Output data

List of the parameters used in IQSTAR:

S-Parameters Data

Refer to S-Parameters Measurements

Table 1. Available S-Parameters data
Name Description Formula Vectorial Scalar
Sij S-parameters of port j to port i Measured by the instrument x
Maximum Gain (dB) Maximum Gain depending on input and output matching (in stable condition) x
|H21| Beta gain of the device if the DUT is a Bipolar transistor |(-2.S21)/ (1-S11(1+S22)+S12 S12)| x

1-Tone Data

Refer to 1-Tone Measurements

Table 2. Available 1-Tone data
Name Description Formula Vectorial Scalar
Index Incident wave at port i x x
Time (s) Measurement time x x
Ai (√W) Incident wave at port i Measured by the instrument x
Bi (√W) Reflected wave at port i Measured by the instrument x
Vi (V) Voltage at port i Measured by the instrument x x
Ii (A) Current at port i Measured by the instrument x x
Praw (dBm) Power applied to RF source Measured by the instrument x x
Pin available (dBm) Total power available from the sources at the DUT input plane Measured by the instrument or Pin_del/1-|((Zin-Zsource)/(Zin+Zsource))|² x x
Pin delivered (dBm) Total power delivered to the DUT at the DUT input plane Measured by the instrument or ½ |a1|².(1-|Γin|²) x x(2)
Pout (dBm) Total power delivered to the load at the DUT output plane. Measured by the instrument or ½ |b2|².(1-|Γload|²) x x
Pdc (dBm) Total DC power consumed by the DUT Default : (Vin.Iin)+(Vout.Iout) Could be modified see Consumed Power Expression x x
Pdiss (dBm) Total power dissipated by the DUT 10*log10((Pdc(W) +P in delivered(W))-P out (W))+30 x x(2)
Gt (dB) Transducer gain from the DUT input plane to the DUT output plane 10.log(Pout (W)/ Pin_available (W)) x x
Gp (dB) Power gain from the DUT input plane to the DUT output plane 10.log(Pout(W)/ Pin_delivered (W)) x x(2)
Gt Compression (Max) (dB) Compression transducer gain with respect to the linear gain Gt max value-Gt measured x x
Gt Compression (Linear) (dB) Compression transducer gain with respect to the maximum gain Gt linear value-Gt measured x x
Gp Compression (Max) (dB) Compression power gain with respect to the linear gain Gp max value-Gp measured x x(2)
Gp Compression (Linear) (dB) Compression power gain with respect to the linear gain Gp linear value-Gp measured x x(2)
Transducer (%) Efficiency Transducer Efficiency, efficiency calculated using “Pin_available (Pout (W)- Pin_available(W))/ Pdc (W) *100 x x
Drain Efficiency (%) Drain Efficiency is the efficiency on the output side Pout (W) / Pdc (W) *100 x x
PAE (%) PAE, efficiency calculated using “Pin_delivered” (Pout (W)- Pin_delivered (W))/ Pdc (W) *100 x x(2)
Gamma Load Reflection coefficient presented at the output DUT reference plane b2/a2 x(1)
Gamma Source Reflection coefficient presented at the input DUT reference plane 0 x
Gamma In Reflection coefficient presented by the input of the DUT b1/a1 x
Zload (Ω) Impedance presented at the output DUT reference plane Z0.(1+Γload/1-Γload) x(1)
Zsource (Ω) Impedance presented at the input DUT reference plane by the source 50 ohms x
Zin (Ω) Impedance presented by the input of the DUT Z0.(1+Γin/1-Γin) x
AM/PM (°) Phase Wave ratio between the device input and output angle(B2/A1) x
AM/PM (Normalized) (°) Normalized phase wave ratio between the maximum and the minimum phase shift max(AMPM)-min(AMPM) x
Offset AM/PM Relative phase wave ratio shifts between the device input and output (AMPM)-first(AMPM) x
Input Return Loss Input return loss between the DUT and the source impedance Zsource insource*|/|1-(Γinsource| or 10*log10(Preflect(W)/Pin_available(W))+30 x x(2)
Frequency (GHz) Frequency Measured by the instrument x x
Hi (dBc) Power difference between Pout at i.f0 and Pout at f0 Pouti(dBm) - Pout1(dBm) x
Spurious i [Frequency] (GHz) Frequency of the spurious number i Measured by the instrument x x
Spurious i [Power] (dBm) Power level of the spurious number i Measured by the instrument x x
Tmonitor (°C) Temperature measure by monitor from Thermal Station Measured by the instrument x x
Tsensor n (°C) Temperature measure by sensor n from Thermal Station Measured by the instrument x x
Psensor n (Pa) Pressure measure by sensor n from Thermal Station Measured by the instrument x x
Ppm n (dBm) Power level measure by power meter n from Power Meter Matrix Measured by the instrument x x

