C++ Question please help me with payload coding

Mr Martian

Mr Martian

Orbinaut/Addon dev/Donator
Addon Developer
Donator
Joined
Jun 6, 2012
Messages
304
Reaction score
88
Points
28
Location
Sydney, Australia, Earth, Sol
Website
www.orbithangar.com
hey i am trying to create a ship wit vc++ that has a payload and i cant do it. ive read so many tutorials and tried so many different things. ive been trying to learn how to ad payloads for over a week now and its just getting frustrating. i am really new to coding and i was wondering if i post my code here, if someone would like to ad a really simple payload capability, it would really mean a lot to me :)

---------- Post added at 02:51 AM ---------- Previous post was at 02:44 AM ----------

this is the code here:

Code: 
//############################################################################//
#define ORBITER_MODULE
#define _CRT_SECURE_NO_WARNINGS
#define _CRT_NONSTDC_NO_DEPRECATE
#include <math.h>
#include <stdio.h>
#include "orbitersdk.h"
//############################################################################//
#include "IPA_Vehicle.h"
//############################################################################//
//Airfoil coefficient functions
//Return lift, moment and zero-lift drag coefficients as a
//function of angle of attack (alpha or beta)
//############################################################################//
//vertical lift component (wings and body)
void VLiftCoeff(VESSEL *v,double aoa,double M,double Re,void *context,double *cl,double *cm,double *cd)
{
 int i;
 const int nabsc=9;
 static const double AOA[nabsc]={-180*RAD,-60*RAD,-30*RAD, -2*RAD, 15*RAD,20*RAD,25*RAD,60*RAD,180*RAD};
 static const double CL[nabsc] ={       0,      0,   -0.4,      0,    0.7,     1,   0.8,     0,      0};
 static const double CM[nabsc] ={       0,      0,  0.014, 0.0039, -0.006,-0.008,-0.010,     0,      0};
 for(i=0;i<nabsc-1 && AOA[i+1]<aoa;i++);
 double f=(aoa-AOA[i])/(AOA[i+1]-AOA[i]);
 *cl=CL[i]+(CL[i+1]-CL[i])*f;  //aoa-dependent lift coefficient
 *cm=CM[i]+(CM[i+1]-CM[i])*f;  //aoa-dependent moment coefficient
 double saoa=sin(aoa);
 double pd=0.015+0.4*saoa*saoa;  //profile drag
 *cd=pd+oapiGetInducedDrag(*cl,1.5,0.7)+oapiGetWaveDrag(M,0.75,1.0,1.1,0.04);
 //profile drag+(lift-)induced drag+transonic/supersonic wave (compressibility) drag
}
//############################################################################//
//horizontal lift component (vertical stabilisers and body)
void HLiftCoeff(VESSEL *v,double betta,double M,double Re,void *context,double *cl,double *cm,double *cd)
{
 int i;
 const int nabsc=8;
 static const double BETA[nabsc]={-180*RAD,-135*RAD,-90*RAD,-45*RAD,45*RAD,90*RAD,135*RAD,180*RAD};
 static const double CL[nabsc]  ={       0,    +0.3,      0,   -0.3,  +0.3,     0,   -0.3,      0};
 for(i=0;i<nabsc-1 && BETA[i+1]<betta;i++);
 *cl=CL[i]+(CL[i+1]-CL[i])*(betta-BETA[i])/(BETA[i+1]-BETA[i]);
 *cm=0.0;
 *cd=0.015+oapiGetInducedDrag(*cl,1.5,0.6)+oapiGetWaveDrag(M,0.75,1.0,1.1,0.04);
}
//############################################################################//
//Class creation
IPA_Vehicle::IPA_Vehicle(OBJHANDLE hObj,int fmodel):VESSEL2(hObj,fmodel){}
IPA_Vehicle::~IPA_Vehicle(){}
//############################################################################//
//Fill animation definition
void IPA_Vehicle::make_anim(int n,int id,int tp,int repeat,int trigkey,int status,double spd,double proc,double init,int grpcnt,int compcnt)
{
 ani[n].id=id;
 ani[n].tp=tp;
 ani[n].repeat=repeat;
 ani[n].trigkey=trigkey;
 ani[n].status=status;
 ani[n].spd=spd;
 ani[n].proc=proc;
 ani[n].init=init;
 ani[n].grpcnt=grpcnt;
 ani[n].compcnt=compcnt;
}
//############################################################################//
//Fill animation component definition
void IPA_Vehicle::make_anim_comp(int n,int c,int msh,int id,int tp,int grp,int parent,VECTOR3 ref,VECTOR3 axshsc,double angle,double st0,double st1)
{
 ani[n].comp[c].msh=msh;
 ani[n].comp[c].id=id;
 ani[n].comp[c].tp=tp;
 ani[n].comp[c].grp=grp;
 ani[n].comp[c].parent=parent;
 ani[n].comp[c].ref=ref;
 ani[n].comp[c].axshsc=axshsc;
 ani[n].comp[c].angle=(float)angle;
 ani[n].comp[c].st0=st0;
 ani[n].comp[c].st1=st1;
}
//############################################################################//
//Define animations
void IPA_Vehicle::define_animations()
{
 int i,j,k,n,a,b;
 //Sequence 0
 make_anim(0,0,0,1,34,1,0.033,0,0,1,1);

