本文整理汇总了C++中Signal::SetValue方法的典型用法代码示例。如果您正苦于以下问题：C++ Signal::SetValue方法的具体用法？C++ Signal::SetValue怎么用？C++ Signal::SetValue使用的例子？那么, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在类Signal的用法示例。
在下文中一共展示了Signal::SetValue方法的2个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于系统推荐出更棒的C++代码示例。
示例1: Evaluate
//.........这里部分代码省略.........
// 7. Get frequency from transmitter of ground station (participants[0])
Signal* uplinkSignal = gsTransmitter->GetSignal();
Real uplinkFreq = uplinkSignal->GetValue();
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" UpLink signal frequency = %.12lf MHz\n", uplinkFreq);
#endif
// 8. Calculate media correction for uplink leg:
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" Media correction for uplink leg\n");
#endif
Real roundTripTime = ((uplinkRange + downlinkRange)*GmatMathConstants::KM_TO_M/GmatPhysicalConstants::SPEED_OF_LIGHT_VACUUM)/GmatTimeConstants::SECS_PER_DAY;
// DO NOT LEAVE THIS TYPE OF MESSAGE IN THE CODE WITHOUT #ifdef WRAPPERS!!!
//MessageInterface::ShowMessage("Round trip time = %.12lf\n", roundTripTime);
RealArray uplinkCorrection = CalculateMediaCorrection(uplinkFreq, r1, r2, currentMeasurement.epoch - roundTripTime);
Real uplinkRangeCorrection = uplinkCorrection[0]/GmatMathConstants::KM_TO_M;
Real uplinkRealRange = uplinkRange + uplinkRangeCorrection;
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" Uplink range correction = %.12lf km\n",uplinkRangeCorrection);
MessageInterface::ShowMessage(" Uplink real range = %.12lf km\n",uplinkRealRange);
#endif
// 9. Doppler shift the frequency from the transmitter using uplinkRangeRate:
Real uplinkDSFreq = (1 - uplinkRangeRate*GmatMathConstants::KM_TO_M/GmatPhysicalConstants::SPEED_OF_LIGHT_VACUUM)*uplinkFreq;
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" Uplink Doppler shift frequency = %.12lf MHz\n", uplinkDSFreq);
#endif
// 10.Set frequency for the input signal of transponder
Signal* inputSignal = scTransponder->GetSignal(0);
inputSignal->SetValue(uplinkDSFreq);
scTransponder->SetSignal(inputSignal, 0);
// 11. Check the transponder feasibility to receive the input signal:
if (scTransponder->IsFeasible(0) == false)
{
currentMeasurement.isFeasible = false;
currentMeasurement.value[0] = 0;
MessageInterface::ShowMessage("The transponder is unfeasible to receive uplink signal.\n");
throw new GmatBaseException("The transponder is unfeasible to receive uplink signal.\n");
}
// 12. Get frequency of transponder output signal
Signal* outputSignal = scTransponder->GetSignal(1);
Real downlinkFreq = outputSignal->GetValue();
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" Downlink frequency = %.12lf Mhz\n", downlinkFreq);
#endif
// 13. Doppler shift the transponder output frequency by the downlinkRangeRate:
Real downlinkDSFreq = (1 - downlinkRangeRate*GmatMathConstants::KM_TO_M/GmatPhysicalConstants::SPEED_OF_LIGHT_VACUUM)*downlinkFreq;
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" Downlink Doppler shift frequency = %.12lf MHz\n", downlinkDSFreq);
#endif
// 14. Set frequency on receiver
Signal* downlinkSignal = gsReceiver->GetSignal();
downlinkSignal->SetValue(downlinkDSFreq);
// 15. Check the receiver feasibility to receive the downlink signal
if (gsReceiver->IsFeasible() == false)示例2: Evaluate
//.........这里部分代码省略.........
// 7. Get frequency from transmitter of ground station (participants[0])
Signal* uplinkSignal = gsTransmitter->GetSignal();
Real uplinkFreq = uplinkSignal->GetValue();
// 8. Calculate media correction for uplink leg:
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage("6. Media correction for uplink leg\n");
MessageInterface::ShowMessage(" UpLink signal frequency = %.12lf MHz\n", uplinkFreq);
#endif
Real roundTripTime = ((uplinkRange + downlinkRange)*GmatMathConstants::KM_TO_M/GmatPhysicalConstants::SPEED_OF_LIGHT_VACUUM)/GmatTimeConstants::SECS_PER_DAY;
RealArray uplinkCorrection = CalculateMediaCorrection(uplinkFreq, r1, r2, currentMeasurement.epoch - roundTripTime);
Real uplinkRangeCorrection = uplinkCorrection[0]/GmatMathConstants::KM_TO_M;
Real uplinkRealRange = uplinkRange + uplinkRangeCorrection;
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" Uplink range correction = %.12lf km\n",uplinkRangeCorrection);
MessageInterface::ShowMessage(" Uplink real range = %.12lf km\n",uplinkRealRange);
#endif
// 9. Doppler shift the frequency from the transmitter using uplinkRangeRate:
Real uplinkDSFreq = (1 - uplinkRangeRate*GmatMathConstants::KM_TO_M/GmatPhysicalConstants::SPEED_OF_LIGHT_VACUUM)*uplinkFreq;
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage("7. Transponder input and output frequencies\n");
MessageInterface::ShowMessage(" Uplink Doppler shift frequency = %.12lf MHz\n", uplinkDSFreq);
#endif
// 10.Set frequency for the input signal of transponder
Signal* inputSignal = scTransponder->GetSignal(0);
inputSignal->SetValue(uplinkDSFreq);
scTransponder->SetSignal(inputSignal, 0);
// 11. Check the transponder feasibility to receive the input signal:
if (scTransponder->IsFeasible(0) == false)
{
currentMeasurement.isFeasible = false;
currentMeasurement.value[0] = 0;
MessageInterface::ShowMessage("The transponder is unfeasible to receive uplink signal.\n");
throw new GmatBaseException("The transponder is unfeasible to receive uplink signal.\n");
}
// 12. Get frequency of transponder output signal
Signal* outputSignal = scTransponder->GetSignal(1);
Real downlinkFreq = outputSignal->GetValue();
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" Downlink frequency = %.12lf Mhz\n", downlinkFreq);
#endif
// 13. Doppler shift the transponder output frequency by the downlinkRangeRate:
Real downlinkDSFreq = (1 - downlinkRangeRate*GmatMathConstants::KM_TO_M/GmatPhysicalConstants::SPEED_OF_LIGHT_VACUUM)*downlinkFreq;
#ifdef DEBUG_RANGE_CALC_WITH_EVENTS
MessageInterface::ShowMessage(" Downlink Doppler shift frequency = %.12lf MHz\n", downlinkDSFreq);
#endif
// 14. Set frequency on receiver
Signal* downlinkSignal = gsReceiver->GetSignal();