Vessel Chang'e 4 Lander, Rover, Queqiao and Longjiang 1 and 2 Lunar probes

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Jeremyxxx

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Here we go again!

============================ ERROR: ===========================
Mesh not found: .\Meshes\.msh
[LoadMesh | .\Mesh.cpp | 1269]
===============================================================
============================ ERROR: ===========================
Could not load vessel module: Queqiao
[Vessel::LoadModule | .\Vessel.cpp | 5747]
===============================================================
============================ ERROR: ===========================
Mesh not found: .\Meshes\.msh
[LoadMesh | .\Mesh.cpp | 1269]
===============================================================
000033.509: **** Closing simulation session
 
gattispilot

gattispilot

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Weird. So is the module in the module folder and cfg present
 
gattispilot

gattispilot

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If it is there I wonder why it will not load?

Can you open a scn and try to load the Queqiao in and see what happens?

So on the lander:
I change the touchdown points to this:
const double pesototal = MASS +FUELMASS;
const double xtx_target = -0.1;
const double xtst = (-1)*(pesototal*9.80655) / (3 * xtx_target);
const double xtda = 0.9*(2 * sqrt(pesototal*xtst));

static const DWORD ntdvtx_geardown = 3;
static TOUCHDOWNVTX tdvtx_geardown[ntdvtx_geardown] = {
{ _V(-4, -3.2806, -4), xtst, xtda, 500.0, 500.0 },
{ _V(4, -3.2806, -4), xtst, xtda, 500.0, 500.0 },
{ _V(4, -3.2806, 4), xtst, xtda, 500.0, 500.0 }
};

But now when I lift off using rcs I get that tilt/rotation.
 
Last edited:
J

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============================ ERROR: ===========================
Could not load vessel module: Queqiao
[Vessel::LoadModule | .\Vessel.cpp | 5747]
===============================================================
 
gattispilot

gattispilot

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That is weird since the cfg and dll are there?

try this scn:
Code: 
BEGIN_DESC
Current scenario state


Contains the latest simulation state.
END_DESC

BEGIN_ENVIRONMENT
  System Sol
  Date MJD 58489.7398161821
  Help CurrentState_img
END_ENVIRONMENT

BEGIN_FOCUS
  Ship Queqiao
END_FOCUS

BEGIN_CAMERA
  TARGET Queqiao
  MODE Extern
  POS 3.647426 51.852680 -34.273494
  TRACKMODE TargetRelative
  FOV 58.27
END_CAMERA

BEGIN_HUD
  TYPE Surface
END_HUD

BEGIN_SHIPS
ISS:ProjectAlpha_ISS
  STATUS Orbiting Earth
  RPOS -6524891.159 1380887.538 902059.354
  RVEL 1224.5876 7246.4040 -2292.7146
  AROT 174.165 -14.481 -27.111
  VROT 0.0890 -0.0295 -0.0520
  AFCMODE 7
  IDS 0:588 100 1:586 100 2:584 100 3:582 100 4:580 100
  NAVFREQ 0 0
  XPDR 466
END
Queqiao:Queqiao
  SOLP 0 0.2500 0 1.0000 
  ANTENNA 0 0.0000
  PANEL 0 0.0000
  STATUS Orbiting Earth
  RPOS 5665548.461 -283.592 4121915.301
  RVEL -4442.3909 -1.4002 6096.1141
  AROT 0.000 0.734 0.000
  VROT 0.0000 0.0082 0.0000
  AFCMODE 7
  NAVFREQ 0 0
  XPDR 0
END
END_SHIPS
 
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Jeremyxxx

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Did test out the scenario.... Still invisible!

============================ ERROR: ===========================
Could not load vessel module: Queqiao
[Vessel::LoadModule | .\Vessel.cpp | 5747]
===============================================================
 
gattispilot

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And module and cfg are there, right? Not sure what is going on. Can you post the cfg?
 
gattispilot

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So lets try this.

It is just the satellite,cfg ,dll,mesh and scn:
https://drive.google.com/open?id=1UDefxcczbzCw1vzhwbF5hzQOPOotXxEl

---------- Post added at 05:53 AM ---------- Previous post was at 05:02 AM ----------

On the lander. At a lost.