 ani[0].grp=(UINT**)malloc(1*sizeof(UINT*));
 static UINT g0[1+1]={1,29}; ani[0].grp[0]=g0;

 ani[0].comp=(animcompinfo*)malloc(1*sizeof(animcompinfo));
 make_anim_comp(0,0,0,3,0,0,-1,_V(0,-0.232,0),_V(0,0,1),6.283,0,1);

 //Sequence 1
 make_anim(1,0,0,0,37,-2,0.079,0,0,1,1);

 ani[1].grp=(UINT**)malloc(1*sizeof(UINT*));
 static UINT g1[3+1]={3,66,6,7}; ani[1].grp[0]=g1;

 ani[1].comp=(animcompinfo*)malloc(1*sizeof(animcompinfo));
 make_anim_comp(1,0,0,0,1,0,-1,_V(0,0,0),_V(0,0,47),0,0,1);

 //Sequence 2
 make_anim(2,0,0,0,2,-2,0.079,0,0,3,3);

 ani[2].grp=(UINT**)malloc(3*sizeof(UINT*));
 static UINT g2[3+1]={3,0,1,2}; ani[2].grp[0]=g2;
 static UINT g3[1+1]={1,0}; ani[2].grp[1]=g3;
 static UINT g4[1+1]={1,2}; ani[2].grp[2]=g4;

 ani[2].comp=(animcompinfo*)malloc(3*sizeof(animcompinfo));
 make_anim_comp(2,0,0,2,1,0,-1,_V(0,0,0),_V(0,0,6),0,0,0.5);
 make_anim_comp(2,1,0,4,2,1,-1,_V(-6.782,0,386.895),_V(29,1,1),0,0.5,1);
 make_anim_comp(2,2,0,5,2,2,-1,_V(6.782,0,386.895),_V(29,1,1),0,0.5,1);

 //Sequence 3
 make_anim(3,0,0,0,3,-2,0.079,0,0,1,1);

 ani[3].grp=(UINT**)malloc(1*sizeof(UINT*));
 static UINT g5[3+1]={3,3,4,5}; ani[3].grp[0]=g5;

 ani[3].comp=(animcompinfo*)malloc(1*sizeof(animcompinfo));
 make_anim_comp(3,0,0,1,1,0,-1,_V(0,0,0),_V(0,-9,0),0,0,1);

 //Zero out components
 for(i=0;i<ANIM_COUNT;i++)for(j=0;j<ani[i].compcnt;j++)ani[i].comp[j].cmpt=NULL;
 
 //Animation core creation
 n=0;
 for(i=0;i<ANIM_COUNT;i++){
  for(j=0;j<ani[i].compcnt;j++){
    if(ani[i].comp[j].tp==0)ani[i].comp[j].cmpdef=new MGROUP_ROTATE   (ani[i].comp[j].msh,&(ani[i].grp[ani[i].comp[j].grp][1]),ani[i].grp[ani[i].comp[j].grp][0],ani[i].comp[j].ref,ani[i].comp[j].axshsc,ani[i].comp[j].angle);
    if(ani[i].comp[j].tp==1)ani[i].comp[j].cmpdef=new MGROUP_TRANSLATE(ani[i].comp[j].msh,&(ani[i].grp[ani[i].comp[j].grp][1]),ani[i].grp[ani[i].comp[j].grp][0],ani[i].comp[j].axshsc);
    if(ani[i].comp[j].tp==2)ani[i].comp[j].cmpdef=new MGROUP_SCALE    (ani[i].comp[j].msh,&(ani[i].grp[ani[i].comp[j].grp][1]),ani[i].grp[ani[i].comp[j].grp][0],ani[i].comp[j].ref,ani[i].comp[j].axshsc);
  }
  ani[i].id=CreateAnimation(ani[i].init);
  n+=ani[i].compcnt;
 }

