{
m_lnblist.push_back(eDVBSatelliteLNBParameters());
eDVBSatelliteLNBParameters &lnb_ref = m_lnblist.front();
+ eDVBSatelliteDiseqcParameters &diseqc_ref = lnb_ref.m_diseqc_parameters;
eDVBSatelliteParameters &astra1 = lnb_ref.m_satellites[192];
- eDVBSatelliteDiseqcParameters &diseqc_ref = astra1.m_diseqc_parameters;
eDVBSatelliteSwitchParameters &switch_ref = astra1.m_switch_parameters;
lnb_ref.m_lof_hi = 10600000;
diseqc_ref.m_swap_cmds = false;
diseqc_ref.m_toneburst_param = eDVBSatelliteDiseqcParameters::NO;
diseqc_ref.m_uncommitted_cmd = 0;
- diseqc_ref.m_use_fast = 1;
+ diseqc_ref.m_use_fast = 0;
switch_ref.m_22khz_signal = eDVBSatelliteSwitchParameters::HILO;
switch_ref.m_voltage_mode = eDVBSatelliteSwitchParameters::HV;
for (;it != m_lnblist.end(); ++it )
{
eDVBSatelliteLNBParameters &lnb_param = *it;
+ eDVBSatelliteDiseqcParameters &di_param = lnb_param.m_diseqc_parameters;
std::map<int, eDVBSatelliteParameters>::iterator sit =
lnb_param.m_satellites.find(sat.orbital_position);
if ( sit != lnb_param.m_satellites.end())
{
- eDVBSatelliteDiseqcParameters &di_param = sit->second.m_diseqc_parameters;
+
eDVBSatelliteSwitchParameters &sw_param = sit->second.m_switch_parameters;
eDVBSatelliteRotorParameters &rotor_param = sit->second.m_rotor_parameters;
int hi=0,
frontend.getData(0, lastcsw);
frontend.getData(1, lastucsw);
frontend.getData(2, lastToneburst);
- frontend.getData(3, lastRotorCmd);
- frontend.getData(4, curRotorPos);
+ frontend.getData(5, lastRotorCmd);
+ frontend.getData(6, curRotorPos);
if ( sat.frequency > lnb_param.m_lof_threshold )
hi = 1;
}
if ( rotor_param.m_inputpower_parameters.m_use )
{ // use measure rotor input power to detect rotor state
+ sec_sequence.push_back( eSecCommand(eSecCommand::SET_VOLTAGE, iDVBFrontend::voltage18) ); // always turn with high voltage
+ sec_sequence.push_back( eSecCommand(eSecCommand::SLEEP, 50) ); // wait 50sec after voltage change
sec_sequence.push_back( eSecCommand(eSecCommand::MEASURE_IDLE_INPUTPOWER) );
sec_sequence.push_back( eSecCommand(eSecCommand::SEND_DISEQC, diseqc) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::SET_TIMEOUT, 8) ); // 2 seconds rotor start timout
+ sec_sequence.push_back( eSecCommand(eSecCommand::SLEEP, 250) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::MEASURE_RUNNING_INPUTPOWER) );
+ eSecCommand::rotor cmd;
+ cmd.direction=1; // check for running rotor
+ cmd.deltaA=rotor_param.m_inputpower_parameters.m_threshold;
+ cmd.steps=+3;
+ cmd.okcount=0;
+ sec_sequence.push_back( eSecCommand(eSecCommand::IF_INPUTPOWER_DELTA_GOTO, cmd ) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::IF_TIMEOUT_GOTO, +8 ) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::GOTO, -4) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::SET_TIMEOUT, 240) ); // 1 minute running timeout
+ sec_sequence.push_back( eSecCommand(eSecCommand::SLEEP, 250) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::MEASURE_RUNNING_INPUTPOWER) );
+ cmd.direction=0; // check for stopped rotor
+ sec_sequence.push_back( eSecCommand(eSecCommand::IF_INPUTPOWER_DELTA_GOTO, cmd ) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::IF_TIMEOUT_GOTO, +2 ) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::GOTO, -4) );
+ sec_sequence.push_back( eSecCommand(eSecCommand::UPDATE_CURRENT_ROTORPARAMS) );
frontend.setData(3, RotorCmd);
frontend.setData(4, sat.orbital_position);
}