(1) using Full 2-Ports Calibration

(2) using three power sensors

Table 3. Spectrum sub-trace: available data
Name Description Formula Level Span Zero-span
Index Index values Spectrum x x
Frequency (GHz) Frequency values Measured by the instrument Spectrum x
Normalized frequency (GHz) Frequency values -(span / 2.0) to (span / 2.0) Spectrum x
Time (s) Time values Measured by the instrument Spectrum x
Raw power (dBm) Measured powers Measured by the instrument Spectrum x x
Table 4. Spurious sub-trace: available data
Name Description Formula Level
Index Index values Spurious
Frequency (GHz) Frequency values Measured by the instrument Spurious
Raw power (dBm) Measured powers Measured by the instrument Spurious
Detection Threshold (dBm) Detection SpuriousThreshold Defined by user Spurious
Noise floor (dBm) Noise floor Measured by the instrument when DUT is not bias and RF is OFF Spurious
Table 5. IV Trace Screenshot sub-trace: available data
Name Description Formula Level
Index Index values Default
Time Time values Default
Vi Voltage at port i Measured by the instrument Default
Ii Current at port i Measured by the instrument Default

Related Information:

2-Tones Data

Refer to 2-Tones Measurements

Table 6. Available 2-Tones data
Name Description Formula Vectorial Scalar
Index Index values x x
Time (s) Measurement time x x
Ai (√W) Incident wave at port i Measured by the instrument x
Bi (√W) Reflected wave at port i Measured by the instrument x
Vi (V) Voltage at port i Measured by the instrument x
Ii (A) Current at port i Measured by the instrument x
Praw @fn (dBm) Power applied to RF source for frequency n Measured by the instrument x x
Pin available Total (dBm) Total power available from the sources at the DUT input plane Pin available @f1 (W) + Pin available @f2 (W) x x(3)
Pin available @fn (dBm) Power available from the sources at the DUT input plane for frequency n Measured by the instrument @fn x x(3)
Pin delivered Total (dBm) Total power delivered to the DUT at the DUT input plane Pin delivered @f1 (W) + Pin delivered @f2 (W) x x(2)(3)
Pin delivered @fn (dBm) Power delivered to the DUT at the DUT input plane for frequency n Pin delivered @n (W) x x(2)(3)
Pout Total (dBm) Total power delivered to the load at the DUT output plane. Pout@f1 (W) + Pout@f2 (W) x x(3)
Pout @fn (dBm) Power delivered to the load at the DUT output plane at frequency n. Pout@fn (W) x x(3)
Pdc (dBm) Total DC power consumed by the DUT Default : (Vin.Iin)+(Vout.Iout) Could be modified see Consumed Power Expression x x(3)
Pdiss (dBm) Total power dissipated by the DUT 10*log10((Pdc(W) +P in delivered(W))-P out (W))+30 x x
Gt Total (dB) Total transducer gain from the DUT input plane to the DUT output plane 10.log(Pout Total (W)/ Pin_available Total (W)) x x(3)
Gt @fn (dB) Transducer gain from the DUT input plane to the DUT output plane for frequency n 10.log(Pout@fn (W)/ Pin_available@fn (W)) x x(3)
Gp Total (dB) Total power gain from the DUT input plane to the DUT output plane 10.log(Pout Total(W)/ Pin_delivered Total (W)) x x
Gp @fn (dB) Power gain from the DUT input plane to the DUT output plane for frequency n 10.log(Pout @fn(W)/ Pin_delivered @fn (W)) x x
Gx Total Compression (Max) (dB) Total compression gain refer to the linear gain Gx Total max value-Gx Total measured x x(3)
Gx @fn Compression (Max) (dB) Compression gain refer to the linear gain for frequency n Gx @fn max value-Gx @fn measured x x(3)
Gx Total Compression (Linear) (dB) Total compression gain refer to the maximum gain Gx Total linear value-Gx Total measured x x(3)
Gx @fn Compression (Linear) (dB) Compression gain refer to the maximum gain for frequency n Gx @fn linear value-Gx @fn measured x x(3)
Transducer (%) Efficiency Transducer Efficiency, efficiency calculated using “Pin_available (Pout (W)- Pin_available (W))/ Pdc (W) *100 x x(3)
