more rotor stuff

[enigma2.git] / lib / dvb / sec.cpp

diff --git a/lib/dvb/sec.cpp b/lib/dvb/sec.cpp
index edecca902fa12bc779d4d9a8703514cbc6e32cf7..041d1fbcde19c88c65e4b8b212037a524121ded0 100644 (file)
--- a/lib/dvb/sec.cpp
+++ b/lib/dvb/sec.cpp
@@ -70,8 +70,8 @@ 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 +325,23 @@ 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) );
+                                                       sec_sequence.push_back( eSecCommand(eSecCommand::IF_RUNNING_GOTO, +3 ) );
+                                                       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 ) );
+                                                       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);
                                                }