HAve tried different landing points and now when I lift up using rcs it spins badly.
Code: 
// point, stiffness, dampening, isotropic/lateral friction coefficient, longitudinal friction coefficient (only used for first 3 points)
const double pesototal = MASS +FUELMASS;
const double xtx_target = -0.1;
const double xtst = (-1)*(pesototal*9.80655) / (3 * xtx_target);
const double xtda = 0.9*(2 * sqrt(pesototal*xtst));

static const DWORD ntdvtx_geardown = 3;
static TOUCHDOWNVTX tdvtx_geardown[ntdvtx_geardown] = {
	{ _V(4, -3.2806, -4), xtst, xtda, 500.0, 500.0 },
	{ _V(0, -3.2806, 4), xtst, xtda, 500.0, 500.0 },
	{ _V(-4, -3.2806, -4), xtst, xtda, 500.0, 500.0 }
};

//POINT_1 = -10.0 - 3.2806 - 10.0
//POINT_2 = 10.0 - 3.2806 - 10.0
//POINT_3 = 10.0 - 3.2806  10.0
//POINT_4 = -10.0 - 3.2806  10.0

Code: 
ph_main = CreatePropellantResource(FUELMASS);

th_hover[0] = CreateThruster(_V(6, 0, 10), _V(0, 1, 0), 10000/4, ph_main, RCS_ISP);
th_hover[1] = CreateThruster(_V(-6, 0, 10), _V(0, 1, 0), 10000/4, ph_main, RCS_ISP);
th_hover[2] = CreateThruster(_V(6, 0, -10), _V(0, 1, 0), 10000/4, ph_main, RCS_ISP);
th_hover[3] = CreateThruster(_V(-6, 0, -10), _V(0, 1, 0), 10000/4, ph_main, RCS_ISP);

AddExhaust(th_hover[0], 1, 0.3, _V(0, -2.8, 0), _V(0, -1, 0));
thg_hover = CreateThrusterGroup(th_hover,4, THGROUP_HOVER);







th_rcs[0] = CreateThruster(_V(6, 0, 10), _V(0, -1, 0), RCS_THRUST, ph_main, RCS_ISP);
//AddExhaust(th_rcs[0], 1, .1, _V(2.063, 1.0571, 8.3072), _V(0, 1, 0));
// AddExhaust(th_rcs[0], 1, 0.1, _V(1.2234, 1.1706, .782), _V(0, 1, 0));
// Delantero derecho inferior
th_rcs[1] = CreateThruster(_V(6, 0, 10), _V(0, 1, 0), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[1], .5, 0.1, _V(1.261, -2.6, 1.175), _V(0, -1, 0));
AddExhaust(th_rcs[1], .5, 0.1, _V(1.158, -2.6, 1.277), _V(0, -1, 0));// Delantero derecho proa
// Delantero derecho proa
th_rcs[2] = CreateThruster(_V(6, 0, 10), _V(0, 0, -1), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[2], .5, .1, _V(1.167, -1.86, 1.325), _V(0, 0, 1));
//AddExhaust(th_rcs[2], .5, .01, _V(1.1555, 1.2106, .766), _V(-0.464, 0, .8858));
//AddExhaust(th_rcs[2], .5, 0.01, _V(1.148, 1.2179, .782), _V(0, 0, 1));
// Delantero derecho popa
th_rcs[3] = CreateThruster(_V(6, 0, 10), _V(0, 0, 1), RCS_THRUST, ph_main, RCS_ISP);
//AddExhaust(th_rcs[3], 1, .10, _V(0.922, .046, -7.5872), _V(0, 0, -1));
// Delantero derecho exterior
th_rcs[4] = CreateThruster(_V(6, 0, 10), _V(-1, 0, 0), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[4], .5, 0.1, _V(1.324, -1.86, 1.164), _V(1, 0, 0));

// Grupo delantero izquierdo

// Delantero izquierdo superior
th_rcs[5] = CreateThruster(_V(-6, 0, 10), _V(0, -1, 0), RCS_THRUST, ph_main, RCS_ISP);
//AddExhaust(th_rcs[5], 1, .10, _V(-2.063, 1.0571, 8.3072), _V(0, 1, 0));

//AddExhaust(th_rcs[5], 1, 0.1, _V(-1.2234, 1.1706, .782), _V(0, 1, 0));
// Delantero izquierdo inferior
th_rcs[6] = CreateThruster(_V(-6, 0, 10), _V(0, 1, 0), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[6], .5, 0.1, _V(-1.261, -2.6, 1.175), _V(0, -1, 0));
AddExhaust(th_rcs[6], .5, 0.1, _V(-1.158, -2.6, 1.277), _V(0, -1, 0));// Delantero derecho proa
// Delantero izquierdo proa
th_rcs[7] = CreateThruster(_V(-6, 0, 10), _V(0, 0, -1), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[7], .51, .1, _V(-1.167, -1.86, 1.325), _V(0, 0, 1));

