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#include <stdio.h>
#include <stdlib.h>
#include <string.h>
#include <math.h>
#include <unistd.h>
#include <sys/time.h>
#include <time.h>
#include "telescope_simulator.h"
#include "indicom.h"
#include <memory>
// We declare an auto pointer to ScopeSim.
std::auto_ptr<ScopeSim> telescope_sim(0);
#define GOTO_RATE 2 /* slew rate, degrees/s */
#define SLEW_RATE 0.5 /* slew rate, degrees/s */
#define FINE_SLEW_RATE 0.1 /* slew rate, degrees/s */
#define SID_RATE 0.004178 /* sidereal rate, degrees/s */
#define GOTO_LIMIT 5 /* Move at GOTO_RATE until distance from target is GOTO_LIMIT degrees */
#define SLEW_LIMIT 2 /* Move at SLEW_LIMIT until distance from target is SLEW_LIMIT degrees */
#define FINE_SLEW_LIMIT 0.5 /* Move at FINE_SLEW_RATE until distance from target is FINE_SLEW_LIMIT degrees */
#define POLLMS 250 /* poll period, ms */
#define RA_AXIS 0
#define DEC_AXIS 1
#define GUIDE_NORTH 0
#define GUIDE_SOUTH 1
#define GUIDE_WEST 0
#define GUIDE_EAST 1
void ISPoll(void *p);
void ISInit()
{
static int isInit =0;
if (isInit == 1)
return;
isInit = 1;
if(telescope_sim.get() == 0) telescope_sim.reset(new ScopeSim());
//IEAddTimer(POLLMS, ISPoll, NULL);
}
void ISGetProperties(const char *dev)
{
ISInit();
telescope_sim->ISGetProperties(dev);
}
void ISNewSwitch(const char *dev, const char *name, ISState *states, char *names[], int num)
{
ISInit();
telescope_sim->ISNewSwitch(dev, name, states, names, num);
}
void ISNewText( const char *dev, const char *name, char *texts[], char *names[], int num)
{
ISInit();
telescope_sim->ISNewText(dev, name, texts, names, num);
}
void ISNewNumber(const char *dev, const char *name, double values[], char *names[], int num)
{
ISInit();
telescope_sim->ISNewNumber(dev, name, values, names, num);
}
void ISNewBLOB (const char *dev, const char *name, int sizes[], int blobsizes[], char *blobs[], char *formats[], char *names[], int n)
{
INDI_UNUSED(dev);
INDI_UNUSED(name);
INDI_UNUSED(sizes);
INDI_UNUSED(blobsizes);
INDI_UNUSED(blobs);
INDI_UNUSED(formats);
INDI_UNUSED(names);
INDI_UNUSED(n);
}
void ISSnoopDevice (XMLEle *root)
{
INDI_UNUSED(root);
}
ScopeSim::ScopeSim()
{
//ctor
currentRA=15;
currentDEC=15;
Parked=false;
GuideNSNP = new INumberVectorProperty;
GuideWENP = new INumberVectorProperty;
EqPECNV = new INumberVectorProperty;
GuideRateNP = new INumberVectorProperty;
PECErrNSSP = new ISwitchVectorProperty;
PECErrWESP = new ISwitchVectorProperty;
/* initialize random seed: */
srand ( time(NULL) );
}
ScopeSim::~ScopeSim()
{
//dtor
}
const char * ScopeSim::getDefaultName()
{
return (char *)"Telescope Simulator";
}
bool ScopeSim::initProperties()
{
/* Make sure to init parent properties first */