 //Animation sequences
 //SC3 have a pequliar method of arranging sequences, so we have to sort them accordingly
 //FIXME: Lousy implementation, move to code generator?
 k=0;
 for(k=0;k<n;k++){
  for(i=0;i<ANIM_COUNT;i++){
   for(j=0;j<ani[i].compcnt;j++){
    if(ani[i].comp[j].id!=k)continue;
    int p=ani[i].comp[j].parent;
    if((p>=0)&(p<n)){
     ANIMATIONCOMPONENT_HANDLE prnt=NULL;
     for(a=0;a<ANIM_COUNT;a++)for(b=0;b<ani[a].compcnt;b++)if(ani[a].comp[b].id==p)prnt=ani[a].comp[b].cmpt;
     ani[i].comp[j].cmpt=AddAnimationComponent(ani[i].id,ani[i].comp[j].st0,ani[i].comp[j].st1,ani[i].comp[j].cmpdef,prnt);
    }else ani[i].comp[j].cmpt=AddAnimationComponent(ani[i].id,ani[i].comp[j].st0,ani[i].comp[j].st1,ani[i].comp[j].cmpdef);
    break;
   }
  }
 }
}
//############################################################################//
//All the parameters
void IPA_Vehicle::clbkSetClassCaps(FILEHANDLE cfg)
{
 int i;
 THRUSTER_HANDLE **grps;
 int *grpc;

 //Base stuff
 SetSize(222);
 SetEmptyMass(74000000);
 SetPMI(_V(80,80,80));
 SetCrossSections(_V(53,186.9,25.9));
 SetRotDrag(_V(0.36,0.18,0.15));
 SetTouchdownPoints(_V(0,-55.333,9),_V(-9.15,-55.333,-9),_V(9.15,-55.333,-9));
 SetSurfaceFrictionCoeff(0.07,0.3);
 SetCW(0.12,0.15,1.2,1.8);
 EnableTransponder(true);
 InitNavRadios(4);
 SetCameraOffset(_V(-1.231,-3.064,191.134));

 SetVisibilityLimit(0,0.002);
 SetAlbedoRGB(_V((float)255/255,(float)255/255,(float)255/255));
 SetGravityGradientDamping(0);
 SetWingAspect(0);
 SetWingEffectiveness(0);
 SetMaxWheelbrakeForce(200000);
 SetBankMomentScale(0.006);
 SetPitchMomentScale(0.005);

 //Fuel
 ph_h[0]=CreatePropellantResource(50000000);

 //Thrusters and groups
 grps=(THRUSTER_HANDLE**)malloc(15*sizeof(THRUSTER_HANDLE));
 grpc=(int*)malloc(15*sizeof(int));
 for(i=0;i<15;i++){grps[i]=(THRUSTER_HANDLE*)malloc(17*sizeof(THRUSTER_HANDLE));grpc[i]=0;}
 
