X-Git-Url: https://git.cweiske.de/enigma2.git/blobdiff_plain/cbe505c09b3491ad80b7703514ddfc3b083249e1..a81eab44ddc3d7faad43f8434d04f3c55b81b880:/lib/dvb/sec.cpp

diff --git a/lib/dvb/sec.cpp b/lib/dvb/sec.cpp
index edecca90..71a1e460 100644
--- a/lib/dvb/sec.cpp
+++ b/lib/dvb/sec.cpp
@@ -21,8 +21,8 @@ eDVBSatelliteEquipmentControl::eDVBSatelliteEquipmentControl()
 {
 	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;
@@ -36,7 +36,7 @@ eDVBSatelliteEquipmentControl::eDVBSatelliteEquipmentControl()
 	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;
@@ -48,11 +48,12 @@ RESULT eDVBSatelliteEquipmentControl::prepare(iDVBFrontend &frontend, FRONTENDPA
 	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,
@@ -70,8 +71,8 @@ RESULT eDVBSatelliteEquipmentControl::prepare(iDVBFrontend &frontend, FRONTENDPA
 			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;
@@ -325,8 +326,29 @@ RESULT eDVBSatelliteEquipmentControl::prepare(iDVBFrontend &frontend, FRONTENDPA
 						}
 						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);
 						}