacan.hxx
Executable file → Normal file
|
@ -141,7 +141,7 @@ struct FGExternalMotionData {
|
|||
// simulation time when this packet was generated
|
||||
double time;
|
||||
// the artificial lag the client should stay behind the average
|
||||
// simulation time to arrival time diference
|
||||
// simulation time to arrival time difference
|
||||
// FIXME: should be some 'per model' instead of 'per packet' property
|
||||
double lag;
|
||||
|
||||
|
@ -166,6 +166,20 @@ struct FGExternalMotionData {
|
|||
|
||||
// The set of properties recieved for this timeslot
|
||||
std::vector<FGPropertyData*> properties;
|
||||
|
||||
~FGExternalMotionData()
|
||||
{
|
||||
std::vector<FGPropertyData*>::const_iterator propIt;
|
||||
std::vector<FGPropertyData*>::const_iterator propItEnd;
|
||||
propIt = properties.begin();
|
||||
propItEnd = properties.end();
|
||||
|
||||
while (propIt != propItEnd)
|
||||
{
|
||||
delete *propIt;
|
||||
propIt++;
|
||||
}
|
||||
}
|
||||
};
|
||||
|
||||
#endif
|
||||
|
|
|
@ -923,19 +923,20 @@ FGMultiplayMgr::ProcessPosMsg(const FGMultiplayMgr::MsgBuf& Msg,
|
|||
goto noprops;
|
||||
}
|
||||
while (xdr < Msg.propsRecvdEnd()) {
|
||||
FGPropertyData* pData = new FGPropertyData;
|
||||
// simgear::props::Type type = simgear::props::UNSPECIFIED;
|
||||
|
||||
// First element is always the ID
|
||||
pData->id = XDR_decode_uint32(*xdr);
|
||||
unsigned id = XDR_decode_uint32(*xdr);
|
||||
//cout << pData->id << " ";
|
||||
xdr++;
|
||||
|
||||
// Check the ID actually exists and get the type
|
||||
const IdPropertyList* plist = findProperty(pData->id);
|
||||
const IdPropertyList* plist = findProperty(id);
|
||||
|
||||
if (plist)
|
||||
{
|
||||
FGPropertyData* pData = new FGPropertyData;
|
||||
pData->id = id;
|
||||
pData->type = plist->type;
|
||||
// How we decode the remainder of the property depends on the type
|
||||
switch (pData->type) {
|
||||
|
@ -1001,7 +1002,7 @@ FGMultiplayMgr::ProcessPosMsg(const FGMultiplayMgr::MsgBuf& Msg,
|
|||
// We failed to find the property. We'll try the next packet immediately.
|
||||
SG_LOG(SG_NETWORK, SG_INFO, "FGMultiplayMgr::ProcessPosMsg - "
|
||||
"message from " << MsgHdr->Callsign << " has unknown property id "
|
||||
<< pData->id);
|
||||
<< id);
|
||||
}
|
||||
}
|
||||
noprops:
|
||||
|
@ -1015,7 +1016,7 @@ FGMultiplayMgr::ProcessPosMsg(const FGMultiplayMgr::MsgBuf& Msg,
|
|||
//////////////////////////////////////////////////////////////////////
|
||||
//
|
||||
// handle a chat message
|
||||
// FIXME: display chat message withi flightgear
|
||||
// FIXME: display chat message within flightgear
|
||||
//
|
||||
//////////////////////////////////////////////////////////////////////
|
||||
void
|
||||
|
|
0
src/Navaids/awynet.cxx
Executable file → Normal file
0
src/Navaids/awynet.cxx
Executable file → Normal file
0
src/Navaids/awynet.hxx
Executable file → Normal file
0
src/Navaids/awynet.hxx
Executable file → Normal file
|
@ -283,20 +283,6 @@ bool FGMultiplay::process() {
|
|||
|
||||
FGMultiplayMgr* mpmgr = (FGMultiplayMgr*) globals->get_subsystem("mp");
|
||||
mpmgr->SendMyPosition(motionInfo);
|
||||
|
||||
// Now remove the data
|
||||
std::vector<FGPropertyData*>::const_iterator propIt;
|
||||
std::vector<FGPropertyData*>::const_iterator propItEnd;
|
||||
propIt = motionInfo.properties.begin();
|
||||
propItEnd = motionInfo.properties.end();
|
||||
|
||||
//cout << "Deleting data\n";
|
||||
|
||||
while (propIt != propItEnd)
|
||||
{
|
||||
delete *propIt;
|
||||
propIt++;
|
||||
}
|
||||
}
|
||||
|
||||
return true;
|
||||
|
|
Loading…
Reference in a new issue