kr old xml output support

qualityorbit/QualityOrbit.h

@@ -14,7 +14,7 @@ public:
 	void SetDate(double interval, TimeJD date);
 	void AddValues(double dispR, double dispN, double dispB);
 	void CalculateStatistics();
-void Calculate(const SInitOrbit& orbit);
+    void Calculate(const SInitOrbit& orbit);
 	void ToXml(std::ostream& outs) const;
 	const QualityRnbUnit& GetR() const {return m_r;}
 	const QualityRnbUnit& GetN() const {return m_n;}

utils/AscNodeOrbit.cpp

@@ -286,3 +286,31 @@ void AscNodeOrbit::set_age(double age_days)
 {
     m_age = age_days;
 }
+
+static void PutValue(std::ostream& ss, std::string conName, const Vect6& value)
+{
+    ss << "<" << conName << ">";
+
+    PutValue(ss, "x", value.x);
+    PutValue(ss, "y", value.y);
+    PutValue(ss, "z", value.z);
+    PutValue(ss, "vx", value.vx);
+    PutValue(ss, "vy", value.vy);
+    PutValue(ss, "vz", value.vz);
+
+    ss << "</" << conName << ">";
+}
+
+void AscNodeOrbit::ToXml(std::ostream& outs) const
+{
+    PutValue(outs, "date", m_date);
+    PutValue(outs, "latitude", m_latitude);
+    PutValue(outs, "longitude", m_longitude);
+    PutValue(outs, "altitude", m_altitude);
+    PutValue(outs, "drperiod", m_drperiod);
+    PutValue(outs, "drperiodDt", m_drperiodDt);
+    PutValue(outs, "kepJ2000", m_kdj2000);
+    PutValue(outs, "kepEci", m_kdeci);
+    PutValue(outs, "vecJ2000", m_j2000);
+}
+

utils/AscNodeOrbit.h

@@ -4,6 +4,7 @@
 #include "TM.h"
 #include "StateVector.h"
 #include "Propagator.h"
+#include "XMLFunctions.h"
 
 class AscNodeOrbit
 {
@@ -28,6 +29,7 @@ public:
     int get_rev() const { return m_rev; }
     double get_age() const { return m_age; }
     bool is_desc() const { return m_is_desc; }
+    void ToXml(std::ostream& outs) const;
 private:
     void calc_asc_node(Propagator& prop, const TimeJD& date, bool vzmode, bool gcs_node, PhasePoint6D& result) const;
     void calc_desc_node(Propagator& prop, const TimeJD& date, bool vzmode, bool gcs_node, PhasePoint6D& result) const;