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Merge branch 'Orbiter2016' of https://github.com/orbiternassp/NASSP i…
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…nto OpenOrbiter3
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@CaptainSwag101
CaptainSwag101 committed Jan 24, 2024
2 parents 2222d50 + 70bddaf commit 7f48633
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Showing 15 changed files with 275 additions and 268 deletions.
4 changes: 2 additions & 2 deletions Orbitersdk/samples/ProjectApollo/src_launch/RTCC_Mission_C.cpp
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Original file line number Diff line number Diff line change
Expand Up @@ -62,7 +62,7 @@ bool RTCC::CalculationMTP_C(int fcn, LPVOID &pad, char * upString, char * upDesc
int hh, mm;
double ss;

OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss);
OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss, 0.01);

sprintf_s(Buff, "P10,CSM,%d:%d:%.2lf;", hh, mm, ss);
GMGMED(Buff);
Expand All @@ -81,7 +81,7 @@ bool RTCC::CalculationMTP_C(int fcn, LPVOID &pad, char * upString, char * upDesc
GMGMED(Buff);

//P12: IU GRR and Azimuth
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss);
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss, 0.01);
sprintf_s(Buff, "P12,IU1,%d:%d:%.2lf,%.2lf;", hh, mm, ss, Azi);
GMGMED(Buff);

Expand Down
4 changes: 2 additions & 2 deletions Orbitersdk/samples/ProjectApollo/src_launch/RTCC_Mission_C_PRIME.cpp
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Original file line number Diff line number Diff line change
Expand Up @@ -65,7 +65,7 @@ bool RTCC::CalculationMTP_C_PRIME(int fcn, LPVOID &pad, char * upString, char *
int hh, mm;
double ss;

OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss);
OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss, 0.01);

sprintf_s(Buff, "P10,CSM,%d:%d:%.2lf;", hh, mm, ss);
GMGMED(Buff);
Expand All @@ -84,7 +84,7 @@ bool RTCC::CalculationMTP_C_PRIME(int fcn, LPVOID &pad, char * upString, char *
GMGMED(Buff);

//P12: IU GRR and Azimuth
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss);
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss, 0.01);
sprintf_s(Buff, "P12,IU1,%d:%d:%.2lf,%.2lf;", hh, mm, ss, Azi);
GMGMED(Buff);

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4 changes: 2 additions & 2 deletions Orbitersdk/samples/ProjectApollo/src_launch/RTCC_Mission_D.cpp
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Original file line number Diff line number Diff line change
Expand Up @@ -156,7 +156,7 @@ bool RTCC::CalculationMTP_D(int fcn, LPVOID &pad, char * upString, char * upDesc
int hh, mm;
double ss;

OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss);
OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss, 0.01);

sprintf_s(Buff, "P10,CSM,%d:%d:%.2lf;", hh, mm, ss);
GMGMED(Buff);
Expand All @@ -178,7 +178,7 @@ bool RTCC::CalculationMTP_D(int fcn, LPVOID &pad, char * upString, char * upDesc
GMGMED("P15,AGS,,40:00:00;");

//P12: IU GRR and Azimuth
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss);
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss, 0.01);
sprintf_s(Buff, "P12,IU1,%d:%d:%.2lf,%.2lf;", hh, mm, ss, Azi);
GMGMED(Buff);

Expand Down
4 changes: 2 additions & 2 deletions Orbitersdk/samples/ProjectApollo/src_launch/RTCC_Mission_F.cpp
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Original file line number Diff line number Diff line change
Expand Up @@ -65,7 +65,7 @@ bool RTCC::CalculationMTP_F(int fcn, LPVOID &pad, char * upString, char * upDesc
int hh, mm;
double ss;

OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss);
OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss, 0.01);

sprintf_s(Buff, "P10,CSM,%d:%d:%.2lf;", hh, mm, ss);
GMGMED(Buff);
Expand All @@ -87,7 +87,7 @@ bool RTCC::CalculationMTP_F(int fcn, LPVOID &pad, char * upString, char * upDesc
GMGMED("P15,AGS,,90:00:00;");

//P12: IU GRR and Azimuth
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss);
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss, 0.01);
sprintf_s(Buff, "P12,IU1,%d:%d:%.2lf,%.2lf;", hh, mm, ss, Azi);
GMGMED(Buff);

Expand Down
4 changes: 2 additions & 2 deletions Orbitersdk/samples/ProjectApollo/src_launch/RTCC_Mission_G.cpp
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Original file line number Diff line number Diff line change
Expand Up @@ -116,7 +116,7 @@ bool RTCC::CalculationMTP_G(int fcn, LPVOID &pad, char * upString, char * upDesc
int hh, mm;
double ss;

OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss);
OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss, 0.01);

sprintf_s(Buff, "P10,CSM,%d:%d:%.2lf;", hh, mm, ss);
GMGMED(Buff);
Expand All @@ -138,7 +138,7 @@ bool RTCC::CalculationMTP_G(int fcn, LPVOID &pad, char * upString, char * upDesc
GMGMED("P15,AGS,,90:00:00;");

//P12: IU GRR and Azimuth
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss);
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss, 0.01);
sprintf_s(Buff, "P12,IU1,%d:%d:%.2lf,%.2lf;", hh, mm, ss, Azi);
GMGMED(Buff);

