{
m_lnblist.push_back(eDVBSatelliteLNBParameters());
eDVBSatelliteLNBParameters &lnb_ref = m_lnblist.front();
{
m_lnblist.push_back(eDVBSatelliteLNBParameters());
eDVBSatelliteLNBParameters &lnb_ref = m_lnblist.front();
diseqc_ref.m_swap_cmds = false;
diseqc_ref.m_toneburst_param = eDVBSatelliteDiseqcParameters::NO;
diseqc_ref.m_uncommitted_cmd = 0;
diseqc_ref.m_swap_cmds = false;
diseqc_ref.m_toneburst_param = eDVBSatelliteDiseqcParameters::NO;
diseqc_ref.m_uncommitted_cmd = 0;
switch_ref.m_22khz_signal = eDVBSatelliteSwitchParameters::HILO;
switch_ref.m_voltage_mode = eDVBSatelliteSwitchParameters::HV;
switch_ref.m_22khz_signal = eDVBSatelliteSwitchParameters::HILO;
switch_ref.m_voltage_mode = eDVBSatelliteSwitchParameters::HV;
std::map<int, eDVBSatelliteParameters>::iterator sit =
lnb_param.m_satellites.find(sat.orbital_position);
if ( sit != lnb_param.m_satellites.end())
{
std::map<int, eDVBSatelliteParameters>::iterator sit =
lnb_param.m_satellites.find(sat.orbital_position);
if ( sit != lnb_param.m_satellites.end())
{
eDVBSatelliteSwitchParameters &sw_param = sit->second.m_switch_parameters;
eDVBSatelliteRotorParameters &rotor_param = sit->second.m_rotor_parameters;
int hi=0,
eDVBSatelliteSwitchParameters &sw_param = sit->second.m_switch_parameters;
eDVBSatelliteRotorParameters &rotor_param = sit->second.m_rotor_parameters;
int hi=0,
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) );
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) );
- sec_sequence.push_back( eSecCommand(eSecCommand::IF_RUNNING_GOTO, +3 ) );
+ 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) );
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) );
- sec_sequence.push_back( eSecCommand(eSecCommand::IF_STOPPED_GOTO, +3 ) );
+ 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) );
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) );