//AddExhaust(th_rcs[7], .5, 0.01, _V(-1.148, 1.2179, .782), _V(0, 0, 1));
// Delantero izquierdo popa
th_rcs[8] = CreateThruster(_V(-6, 0, 10), _V(0, 0, 1), RCS_THRUST, ph_main, RCS_ISP);
//AddExhaust(th_rcs[8], 1, .10, _V(-0.922, .046, -7.5872), _V(0, 0, -1));

//AddExhaust(th_rcs[8], .5, 0.01, _V(-1.148, 1.2179, .782), _V(0, 0, -1));
// Delantero izquierdo exterior
th_rcs[9] = CreateThruster(_V(-6, 0, 10), _V(1, 0, 0), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[9], .5, 0.1, _V(-1.324, -1.86, -1.164), _V(-1, 0, 0));


// Grupo trasero derecho

// Trasero derecho superior
th_rcs[10] = CreateThruster(_V(6, 0, -10), _V(0, -1, 0), RCS_THRUST, ph_main, RCS_ISP);
//AddExhaust(th_rcs[10], 1, .10, _V(3.4827, .3, -7.4698), _V(0, 1, 0));
//AddExhaust(th_rcs[10], 1, 0.1, _V(1.2234, 1.1706, .782), _V(0, 1, 0));
// Trasero derecho inferior
th_rcs[11] = CreateThruster(_V(6, 0, -10), _V(0, 1, 0), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[11], .5, 0.1, _V(1.261, -2.6, -1.175), _V(0, -1, 0));
AddExhaust(th_rcs[11], .5, 0.1, _V(1.158, -2.6, -1.277), _V(0, -1, 0));// Delantero derecho proa
// Trasero derecho proa
th_rcs[12] = CreateThruster(_V(6, 0, -10), _V(0, 0, -1), RCS_THRUST, ph_main, RCS_ISP);
//AddExhaust(th_rcs[12], 1, .10, _V(1.68, -1.67, -.575), _V(.577, -.577, -.577));

//AddExhaust(th_rcs[12], .5, 0.01, _V(1.148, 1.2179, -.782), _V(0, 0, 1));
// Trasero derecho popa
th_rcs[13] = CreateThruster(_V(6, 0, -10), _V(0, 0, 1), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[13], .5, .1, _V(1.167, -1.86, -1.325), _V(0, 0, -1));

//AddExhaust(th_rcs[13], .5, 0.01, _V(1.148, 1.2179, -.782), _V(0, 0, -1));
// Trasero derecho exterior
th_rcs[14] = CreateThruster(_V(6, 0, -10), _V(-1, 0, 0), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[14], .5, 0.1, _V(1.324, -1.86, -1.164), _V(1, 0, 0));

// Grupo trasero izquierdo

// Trasero izquierdo superior
th_rcs[15] = CreateThruster(_V(-6, 0, -10), _V(0, -1, 0), RCS_THRUST, ph_main, RCS_ISP);
//AddExhaust(th_rcs[15], 1, 0.1, _V(-3.4827, .3, -7.4698), _V(0, 1, 0));
// Trasero izquierdo inferior
th_rcs[16] = CreateThruster(_V(-6, 0, -10), _V(0, 1, 0), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[16], .5, 0.1, _V(-1.261, -2.6, -1.175), _V(0, -1, 0));
AddExhaust(th_rcs[16], .5, 0.1, _V(-1.158, -2.6, -1.277), _V(0, -1, 0));// Delantero derecho proa
// Trasero izquierdo proa
th_rcs[17] = CreateThruster(_V(-6, 0, -10), _V(0, 0, -1), RCS_THRUST, ph_main, RCS_ISP);
//AddExhaust(th_rcs[17], .5, 0.01, _V(-1.148, 1.2179, -.782), _V(0, 0, 1));
// Trasero izquierdo popa
th_rcs[18] = CreateThruster(_V(-6, 0, -10), _V(0, 0, 1), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[18], .5, .1, _V(-1.167, -1.86, -1.325), _V(0, 0, -1));
// Trasero izquierdo exterior
th_rcs[19] = CreateThruster(_V(-6, 0, -10), _V(1, 0, 0), RCS_THRUST, ph_main, RCS_ISP);
AddExhaust(th_rcs[19], .5, 0.1, _V(-1.324, -1.86, -1.164), _V(-1, 0, 0));

////visual rcs

// Grupo motor de cabeceo hacia arriba "PITCH-UP"
th_group[0] = th_rcs[1];
th_group[1] = th_rcs[6];
th_group[2] = th_rcs[10];
th_group[3] = th_rcs[15];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_PITCHUP);