Drain Efficiency (%) Drain Efficiency is the efficiency on the output side Pout (W) / Pdc (W) *100 x x(3)
PAE (%) PAE, efficiency calculated using “Pin_delivered” (Pout (W)- Pin_delivered (W))/ Pdc (W) *100 x(2)(3)
Gamma Load Reflection coefficient presented at the output DUT reference plane b2/a2 x(1)
Gamma Source Reflection coefficient presented at the input DUT reference plane 0 x
Gamma In Reflection coefficient presented by the input of the DUT b1/a1 x
Zload (Ω) Impedance presented at the output DUT reference plane Z0.(1+Γload/1-Γload) x(1)
Zsource (Ω) Impedance presented at the input DUT reference plane by the source 50 ohms x
Zin (Ω) Impedance presented by the input of the DUT Z0.(1+Γin/1-Γin) x
AM/PM (°) Phase Wave ratio between the device input and output angle(B2/A1) x
AM/PM (Normalized) (°) Normalized phase wave ratio between the maximum and the minimum phase shift max(AMPM)-min(AMPM) x
Offset AM/PM (°) Relative phase wave ratio shifts between the device input and output (AMPM)-first(AMPM) x
Input Return Loss (dB) Input return loss between the DUT and the source impedance Zsource insource*|/|1-(Γinsource| or 10*log10(Preflect(W)/Pin_available(W))+30 x x(2)(3)
Frequency (GHz) Frequency x x(3)
I3 (Lower/Upper) (dBm) Intermodulation power (of lower or upper side) of the third order (@2f1 -f2) delivered to the load at the DUT output plane. Power measured @2f1 -f2 (lower) or @2f2 -f1 (upper) x
I5 (Lower/Upper) (dBm) Intermodulation power(of lower or upper side) of the fifth order (@3f1 -2f2) delivered to the load at the DUT output plane. Power measured @3f1-2f2 (lower) or @3f2 -2f1 (upper) x
I7 (Lower/Upper) (dBm) Intermodulation power(of lower or upper side) of the seventh order (@4f1 -3f2) delivered to the load at the DUT output plane. Power measured @4f1-3f2 (lower) or @4f2 -3f1 (upper) x
I9 (Lower/Upper) (dBm) Intermodulation power(of lower or upper side) of the ninth order (@5f1 -4f2) delivered to the load at the DUT output plane. Power measured @5f1-4f2 (lower) or @5f2 -4f1 (upper) x
C/Ij (Total) (dBc) Total Carrier to Total jth Order Intermodulation Ratio dBm((Pout Total (W))/ (Ij lower (W)+Ij upper(W)) x x(3)
C/Ij (Lower) (dBc) Lower Carrier to lower jth Order Intermodulation Ratio dBm((Pout lower (W))/ (Ij lower (W)) x x(3)
C/Ij (Upper) (dBc) Upper Carrier to Upper jth Order Intermodulation Ratio dBm((Pout Upper (W))/ (Ij upper (W)) x x(3)
OIPj (Total) (dBm) Total jth Order Intercept Point [dBm(Pout@f 1 (W)+Pout@f 2 (W))+C/I j total/2] -3 x
OIPj (Lower) (dBm) Lower side of the jth Order Intercept Point dBm[(Pout@f 1 (W)+(C/I j lower)/2 ] x
OIPj (Upper) (dBm) Upper side of the jth Order Intercept Point dBm[(Pout@f 2 (W))+(C/I j upper)/2 ] x
IIPj (Total) (dBm) Total input jth Order Intercept Point [dBm(Pin available@f 1 (W)+Pin available@f 2 (W))+C/I j total/2] -3 x
IIPj (Lower) (dBm) Lower side of the input jth Order Intercept Point dBm[(Pin available@f 1 (W)+(C/I j lower)/2 ] x
IIPj (Upper) (dBm) Upper side of the input jth Order Intercept Point dBm[(Pavailable@f 2 (W))+(C/I j upper)/2 ] x
IIPjmin (Total) (dBm) Minimum Total Input 3rd Order Intercept Point [dBm(Pin_ delivered@f1(W)+ Pin_ delivered@f2 (W))+C/I j total/2] - 3 x
IIPjmin (Lower) (dBm) Minimum Lower Input 3rd Order Intercept Point dBm(Pin_ delivered@f1(W)+C/I j lower/2) x
IIPjmin (Upper) (dBm) Minimum Upper Input 3rd Order Intercept Point dBm(Pin_ delivered@f2(W)+C/I j upper/2) x
Tmonitor (°C) Temperature measure by monitor from Thermal Station Measured by the instrument x x
Tsensor n (°C) Temperature measure by sensor n from Thermal Station Measured by the instrument x x
Psensor n (Pa) Pressure measure by sensor n from Thermal Station Measured by the instrument x x
Ppm n (dBm) Power level measure by power meter n from Power Meter Matrix Measured by the instrument x x