Expand Down
12 changes: 6 additions & 6 deletions Orbitersdk/samples/ProjectApollo/src_launch/RTCC_Mission_H1.cpp
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Original file line number Diff line number Diff line change
Expand Up @@ -202,7 +202,7 @@ bool RTCC::CalculationMTP_H1(int fcn, LPVOID &pad, char * upString, char * upDes
int hh, mm;
double ss;

OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss);
OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss, 0.01);

sprintf_s(Buff, "P10,CSM,%d:%d:%.2lf;", hh, mm, ss);
GMGMED(Buff);
Expand All @@ -224,7 +224,7 @@ bool RTCC::CalculationMTP_H1(int fcn, LPVOID &pad, char * upString, char * upDes
GMGMED("P15,AGS,,100:00:00;");

//P12: IU GRR and Azimuth
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss);
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss, 0.01);
sprintf_s(Buff, "P12,IU1,%d:%d:%.2lf,%.2lf;", hh, mm, ss, Azi);
GMGMED(Buff);

Expand Down Expand Up @@ -577,7 +577,7 @@ bool RTCC::CalculationMTP_H1(int fcn, LPVOID &pad, char * upString, char * upDes
F23time = LOIFP - 11.0*60.0;
while (PZMCCDIS.data[0].GET_LOI < LOIFP - 5.0 || init)
{
OrbMech::SStoHHMMSS(F23time, hh, mm, ss);
OrbMech::SStoHHMMSS(F23time, hh, mm, ss, 0.01);
sprintf_s(Buff, "F23,%d:%d:%.2lf,%d:%d:%.2lf;", hh, mm, ss, hh, mm + 10, ss);
GMGMED(Buff);
TranslunarMidcourseCorrectionProcessor(sv, CSMmass, LMmass);
Expand Down Expand Up @@ -607,7 +607,7 @@ bool RTCC::CalculationMTP_H1(int fcn, LPVOID &pad, char * upString, char * upDes
F23time = LOIFP - 11.0*60.0;
while (PZMCCDIS.data[0].GET_LOI < LOIFP - 5.0 || init)
{
OrbMech::SStoHHMMSS(F23time, hh, mm, ss);
OrbMech::SStoHHMMSS(F23time, hh, mm, ss, 0.01);
sprintf_s(Buff, "F23,%d:%d:%.2lf,%d:%d:%.2lf;", hh, mm, ss, hh, mm + 10, ss);
GMGMED(Buff);
TranslunarMidcourseCorrectionProcessor(sv, CSMmass, LMmass);
Expand Down Expand Up @@ -2769,7 +2769,7 @@ bool RTCC::CalculationMTP_H1(int fcn, LPVOID &pad, char * upString, char * upDes
SystemParameters.MCGZSS = SystemParameters.MCGZSL + KFactor / 3600.0;
}

OrbMech::SStoHHMMSS(GETfromGMT(GetAGSClockZero()), hh, mm, ss);
OrbMech::SStoHHMMSS(GETfromGMT(GetAGSClockZero()), hh, mm, ss, 0.01);

AP11LMASCPAD pad2;

Expand Down Expand Up @@ -2844,7 +2844,7 @@ bool RTCC::CalculationMTP_H1(int fcn, LPVOID &pad, char * upString, char * upDes

AP11ManeuverPAD(&opt, *form);
sprintf(form->purpose, "SEP BURN");
OrbMech::SStoHHMMSS(form->GETI - 5.0*60.0, hh, mm, ss);
OrbMech::SStoHHMMSS(form->GETI - 5.0*60.0, hh, mm, ss, 0.01);
sprintf(form->remarks, "Jettison PAD: GET %d:%d:%.2lf R 219 P 358 Y 342\nSep burn is Z-axis, retrograde", hh, mm, ss);
form->type = 2;

Expand Down
6 changes: 3 additions & 3 deletions Orbitersdk/samples/ProjectApollo/src_launch/RTCC_Mission_SL.cpp
View file
Original file line number Diff line number Diff line change
Expand Up @@ -53,7 +53,7 @@ bool RTCC::CalculationMTP_SL(int fcn, LPVOID &pad, char * upString, char * upDes
int hh, mm;
gmt = modf(oapiGetSimMJD(), &iptr)*24.0*3600.0 + 4.0*3600.0; //TBD: Not sure this is good

OrbMech::SStoHHMMSS(gmt, hh, mm, ss);
OrbMech::SStoHHMMSS(gmt, hh, mm, ss, 0.01);

sprintf_s(Buff, "P10,CSM,%d:%d:%.2lf;", hh, mm, ss);
GMGMED(Buff);
Expand Down Expand Up @@ -94,7 +94,7 @@ bool RTCC::CalculationMTP_SL(int fcn, LPVOID &pad, char * upString, char * upDes
int hh, mm;
double ss;

OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss);
OrbMech::SStoHHMMSS(LaunchMJD*3600.0, hh, mm, ss, 0.01);

sprintf_s(Buff, "P10,CSM,%d:%d:%.2lf;", hh, mm, ss);
GMGMED(Buff);
Expand All @@ -113,7 +113,7 @@ bool RTCC::CalculationMTP_SL(int fcn, LPVOID &pad, char * upString, char * upDes
GMGMED(Buff);

//P12: IU GRR and Azimuth
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss);
OrbMech::SStoHHMMSS(T_GRR, hh, mm, ss, 0.01);
sprintf_s(Buff, "P12,IU1,%d:%d:%.2lf,%.2lf;", hh, mm, ss, Azi);
GMGMED(Buff);

Expand Down
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