 th_h[0]=CreateThruster(_V(0,0,0),_V(0,0,1),5047000000,ph_h[0],5000000000,0,101400);
 grps[0][grpc[0]]=th_h[0];
 grpc[0]++;
 th_h[1]=CreateThruster(_V(0,0,0),_V(0,0,-1),5047000000,ph_h[0],5000000000,0,101400);
 grps[1][grpc[1]]=th_h[1];
 grpc[1]++;
 th_h[2]=CreateThruster(_V(0,0,0),_V(0,1,0),3000000000,ph_h[0],5000000000,0,101400);
 grps[2][grpc[2]]=th_h[2];
 grpc[2]++;
 th_h[3]=CreateThruster(_V(-6,0.7,-0.4),_V(0,-1,0),59060000,ph_h[0],5000000000,0,101400);
 grps[7][grpc[7]]=th_h[3];
 grpc[7]++;
 th_h[4]=CreateThruster(_V(6,-0.7,-0.4),_V(0,1,0),59060000,ph_h[0],5000000000,0,101400);
 grps[7][grpc[7]]=th_h[4];
 grpc[7]++;
 th_h[5]=CreateThruster(_V(-6,-0.7,-0.4),_V(0,1,0),59060000,ph_h[0],5000000000,0,101400);
 grps[8][grpc[8]]=th_h[5];
 grpc[8]++;
 th_h[6]=CreateThruster(_V(6,0.7,-0.4),_V(0,-1,0),59060000,ph_h[0],5000000000,0,101400);
 grps[8][grpc[8]]=th_h[6];
 grpc[8]++;
 th_h[7]=CreateThruster(_V(0,0,15),_V(0,1,0),59060000,ph_h[0],5000000000,0,101400);
 grps[3][grpc[3]]=th_h[7];
 grpc[3]++;
 grps[11][grpc[11]]=th_h[7];
 grpc[11]++;
 th_h[8]=CreateThruster(_V(0,0,-15),_V(0,-1,0),59060000,ph_h[0],5000000000,0,101400);
 grps[3][grpc[3]]=th_h[8];
 grpc[3]++;
 grps[12][grpc[12]]=th_h[8];
 grpc[12]++;
 th_h[9]=CreateThruster(_V(0,0,15),_V(0,-1,0),59060000,ph_h[0],5000000000,0,101400);
 grps[4][grpc[4]]=th_h[9];
 grpc[4]++;
 grps[12][grpc[12]]=th_h[9];
 grpc[12]++;
 th_h[10]=CreateThruster(_V(0,0,-15),_V(0,1,0),59060000,ph_h[0],5000000000,0,101400);
 grps[4][grpc[4]]=th_h[10];
 grpc[4]++;
 grps[11][grpc[11]]=th_h[10];
 grpc[11]++;
 th_h[11]=CreateThruster(_V(0,0,15),_V(1,0,0),59060000,ph_h[0],5000000000,0,101400);
 grps[6][grpc[6]]=th_h[11];
 grpc[6]++;
 grps[9][grpc[9]]=th_h[11];
 grpc[9]++;
 th_h[12]=CreateThruster(_V(0,0,-15),_V(-1,0,0),59060000,ph_h[0],5000000000,0,101400);
 grps[6][grpc[6]]=th_h[12];
 grpc[6]++;
 grps[10][grpc[10]]=th_h[12];
 grpc[10]++;
 th_h[13]=CreateThruster(_V(0,0,15),_V(-1,0,0),59060000,ph_h[0],5000000000,0,101400);
 grps[5][grpc[5]]=th_h[13];
 grpc[5]++;
 grps[10][grpc[10]]=th_h[13];
 grpc[10]++;
 th_h[14]=CreateThruster(_V(0,0,-15),_V(1,0,0),59060000,ph_h[0],5000000000,0,101400);
 grps[5][grpc[5]]=th_h[14];
 grpc[5]++;
 grps[9][grpc[9]]=th_h[14];
 grpc[9]++;
 th_h[15]=CreateThruster(_V(0,0,0),_V(0,0,-1),59060000,ph_h[0],5000000000,0,101400);
 grps[14][grpc[14]]=th_h[15];
 grpc[14]++;
 th_h[16]=CreateThruster(_V(0,0,0),_V(0,0,1),59060000,ph_h[0],5000000000,0,101400);
 grps[13][grpc[13]]=th_h[16];
 grpc[13]++;
 for(i=0;i<15;i++){
  if(i<15)thg_h[i]=CreateThrusterGroup(grps[i],grpc[i],(THGROUP_TYPE)(THGROUP_MAIN+i));
     else thg_h[i]=CreateThrusterGroup(grps[i],grpc[i],THGROUP_USER);
 }

SURFHANDLE tex = oapiRegisterExhaustTexture ("exhaust_atsme");
AddExhaust (th_h, 10, 2, tex);

SURFHANDLE tex2 = oapiRegisterExhaustTexture ("exhaust_atrcs");
AddExhaust (th_h, 10, 2, tex2);