(1) using Full 2-Ports Calibration

(2) using three power sensors

(3) using Vector Signal Analyzer

3-Tones Data

Refer to 3-Tones Measurements

Table 7. Available 3-Tones data
Name Description Formula Vectorial Scalar
Index Index values x
Time (s) Measurement time x
Ai (√W) Incident wave at port i Measured by the instrument x
Bi (√W) Reflected wave at port i Measured by the instrument x
Vi (V) Voltage at port i Measured by the instrument x
Ii (A) Current at port i Measured by the instrument x
Praw (dBm) Power applied to RF source Measured by the instrument x x
Pin available (dBm) Total power available from the sources at the DUT input plane Measured by the instrument or Pin_del/1-|((Zin-Zsource)/(Zin-Zsource))|² x
P in delivered (dBm) Total power delivered to the DUT at the DUT input plane Measured by the instrument or ½ |a1|².(1-|Γin|²) x
P out (dBm) Total power delivered to the load at the DUT output plane. Measured by the instrument or ½ |b2|².(1-|Γload|²) x
Pdc (dBm) Total DC power consumed by the DUT Default : (Vin.Iin)+(Vout.Iout) Could be modified see Consumed Power Expression x
Pdiss (dBm) Total power dissipated by the DUT 10*log10((Pdc(W) +P in delivered(W))-P out (W))+30 x
Gt (dB) Transducer gain from the DUT input plane to the DUT output plane 10.log(Pout (W)/ Pin_available (W)) x
Gp (dB) Power gain from the DUT input plane to the DUT output plane 10.log(Pout(W)/ Pin_delivered (W)) x
Gt Compression (Max) (dB) Compression transducer gain with respect to the linear gain Gt max value-Gt measured x
Gt Compression (Linear) (dB) Compression transducer gain with respect to the maximum gain Gt linear value-Gt measured x
Gp Compression (Max) (dB) Compression power gain with respect to the linear gain Gp max value-Gp measured x
Gp Compression (Linear) (dB) Compression power gain with respect to the linear gain Gp linear value-Gp measured x
Transducer (%) Efficiency Transducer Efficiency, efficiency calculated using “Pin_available (Pout (W)- Pin_available(W))/ Pdc (W) *100 x
Drain Efficiency (%) Drain Efficiency is the efficiency on the output side Pout (W) / Pdc (W) *100 x
PAE (%) PAE, efficiency calculated using “Pin_delivered” (Pout (W)- Pin_delivered (W))/ Pdc (W) *100 x
Gamma Load Reflection coefficient presented at the output DUT reference plane b2/a2 x
Gamma Source Reflection coefficient presented at the input DUT reference plane 0 x
Gamma In Reflection coefficient presented by the input of the DUT b1/a1 x
Zload (Ω) Impedance presented at the output DUT reference plane Z0.(1+Γload/1-Γload) x
Zsource (Ω) Impedance presented at the input DUT reference plane by the source 50 ohms x
Zin (Ω) Impedance presented by the input of the DUT Z0.(1+Γin/1-Γin) x
AM/PM (°) Phase Wave ratio between the device input and output angle(B2/A1) x
AM/PM (Normalized) (°) Normalized phase wave ratio between the maximum and the minimum phase shift max(AMPM)-min(AMPM) x
Offset AM/PM Relative phase wave ratio shifts between the device input and output (AMPM)-first(AMPM) x
Input Return Loss Input return loss between the DUT and the source impedance Zsource insource*|/|1-(Γinsource| or 10*log10(Preflect(W)/Pin_available(W))+30 x
Frequency (GHz) Frequency Measured by the instrument x
Delta (Hz) Frequency delta between the carrier and the left or right tone Measured by the instrument x
Phase Initial phase of the three tones signal Measured by the instrument x
Tmonitor (°C) Temperature measure by monitor from Thermal Station Measured by the instrument x
Tsensor n (°C) Temperature measure by sensor n from Thermal Station Measured by the instrument x
Psensor n (Pa) Pressure measure by sensor n from Thermal Station Measured by the instrument x
Ppm n (dBm) Power level measure by power meter n from Power Meter Matrix Measured by the instrument x