// Grupo motor de cabeceo hacia abajo "PITCH-DOWN"
th_group[0] = th_rcs[0];

th_group[1] = th_rcs[5];
th_group[2] = th_rcs[11];
th_group[3] = th_rcs[16];
//th_group[4] = th_rcs[21];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_PITCHDOWN);

// Grupo motor de balanceo izquierda "YAW-RIGHT"
th_group[0] = th_rcs[8];
th_group[1] = th_rcs[18];
th_group[2] = th_rcs[2];
th_group[3] = th_rcs[12];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_YAWRIGHT);

// Grupo motor de balanceo derecha "YAW-LEFT"
th_group[0] = th_rcs[3];
th_group[1] = th_rcs[13];
th_group[2] = th_rcs[7];
th_group[3] = th_rcs[17];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_YAWLEFT);

// Grupo motor de alabeo derecho "BANK-RIGHT"
th_group[0] = th_rcs[0];
th_group[1] = th_rcs[6];
th_group[2] = th_rcs[10];
th_group[3] = th_rcs[16];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_BANKRIGHT);

// Grupo motor de alabeo izquierdo "BANK-LEFT"
th_group[0] = th_rcs[1];
th_group[1] = th_rcs[5];
th_group[2] = th_rcs[11];
th_group[3] = th_rcs[15];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_BANKLEFT);

// 2-Movimientos traslacionales

// Grupo motor de traslación derecha "RIGHT"
// Este grupo lo podían formar los impulsores izquierdos delantero de proa y trasero de popa
th_group[0] = th_rcs[9];
th_group[1] = th_rcs[19];
CreateThrusterGroup(th_group, 2, THGROUP_ATT_RIGHT);

// Grupo motor de traslación izquierda "LEFT"
// Este grupo lo podían formar los impulsores derechos delantero de proa y trasero de popa
th_group[0] = th_rcs[4];
th_group[1] = th_rcs[14];
CreateThrusterGroup(th_group, 2, THGROUP_ATT_LEFT);

// Grupo motor de traslación arriba "DOWN"
th_group[0] = th_rcs[0];
th_group[1] = th_rcs[5];
th_group[2] = th_rcs[10];
th_group[3] = th_rcs[15];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_DOWN);

// Grupo motor de traslación abajo "UP"
th_group[0] = th_rcs[1];
th_group[1] = th_rcs[6];
th_group[2] = th_rcs[11];
th_group[3] = th_rcs[16];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_UP);

// Grupo motor de traslación adelante "FORWARD"
th_group[0] = th_rcs[3];
th_group[1] = th_rcs[8];
th_group[2] = th_rcs[13];
th_group[3] = th_rcs[18];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_FORWARD);

// Grupo motor de traslación atrás "BACK"
th_group[0] = th_rcs[2];
th_group[1] = th_rcs[7];
th_group[2] = th_rcs[12];
th_group[3] = th_rcs[17];
CreateThrusterGroup(th_group, 4, THGROUP_ATT_BACK);
 
J

Jeremyxxx

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Tried again, but still the same as multiple attempts on my computer!

============================ ERROR: ===========================
Could not load vessel module: Queqiao
[Vessel::LoadModule | .\Vessel.cpp | 5747]
===============================================================
 
gattispilot

gattispilot

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Not sure why the module will not load. The cfg and dll is present.
 
J

Jeremyxxx

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It might of been due to my computer not having the harddrive or the D3D9 that would make the Queqiao work.
 
gattispilot

gattispilot

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Jeremyxxx said:
It might of been due to my computer not having the harddrive or the D3D9 that would make the Queqiao work.
Click to expand...
not sure about that. I haven't tested in d3d9 though. Have you tried regular graphics?
 
gattispilot

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I have no clue.

So on the lander I am trying to load the SpiderLEm example to get to work. Still got issues;(



not sure how to fix them?
Code: 
Error	8	error LNK2001: unresolved external symbol "public: bool __thiscall SpiderLEM::eTimerRunning(void)" (?eTimerRunning@SpiderLEM@@QAE_NXZ)	C:\Orbiter2016\Orbitersdk\samples\CHANGE4LANDERnew\SpiderLEM.obj	CHANGE4LANDER
h.
Code: 
	bool	eTimerRunning();
Code: 
if (eTimerRunning())
	{
		switch (eTimeMode) // Event Clock
		{
		case STOPPED:
			eTime = eTime + 0;
			break;
		case COUNTUP:
			eTime = eTime + simdt;
			break;
		case COUNTDOWN:
			eTime = eTime - simdt;
			break;
		}
	}
 
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