 //Exhausts
 AddExhaust(th_h[0],100,7,_V(0,17.89,-211.068),_V(0,0,-1), tex);
 AddExhaust(th_h[0],150,7,_V(0,17.89,-193.095),_V(0,0,-1), tex);
 AddExhaust(th_h[0],100,7,_V(0,-12.807,-211.068),_V(0,0,-1), tex);
 AddExhaust(th_h[0],150,7,_V(0,-12.807,-193.095),_V(0,0,-1), tex);
 AddExhaust(th_h[1],17,1.4,_V(-13.736,4.766,177.12),_V(0,0,1));
 AddExhaust(th_h[1],17,1.4,_V(13.736,4.766,177.12),_V(0,0,1));
 AddExhaust(th_h[1],17,1.4,_V(-37.883,5.646,20.519),_V(0,0,1));
 AddExhaust(th_h[1],17,1.4,_V(37.883,5.646,20.519),_V(0,0,1));
  AddExhaust(th_h[2],20,2.1,_V(-24.978,-0.929,138.311),_V(0,-1,0));
 AddExhaust(th_h[2],20,2.1,_V(24.978,-0.929,138.311),_V(0,-1,0));
 AddExhaust(th_h[2],20,2.1,_V(24.978,-0.929,128.926),_V(0,-1,0));
 AddExhaust(th_h[2],20,2.1,_V(-24.978,-0.929,128.926),_V(0,-1,0));
 AddExhaust(th_h[2],30,2.1,_V(-49.978,0.293,3.03),_V(0,-1,0));
 AddExhaust(th_h[2],30,2.1,_V(-38.345,0.293,3.03),_V(0,-1,0));
 AddExhaust(th_h[2],30,2.1,_V(49.978,0.293,3.03),_V(0,-1,0));
 AddExhaust(th_h[2],30,2.1,_V(38.345,0.293,3.03),_V(0,-1,0));
 AddExhaust(th_h[2],30,2.1,_V(24.169,-24,-114.860),_V(0,-1,0));
 AddExhaust(th_h[2],30,2.1,_V(24.169,-14.664,-105.475),_V(0,-1,0));
 AddExhaust(th_h[2],30,2.1,_V(-24.169,-14.664,-114.860),_V(0,-1,0));
 AddExhaust(th_h[2],30,2.1,_V(-24.169,-14.664,-105.475),_V(0,-1,0));
 AddExhaust(th_h[9],0.6,0.078,_V(-0.8,-0.25,9.6),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-27.166,15.593,122.826),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-25.43,15.593,122.826),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-23.695,15.593,122.826),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-26.408,21.138,-70.376),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-24.697,21.138,-70.376),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-23.133,21.138,-70.376),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(27.166,15.593,122.826),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(25.43,15.593,122.826),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(23.695,15.593,122.826),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-27.166,-1.784,122.826),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-25.43,-1.784,122.826),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-23.695,-1.784,122.826),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(27.166,-1.784,122.826),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(25.43,-1.784,122.826),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(23.695,-1.784,122.826),_V(0,-1,0), tex2);
 AddExhaust(th_h[11],25,2,_V(-33.728,5.108,122.862),_V(-1,0,0), tex2);
 AddExhaust(th_h[11],25,2,_V(-33.728,6.892,122.862),_V(-1,0,0), tex2);
 AddExhaust(th_h[11],25,2,_V(-33.728,8.456,122.862),_V(-1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(33.728,8.456,122.862),_V(1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(33.728,6.892,122.862),_V(1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(33.728,5.108,122.862),_V(1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(-34.229,1.674,-70.352),_V(-1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(-34.229,3.409,-70.352),_V(-1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(-34.229,5.145,-70.352),_V(-1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(-32.414,-9.556,-110.831),_V(-1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(-32.414,-11.218,-110.831),_V(-1,0,0), tex2);
 AddExhaust(th_h[13],25,2,_V(-32.414,-12.929,-110.831),_V(-1,0,0), tex2);
 AddExhaust(th_h[11],25,2,_V(34.229,1.662,-70.352),_V(1,0,0), tex2);
 AddExhaust(th_h[11],25,2,_V(34.229,3.409,-70.352),_V(1,0,0), tex2);
 AddExhaust(th_h[11],25,2,_V(34.229,5.145,-70.352),_V(1,0,0), tex2);
 AddExhaust(th_h[11],25,2,_V(32.390,-12.975,-110.831),_V(1,0,0), tex2);
 AddExhaust(th_h[11],25,2,_V(32.390,-11.265,-110.831),_V(1,0,0), tex2);
 AddExhaust(th_h[11],25,2,_V(32.390,-9.554,-110.831),_V(1,0,0), tex2);
 AddExhaust(th_h[3],25,2,_V(38.934,-0.22,-32.921),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(37.174,-0.22,-32.921),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(35.463,-0.22,-32.921),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-35.463,-0.22,-32.921),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-37.174,-0.22,-32.921),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-38.934,-0.22,-32.921),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(38.934,11.169,-32.921),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(26.371,21.165,-70.315),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(24.709,21.165,-70.315),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(22.998,21.165,-70.340),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-37.247,11.145,-32.973),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-35.292,11.145,-32.973),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-39.007,11.145,-32.973),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-24.489,-1.809,-110.857),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-23.023,-1.809,-110.857),_V(0,1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(-21.263,-1.809,-110.857),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(21.263,-1.809,-110.857),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(23.023,-1.809,-110.857),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(24.489,-1.809,-110.857),_V(0,1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-27.153,15.541,122.911),_V(0,1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-23.683,15.541,122.911),_V(0,1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-25.443,15.541,122.911),_V(0,1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(25.443,15.541,122.911),_V(0,1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(23.683,15.541,122.911),_V(0,1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(27.153,15.541,122.911),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-24.66,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-22.9,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-21.190,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-26.393,21.147,-70.358),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-24.633,21.147,-70.358),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-23.030,21.147,-70.358),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(23.030,21.147,-70.358),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(24.633,21.147,-70.358),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(26.393,21.147,-70.358),_V(0,1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-26.393,-11.837,-70.358),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-24.633,-11.837,-70.358),_V(0,-1,0), tex2);
 AddExhaust(th_h[5],25,2,_V(-23.030,-11.837,-70.358),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(23.030,-11.837,-70.358),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(24.633,-11.837,-70.358),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(26.393,-11.837,-70.358),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(21.190,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(23.119,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(24.66,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-23.119,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-21.190,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-24.9,-15.688,-110.837),_V(0,-1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(24.9,-1.68,-111.005),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(22.762,-1.68,-111.005),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(21.159,-1.68,-111.005),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-21.159,-1.68,-111.005),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-22.762,-1.68,-111.005),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-24.9,-1.68,-111.005),_V(0,1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-27.153,-1.858,122.862),_V(0,-1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-23.683,-1.858,122.862),_V(0,-1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(-25.491,-1.858,122.862),_V(0,-1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(25.491,-1.858,122.862),_V(0,-1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(23.683,-1.858,122.862),_V(0,-1,0), tex2);
 AddExhaust(th_h[8],25,2,_V(27.153,-1.858,122.862),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(24.624,-15.676,-110.825),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(22.937,-15.676,-110.825),_V(0,-1,0), tex2);
 AddExhaust(th_h[3],25,2,_V(21.178,-15.676,-110.825),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(23.01,-12.181,-70.357),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(26.383,-12.181,-70.357),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(24.721,-12.181,-70.357),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-23.01,-12.181,-70.357),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-26.383,-12.181,-70.357),_V(0,-1,0), tex2);
 AddExhaust(th_h[10],25,2,_V(-24.721,-12.181,-70.357),_V(0,-1,0), tex2);