INDI::Telescope::initProperties();
/* Property for guider support. How many seconds to guide either northward or southward? */
IUFillNumber(&GuideNSN[GUIDE_NORTH], "TIMED_GUIDE_N", "North (sec)", "%g", 0, 10, 0.001, 0);
IUFillNumber(&GuideNSN[GUIDE_SOUTH], "TIMED_GUIDE_S", "South (sec)", "%g", 0, 10, 0.001, 0);
IUFillNumberVector(GuideNSNP, GuideNSN, 2, deviceName(), "TELESCOPE_TIMED_GUIDE_NS", "Guide North/South", MOTION_TAB, IP_RW, 0, IPS_IDLE);
/* Property for guider support. How many seconds to guide either westward or eastward? */
IUFillNumber(&GuideWEN[GUIDE_WEST], "TIMED_GUIDE_W", "West (sec)", "%g", 0, 10, 0.001, 0);
IUFillNumber(&GuideWEN[GUIDE_EAST], "TIMED_GUIDE_E", "East (sec)", "%g", 0, 10, 0.001, 0);
IUFillNumberVector(GuideWENP, GuideWEN, 2, deviceName(), "TELESCOPE_TIMED_GUIDE_WE", "Guide West/East", MOTION_TAB, IP_RW, 0, IPS_IDLE);
/* Simulated periodic error in RA, DEC */
IUFillNumber(&EqPECN[RA_AXIS],"RA_PEC","RA (hh:mm:ss)","%010.6m",0,24,0,15.);
IUFillNumber(&EqPECN[DEC_AXIS],"DEC_PEC","DEC (dd:mm:ss)","%010.6m",-90,90,0,15.);
IUFillNumberVector(EqPECNV,EqPECN,2,deviceName(),"EQUATORIAL_PEC","Periodic Error",MOTION_TAB,IP_RO,60,IPS_IDLE);
/* Enable client to manually add periodic error northward or southward for simulation purposes */
IUFillSwitch(&PECErrNSS[MOTION_NORTH], "PEC_N", "North", ISS_OFF);
IUFillSwitch(&PECErrNSS[MOTION_SOUTH], "PEC_S", "South", ISS_OFF);
IUFillSwitchVector(PECErrNSSP, PECErrNSS, 2, deviceName(),"PEC_NS", "PE N/S", MOTION_TAB, IP_RW, ISR_1OFMANY, 60, IPS_IDLE);
/* Enable client to manually add periodic error westward or easthward for simulation purposes */
IUFillSwitch(&PECErrWES[MOTION_WEST], "PEC_W", "West", ISS_OFF);
IUFillSwitch(&PECErrWES[MOTION_EAST], "PEC_E", "East", ISS_OFF);
IUFillSwitchVector(PECErrWESP, PECErrWES, 2, deviceName(),"PEC_WE", "PE W/E", MOTION_TAB, IP_RW, ISR_1OFMANY, 60, IPS_IDLE);
/* How fast do we guide compared to sideral rate */
IUFillNumber(&GuideRateN[RA_AXIS], "GUIDE_RATE_WE", "W/E Rate", "%g", 0, 1, 0.1, 0.3);
IUFillNumber(&GuideRateN[DEC_AXIS], "GUIDE_RATE_NS", "N/S Rate", "%g", 0, 1, 0.1, 0.3);
IUFillNumberVector(GuideRateNP, GuideRateN, 2, deviceName(), "GUIDE_RATE", "Guiding Rate", MOTION_TAB, IP_RW, 0, IPS_IDLE);
/* Add debug controls so we may debug driver if necessary */
addDebugControl();
return true;
}
void ScopeSim::ISGetProperties (const char *dev)
{
/* First we let our parent populate */
INDI::Telescope::ISGetProperties(dev);
if(isConnected())
{
defineNumber(GuideNSNP);
defineNumber(GuideWENP);
defineNumber(GuideRateNP);
defineNumber(EqPECNV);
defineSwitch(PECErrNSSP);
defineSwitch(PECErrWESP);
}
return;
}
bool ScopeSim::updateProperties()
{
INDI::Telescope::updateProperties();
if (isConnected())
{
