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| author | Andreas Monzner <andreas.monzner@multimedia-labs.de> | 2005-05-26 10:40:15 +0000 |
|---|---|---|
| committer | Andreas Monzner <andreas.monzner@multimedia-labs.de> | 2005-05-26 10:40:15 +0000 |
| commit | 01921e17fbec0161d4f1578d6648c08e4968f0c4 (patch) | |
| tree | 04901f031770849cf016a90c8d35cc7baf8dcbaa /lib/dvb/sec.cpp | |
| parent | cbe505c09b3491ad80b7703514ddfc3b083249e1 (diff) | |
| download | enigma2-01921e17fbec0161d4f1578d6648c08e4968f0c4.tar.gz enigma2-01921e17fbec0161d4f1578d6648c08e4968f0c4.zip | |
more rotor stuff
Diffstat (limited to 'lib/dvb/sec.cpp')
| -rw-r--r-- | lib/dvb/sec.cpp | 19 |
1 files changed, 17 insertions, 2 deletions
diff --git a/lib/dvb/sec.cpp b/lib/dvb/sec.cpp index edecca90..041d1fbc 100644 --- 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); } |