  	PARTICLESTREAMSPEC contrail_main = {
		0, 23.0, 120, 3000.2, 0.05, 1.3, 9, 99.10, PARTICLESTREAMSPEC::DIFFUSE,
		PARTICLESTREAMSPEC::LVL_PSQRT, 0, 0.1,
		PARTICLESTREAMSPEC::ATM_PLOG, 1e-2, 0.1

	};PARTICLESTREAMSPEC contrail_hover = {
		0, 7.0, 120, 1000.2, 0.05, 0.2, 9, 99.10, PARTICLESTREAMSPEC::DIFFUSE,
		PARTICLESTREAMSPEC::LVL_PSQRT, 0, 0.1,
		PARTICLESTREAMSPEC::ATM_PLOG, 1e-2, 0.1

	};
		PARTICLESTREAMSPEC exhaust_smoke = {
		0, 14.0, 120, 3000.2, 0.05, 1.3, 9, 99.10, PARTICLESTREAMSPEC::DIFFUSE,
		PARTICLESTREAMSPEC::LVL_PSQRT, 0, 0.1,
		PARTICLESTREAMSPEC::ATM_PLOG, 1e-2, 0.1
	};SURFHANDLE tex7 = oapiRegisterParticleTexture ("Exhaust2")
	;exhaust_smoke.tex = oapiRegisterParticleTexture ("Contrail4");
		;AddExhaust (th_h, 16.0, 2.0, tex7);


	PARTICLESTREAMSPEC exhaust_main = {
		0, 10.0, 90, 600.5, 0.05, 0.5, 2, 6.0, PARTICLESTREAMSPEC::EMISSIVE,
		PARTICLESTREAMSPEC::LVL_SQRT, 0, 1,
		PARTICLESTREAMSPEC::ATM_PLOG, 1e-5, 0.1
	};SURFHANDLE tex4 = oapiRegisterParticleTexture ("Exhaust2")
	;exhaust_main.tex = oapiRegisterParticleTexture ("Contrail2");
		;AddExhaust (th_h, 16.0, 2.0, tex4);