defineNumber(GuideNSNP);
defineNumber(GuideWENP);
defineNumber(GuideRateNP);
defineNumber(EqPECNV);
defineSwitch(PECErrNSSP);
defineSwitch(PECErrWESP);
}
else
{
deleteProperty(GuideNSNP->name);
deleteProperty(GuideWENP->name);
deleteProperty(EqPECNV->name);
deleteProperty(PECErrNSSP->name);
deleteProperty(PECErrNSSP->name);
deleteProperty(GuideRateNP->name);
}
return true;
}
bool ScopeSim::Connect()
{
bool rc=false;
if(isConnected()) return true;
rc=Connect(PortT[0].text);
if(rc)
SetTimer(POLLMS);
return rc;
}
bool ScopeSim::Connect(char *)
{
return true;
}
bool ScopeSim::Disconnect()
{
return true;
}
bool ScopeSim::ReadScopeStatus()
{
static struct timeval ltv;
struct timeval tv;
double dt=0, da_ra=0, da_dec=0, dx=0, dy=0, ra_guide_dt=0, dec_guide_dt=0;
static double last_dx=0, last_dy=0;
int nlocked, ns_guide_dir=-1, we_guide_dir=-1;
char RA_DISP[64], DEC_DISP[64], RA_GUIDE[64], DEC_GUIDE[64], RA_PEC[64], DEC_PEC[64], RA_TARGET[64], DEC_TARGET[64];
/* update elapsed time since last poll, don't presume exactly POLLMS */
gettimeofday (&tv, NULL);
if (ltv.tv_sec == 0 && ltv.tv_usec == 0)
ltv = tv;
dt = tv.tv_sec - ltv.tv_sec + (tv.tv_usec - ltv.tv_usec)/1e6;
ltv = tv;
if ( fabs(targetRA - currentRA)*15. >= GOTO_LIMIT )
da_ra = GOTO_RATE *dt;
else if ( fabs(targetRA - currentRA)*15. >= SLEW_LIMIT )
da_ra = SLEW_RATE *dt;
else
da_ra = FINE_SLEW_RATE *dt;
if ( fabs(targetDEC - currentDEC) >= GOTO_LIMIT )
da_dec = GOTO_RATE *dt;
else if ( fabs(targetDEC - currentDEC) >= SLEW_LIMIT )
da_dec = SLEW_RATE *dt;
else
da_dec = FINE_SLEW_RATE *dt;
switch (MovementNSSP->s)
{
case IPS_BUSY:
if (MovementNSS[MOTION_NORTH].s == ISS_ON)
currentDEC += da_dec;
else if (MovementNSS[MOTION_SOUTH].s == ISS_ON)
currentDEC -= da_dec;
NewRaDec(currentRA, currentDEC);
return true;
break;
}
switch (MovementWESP->s)
{
case IPS_BUSY:
if (MovementWES[MOTION_WEST].s == ISS_ON)
currentRA += da_ra/15.;
else if (MovementWES[MOTION_EAST].s == ISS_ON)
currentRA -= da_ra/15.;
NewRaDec(currentRA, currentDEC);
return true;
break;
}
/* Process per current state. We check the state of EQUATORIAL_EOD_COORDS_REQUEST and act acoordingly */
switch (TrackState)
{
case SCOPE_IDLE:
EqNV->s = IPS_IDLE;
break;
case SCOPE_SLEWING:
case SCOPE_PARKING:
/* slewing - nail it when both within one pulse @ SLEWRATE */
nlocked = 0;
dx = targetRA - currentRA;
if (fabs(dx)*15. <= da_ra)
{
currentRA = targetRA;
nlocked++;
}
else if (dx > 0)
currentRA += da_ra/15.;
else
currentRA -= da_ra/15.;
dy = targetDEC - currentDEC;
if (fabs(dy) <= da_dec)
{
currentDEC = targetDEC;
nlocked++;
}
else if (dy > 0)
currentDEC += da_dec;
else
currentDEC -= da_dec;
EqNV->s = IPS_BUSY;
if (nlocked == 2)
{
if (TrackState == SCOPE_SLEWING)
{
// Initially no PEC in both axis.