  //Exhausts
 ;AddExhaustStream(th_h[0], _V(0,17.89,-193.095), &contrail_main);		//main throttle
  ;AddExhaustStream(th_h[0], _V(0,17.89,-193.095), &contrail_main);
 AddExhaustStream(th_h[0], _V(0,17.89,-193.095), &exhaust_main);
 AddExhaustStream(th_h[0], _V(0,-12.807,-193.095), &contrail_main);
  AddExhaustStream(th_h[0], _V(0,17.89,-193.095), &exhaust_smoke);
 AddExhaustStream(th_h[0], _V(0,-12.807,-193.095), &exhaust_smoke);
  AddExhaustStream(th_h[0], _V(0,-12.807,-193.095), &contrail_main);
 AddExhaustStream(th_h[0], _V(0,-12.807,-193.095), &exhaust_main);		//end main throttle	


  AddExhaustStream(th_h[2], _V(-24.978,-0.929,138.311), &contrail_hover);		//hover smoke
  AddExhaustStream(th_h[2], _V(24.978,-0.929,138.311), &contrail_hover);
  AddExhaustStream(th_h[2], _V(49.966,6.653,258.045), &contrail_hover);
  AddExhaustStream(th_h[2], _V(24.978,-0.929,128.926), &contrail_hover);
  AddExhaustStream(th_h[2], _V(-24.978,-0.929,128.926), &contrail_hover);
  AddExhaustStream(th_h[2], _V(-49.978,0.293,3.03), &contrail_hover);
  AddExhaustStream(th_h[2], _V(-38.345,0.293,3.03), &contrail_hover);
  AddExhaustStream(th_h[2], _V(49.978,0.293,3.03), &contrail_hover);
  AddExhaustStream(th_h[2], _V(38.345,0.293,3.03), &contrail_hover);
  AddExhaustStream(th_h[2], _V(24.169,-24,-114.860), &contrail_hover);
  AddExhaustStream(th_h[2], _V(24.169,-14.664,-105.475), &contrail_hover);	
  AddExhaustStream(th_h[2], _V(-24.169,-14.664,-114.860), &contrail_hover);		//end hover smoke

 //Meshes
 SetMeshVisibilityMode(msh_idh[0]=AddMesh(msh_h[0]=oapiLoadMeshGlobal("SMIPA")),3);

 //Animations
 define_animations();

 //Docks
 CreateDock(_V(0,5.765,179.510),_V(0,0,1),_V(0,1,0));
 CreateDock(_V(0,-11.994,226.518),_V(0,0,1),_V(0,1,0));
 CreateDock(_V(-23.839,-11.098,102.086),_V(-1,0,0),_V(0,1,0));
 CreateDock(_V(-23.839,-11.098,127.936),_V(-1,0,0),_V(0,1,0));
 CreateDock(_V(23.839,-11.098,102.086),_V(1,0,0),_V(0,1,0));
 CreateDock(_V(23.839,-11.098,127.936),_V(1,0,0),_V(0,1,0));

 //Airfoils
 CreateAirfoil3(LIFT_VERTICAL,_V(0,0,0),VLiftCoeff,0,0,69986,1.5);
 CreateAirfoil3(LIFT_HORIZONTAL,_V(0,0,0),HLiftCoeff,0,0,2100,1.5);
 CreateControlSurface2(AIRCTRL_ELEVATOR,70.733,1.5,_V(0,0.7,-14),0,(UINT)-1);
 CreateControlSurface2(AIRCTRL_RUDDER  ,70.733,1.5,_V(0,-0.7,-15),0,(UINT)-1);
 CreateControlSurface2(AIRCTRL_AILERON ,70.733,2.333,_V(12,0.7,-4.7),0,(UINT)-1);
 CreateControlSurface2(AIRCTRL_AILERON ,70.733,2.333,_V(-12,0.7,-4.7),0,(UINT)-1);
}
//############################################################################//
void IPA_Vehicle::clbkLoadStateEx(FILEHANDLE scn,void *vs)
{
 char *line;
 int i,n;