EqPECN[0].value = currentRA;
EqPECN[1].value = currentDEC;
IDSetNumber(EqPECNV, NULL);
TrackState = SCOPE_TRACKING;
EqNV->s = IPS_OK;
IDMessage(deviceName(), "Telescope slew is complete. Tracking...");
}
else
{
TrackState = SCOPE_PARKED;
EqNV->s = IPS_IDLE;
IDMessage(deviceName(), "Telescope parked successfully.");
}
}
break;
case SCOPE_TRACKING:
/* tracking */
if (GuideNSN[GUIDE_NORTH].value > 0)
{
if (isDebug())
IDLog(" ****** Commanded to GUIDE NORTH for %g ms *****\n", GuideNSN[GUIDE_NORTH].value*1000);
ns_guide_dir = GUIDE_NORTH;
}
else if (GuideNSN[GUIDE_SOUTH].value > 0)
{
if (isDebug())
IDLog(" ****** Commanded to GUIDE SOUTH for %g ms *****\n", GuideNSN[GUIDE_SOUTH].value*1000);
ns_guide_dir = GUIDE_SOUTH;
}
// WE Guide Selection
if (GuideWEN[GUIDE_WEST].value > 0)
{
we_guide_dir = GUIDE_WEST;
if (isDebug())
IDLog(" ****** Commanded to GUIDE WEST for %g ms ****** \n", GuideWEN[GUIDE_WEST].value*1000);
}
else if (GuideWEN[GUIDE_EAST].value > 0)
{
we_guide_dir = GUIDE_EAST;
if (isDebug())
IDLog(" ****** Commanded to GUIDE EAST for %g ms ****** \n", GuideWEN[GUIDE_EAST].value*1000);
}
if (ns_guide_dir != -1)
{
dec_guide_dt = SID_RATE * GuideRateN[DEC_AXIS].value * GuideNSN[ns_guide_dir].value * (ns_guide_dir==GUIDE_NORTH ? 1 : -1);
// If time remaining is more that dt, then decrement and
if (GuideNSN[ns_guide_dir].value >= dt)
GuideNSN[ns_guide_dir].value -= dt;
else
GuideNSN[ns_guide_dir].value = 0;
EqPECN[DEC_AXIS].value += dec_guide_dt;
if (GuideNSN[ns_guide_dir].value <= 0)
{
GuideNSN[GUIDE_NORTH].value = GuideNSN[GUIDE_SOUTH].value = 0;
GuideNSNP->s = IPS_OK;
IDSetNumber(GuideNSNP, NULL);
}
else
IDSetNumber(GuideNSNP, NULL);
}
if (we_guide_dir != -1)
{
ra_guide_dt = SID_RATE/15.0 * GuideRateN[RA_AXIS].value * GuideWEN[we_guide_dir].value* (we_guide_dir==GUIDE_WEST ? -1 : 1);
if (GuideWEN[we_guide_dir].value >= dt)
GuideWEN[we_guide_dir].value -= dt;
else
GuideWEN[we_guide_dir].value = 0;
EqPECN[RA_AXIS].value += ra_guide_dt;
if (GuideWEN[we_guide_dir].value <= 0)
{
GuideWEN[GUIDE_WEST].value = GuideWEN[GUIDE_EAST].value = 0;
GuideWENP->s = IPS_OK;
IDSetNumber(GuideWENP, NULL);
}
else
IDSetNumber(GuideWENP, NULL);
}
//Mention the followng:
// Current RA displacemet and direction
// Current DEC displacement and direction
// Amount of RA GUIDING correction and direction
// Amount of DEC GUIDING correction and direction
dx = EqPECN[RA_AXIS].value - targetRA;
dy = EqPECN[DEC_AXIS].value - targetDEC;
fs_sexa(RA_DISP, fabs(dx), 2, 3600 );
fs_sexa(DEC_DISP, fabs(dy), 2, 3600 );
fs_sexa(RA_GUIDE, fabs(ra_guide_dt), 2, 3600 );
fs_sexa(DEC_GUIDE, fabs(dec_guide_dt), 2, 3600 );
fs_sexa(RA_PEC, EqPECN[RA_AXIS].value, 2, 3600);
fs_sexa(DEC_PEC, EqPECN[DEC_AXIS].value, 2, 3600);
fs_sexa(RA_TARGET, targetRA, 2, 3600);
fs_sexa(DEC_TARGET, targetDEC, 2, 3600);
if (isDebug() && (dx!=last_dx || dy!=last_dy || ra_guide_dt || dec_guide_dt))
{
last_dx=dx;
last_dy=dy;
IDLog("#########################################\n");
IDLog("dt is %g\n", dt);
IDLog("RA Displacement (%c%s) %s -- %s of target RA %s\n", dx >= 0 ? '+' : '-', RA_DISP, RA_PEC, (EqPECN[RA_AXIS].value - targetRA) > 0 ? "East" : "West", RA_TARGET);
IDLog("DEC Displacement (%c%s) %s -- %s of target RA %s\n", dy >= 0 ? '+' : '-', DEC_DISP, DEC_PEC, (EqPECN[DEC_AXIS].value - targetDEC) > 0 ? "North" : "South", DEC_TARGET);
IDLog("RA Guide Correction (%g) %s -- Direction %s\n", ra_guide_dt, RA_GUIDE, ra_guide_dt > 0 ? "East" : "West");
IDLog("DEC Guide Correction (%g) %s -- Direction %s\n", dec_guide_dt, DEC_GUIDE, dec_guide_dt > 0 ? "North" : "South");
IDLog("#########################################\n");
}
if (ns_guide_dir != -1 || we_guide_dir != -1)
IDSetNumber(EqPECNV, NULL);
break;
default:
break;
}
NewRaDec(currentRA, currentDEC);
return true;
}
bool ScopeSim::Goto(double r,double d)
{
//IDLog("ScopeSim Goto\n");
targetRA=r;
targetDEC=d;
char RAStr[64], DecStr[64];
fs_sexa(RAStr, targetRA, 2, 3600);
fs_sexa(DecStr, targetDEC, 2, 3600);
Parked=false;
TrackState = SCOPE_SLEWING;
EqReqNV->s = IPS_BUSY;
EqNV->s = IPS_BUSY;
IDMessage(deviceName(), "Slewing to RA: %s - DEC: %s", RAStr, DecStr);
return true;
}
bool ScopeSim::Park()
{
targetRA=0;
targetDEC=90;
Parked=true;
TrackState = SCOPE_PARKING;
IDMessage(deviceName(), "Parking telescope in progress...");
return true;
}
bool ScopeSim::ISNewNumber (const char *dev, const char *name, double values[], char *names[], int n)
{
// first check if it's for our device
if(strcmp(dev,deviceName())==0)
{
// This is for our device
// Now lets see if it's something we process here
if(strcmp(name,"TELESCOPE_TIMED_GUIDE_NS")==0)
{
// Unless we're in track mode, we don't obey guide commands.
if (TrackState != SCOPE_TRACKING)
{
GuideNSNP->s = IPS_IDLE;
IDSetNumber(GuideNSNP, NULL);
return true;
}
IUUpdateNumber(GuideNSNP, values, names, n);
return true;
}
if(strcmp(name,"TELESCOPE_TIMED_GUIDE_WE")==0)
{
// Unless we're in track mode, we don't obey guide commands.