 while(oapiReadScenario_nextline(scn,line)){
  //Animation state loading
  if(!strnicmp(line,"ANIM_",5)){
   sscanf(line+5,"%d",&i);
   if((i>=0)&&(i<ANIM_COUNT)){
    n=0;
    if(i>=10)n=1;
    if(i>=100)n=2;
    if(i>=1000)n=3;
    sscanf(line+6+n,"%d",&ani[i].status);
    sscanf(line+6+n+3,"%lf",&ani[i].proc);
    SetAnimation(ani[i].id,ani[i].proc);
   }
  }else{
   ParseScenarioLineEx(line,vs);
  }
 }
}
//############################################################################//
void IPA_Vehicle::clbkSaveState(FILEHANDLE scn)
{
 SaveDefaultState(scn);
 
 //Animation state
 char cbuf[256],nbuf[256];
 int i;

 for(i=0;i<ANIM_COUNT;i++){
  sprintf(cbuf,"%d %0.4f",ani[i].status,ani[i].proc);
  sprintf(nbuf,"ANIM_%d",i);
  oapiWriteScenario_string(scn,nbuf,cbuf);
 }
}
//############################################################################//
int  IPA_Vehicle::clbkConsumeBufferedKey(DWORD key,bool down,char *kstate)
{
 int i;
 if(!down)return 0;
 for(i=0;i<ANIM_COUNT;i++)if(ani[i].tp==0)if(key==ani[i].trigkey){
  //Animation input
  if(!ani[i].repeat){
   switch(ani[i].status){
    //Fix it short
    case -2:ani[i].status=1;break;
    case -1:ani[i].status=1;break;
    case  1:ani[i].status=-1;break;
    case  2:ani[i].status=-1;break;
    default:ani[i].status=2;
   }
  }else{
   switch(ani[i].status){
    case 1:ani[i].status=0;break;
    case 0:ani[i].status=1;break;
    default:ani[i].status=0;
   }
  }
 }
 return 0;
}
//#######################################################################################//
void IPA_Vehicle::clbkPostStep(double simt,double simdt,double mjd)
{
 //Animation timing controls
 int i;
 for(i=0;i<ANIM_COUNT;i++)if(abs(ani[i].status)==1){
  double da=simdt*ani[i].spd;
  if(ani[i].repeat){
   ani[i].proc=fmod(ani[i].proc+da,1);
  }else{
   if(ani[i].status==-1){
    if(ani[i].proc>0.0)ani[i].proc=max(0.0,ani[i].proc-da);
    else                     ani[i].status=-2;
   }else{
    if(ani[i].proc<1.0)ani[i].proc=min(1.0,ani[i].proc+da);
    else                     ani[i].status=2;
   }
  }
  SetAnimation(ani[i].id,ani[i].proc);
 }
}
//#######################################################################################//
//Creation
DLLCLBK void InitModule(HINSTANCE hModule){}
DLLCLBK void ExitModule(HINSTANCE hModule){}
DLLCLBK VESSEL *ovcInit(OBJHANDLE hvessel,int flightmodel){return new IPA_Vehicle(hvessel,flightmodel);}
DLLCLBK void ovcExit(VESSEL *vessel){if(vessel)delete(IPA_Vehicle*)vessel;}
//#######################################################################################//
 
BruceJohnJennerLawso

BruceJohnJennerLawso

Dread Lord of the Idiots
Addon Developer
Joined
Apr 14, 2012
Messages
2,585
Reaction score
0
Points
36
Are you sure youve made it complicated enough? You have enough particle streams there to make it seem like its leaking :lol:. The issue here is that you dont appear to have any sort of function that can create a vessel in the simulation. The steps to getting that are complicated, but a good first step would be to go over to Hlynqacs (sorry I can never remember how its spelled) code repository on sourceforge, find the appropriate function, and add it to your project.
 
You must log in or register to reply here.

Similar threads

Mr Martian
API Question Help redrawing virtual cockpit displays in D3D9
Replies
11
Views
307
jarmonik
J
gattispilot
SDK Question moveing cockpit camera
Replies
3
Views
540
gattispilot
gattispilot
gattispilot
SDK Question Drawing on a texture for a HUD
Replies
6
Views
305
gattispilot
gattispilot
Mr Martian
SDK Question Advice for Creating EXHAUSTSPEC Without Thrusters
Replies
1
Views
734
GLS
GLS
S
SDK Question Setting Up Visual Studio - Newbie building errors with sample projects
Replies
1
Views
708
kuddel
kuddel
Top