if (TrackState != SCOPE_TRACKING)
{
GuideWENP->s = IPS_IDLE;
IDSetNumber(GuideWENP, NULL);
return true;
}
IUUpdateNumber(GuideWENP, values, names, n);
return true;
}
if(strcmp(name,"GUIDE_RATE")==0)
{
IUUpdateNumber(GuideRateNP, values, names, n);
GuideRateNP->s = IPS_OK;
IDSetNumber(GuideRateNP, NULL);
return true;
}
}
// if we didn't process it, continue up the chain, let somebody else
// give it a shot
return INDI::Telescope::ISNewNumber(dev,name,values,names,n);
}
bool ScopeSim::ISNewSwitch (const char *dev, const char *name, ISState *states, char *names[], int n)
{
//IDLog("Enter IsNewSwitch for %s\n",name);
//for(int x=0; x<n; x++) {
// IDLog("Switch %s %d\n",names[x],states[x]);
//}
if(strcmp(dev,deviceName())==0)
{
if(strcmp(name,"PEC_NS")==0)
{
IUUpdateSwitch(PECErrNSSP,states,names,n);
PECErrNSSP->s = IPS_OK;
if (PECErrNSS[MOTION_NORTH].s == ISS_ON)
{
EqPECN[DEC_AXIS].value += SID_RATE * GuideRateN[DEC_AXIS].value;
if (isDebug())
IDLog("$$$$$ Simulating PE in NORTH direction for value of %g $$$$$\n", SID_RATE);
}
else
{
EqPECN[DEC_AXIS].value -= SID_RATE * GuideRateN[DEC_AXIS].value;
if (isDebug())
IDLog("$$$$$ Simulating PE in SOUTH direction for value of %g $$$$$\n", SID_RATE);
}
IUResetSwitch(PECErrNSSP);
IDSetSwitch(PECErrNSSP, NULL);
IDSetNumber(EqPECNV, NULL);
return true;
}
if(strcmp(name,"PEC_WE")==0)
{
IUUpdateSwitch(PECErrWESP,states,names,n);
PECErrWESP->s = IPS_OK;
if (PECErrWES[MOTION_WEST].s == ISS_ON)
{
EqPECN[RA_AXIS].value -= SID_RATE/15. * GuideRateN[RA_AXIS].value;
if (isDebug())
IDLog("$$$$$ Simulator PE in WEST direction for value of %g $$$$$$\n", SID_RATE);
}
else
{
EqPECN[RA_AXIS].value += SID_RATE/15. * GuideRateN[RA_AXIS].value;
if (isDebug())
IDLog("$$$$$$ Simulator PE in EAST direction for value of %g $$$$$$\n", SID_RATE);
}
IUResetSwitch(PECErrWESP);
IDSetSwitch(PECErrWESP, NULL);
IDSetNumber(EqPECNV, NULL);
return true;
}
}
// Nobody has claimed this, so, ignore it
return INDI::Telescope::ISNewSwitch(dev,name,states,names,n);
}
bool ScopeSim::MoveNS(TelescopeMotionNS dir)
{
static int last_motion=-1;
switch (dir)
{
case MOTION_NORTH:
if (last_motion != MOTION_NORTH)
last_motion = MOTION_NORTH;
else
{
IUResetSwitch(MovementNSSP);
MovementNSSP->s = IPS_IDLE;
IDSetSwitch(MovementNSSP, NULL);
}
break;
case MOTION_SOUTH:
if (last_motion != MOTION_SOUTH)
last_motion = MOTION_SOUTH;
else
{
IUResetSwitch(MovementNSSP);
MovementNSSP->s = IPS_IDLE;
IDSetSwitch(MovementNSSP, NULL);
}
break;
}
return true;
}
bool ScopeSim::MoveWE(TelescopeMotionWE dir)
{
static int last_motion=-1;
switch (dir)
{
case MOTION_WEST:
if (last_motion != MOTION_WEST)
last_motion = MOTION_WEST;
else
{
IUResetSwitch(MovementWESP);
MovementWESP->s = IPS_IDLE;
IDSetSwitch(MovementWESP, NULL);
}
break;
case MOTION_EAST:
if (last_motion != MOTION_EAST)
last_motion = MOTION_EAST;
else
{
IUResetSwitch(MovementWESP);
MovementWESP->s = IPS_IDLE;
IDSetSwitch(MovementWESP, NULL);
}
break;
}
return true;
}
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