Related Information:

Video Bandwidth Data

Refer to Video Bandwidth (VBW) Measurements

During video bandwidth measurement all the output data are similar to 2-Tones data, even if IQSTAR don't display all the data they are recorded in the output file.

Table 8. Available Video Bandwidth data
Name Description Formula Vectorial Scalar
C/Ij (Lower) (dBc) Lower Carrier to lower jth Order Intermodulation Ratio dBm((Pout lower (W))/ (Ij lower (W)) x x(3)
C/Ij (Upper) (dBc) Upper Carrier to Upper jth Order Intermodulation Ratio dBm((Pout Upper (W))/ (Ij upper (W)) x x(3)

(3) using Vector Signal Analyzer

Modulated Data

Refer to Modulation Measurements

Table 9. Available Modulated data
Name Description Formula Vectorial Scalar
Index Index values x
Time (s) Measurement time x
Ii (A) Current at port i Measured by the instrument x
Vi (V) Voltage at port i Measured by the instrument x
ACPRi lower (dBc) Adjacent Channel Power Ratio, so it's the ratio between carrier and ith adjacent channel on the lower frequency side Measured by the instrument x
ACPRi upper (dBc) Adjacent Channel Power Ratio, so it's the ratio between carrier and ith adjacent channel on the upper frequency side Measured by the instrument x
EVM ReferenceRMS Root-Mean-Square of the Error vector magnitude Reference Measured by the instrument x
EVM ReferenceRMS with DPD Root-Mean-Square of the Error vector magnitude Reference with a Digital Pre-distortion Measured by the instrument x
EVM Referencepeak Peak value of the Error vector magnitude Reference Measured by the instrument x
EVM Referencepeak with DPD Peak value of the Error vector magnitude Reference with a Digital Pre-distortion Measured by the instrument x
MER RMS Root-Mean-Square of the Modulation Error Ratio Measured by the instrument x
MER RMS with DPD Root-Mean-Square of the Modulation Error Ratio with a Digital Pre-distortion Measured by the instrument x
MER peak Peak value of the Modulation Error Ratio Measured by the instrument x
MER peak with DPD Peak value of the Modulation Error Ratio with a Digital Pre-distortion Measured by the instrument x
Magnitude error RMS Root-Mean-Square of the magnitude error Measured by the instrument x
Magnitude error RMS with DPD Root-Mean-Square of the magnitude error with a Digital Pre-distortion Measured by the instrument x
Magnitude error peak Peak value of the magnitude error Measured by the instrument x
Magnitude error peak with DPD Peak value of the magnitude error with a Digital Pre-distortion Measured by the instrument x
PAPR Peak to Average Power Ratio Measured by the instrument x
Phase error RMS Root-Mean-Square of the phase error Measured by the instrument x
Phase error RMS with DPD Root-Mean-Square of the phase error with a Digital Pre-distortion Measured by the instrument x
Phase error peak Peak value of the phase error Measured by the instrument x
Phase error peak with DPD Peak value of the phase error with a Digital Pre-distortion Measured by the instrument x
Praw (dBm) Power applied to RF source Measured by the instrument x
Pin available (dBm) Total input power available from the drive sources at the DUT plane Measured by the instrument x
Pin available PEAK (dBm) Total PEAK input power available from the drive sources at the DUT plane Pin available AVG (dBm) + PAPRreference(dB) x
P in delivered (dBm) Total power delivered to the DUT at the DUT input plane Measured by the instrument x(2)
Pout (dBm) Total power delivered to the load at the DUT output plane. Measured by the instrument x
Pout PEAK (dBm) Total PEAK power delivered to the load at the DUT output plane. Pout AVG (dBm) + PAPRout(dB) x
Pdc (dBm) Total DC power consumed by the DUT Default : (Vin.Iin)+(Vout.Iout) Could be modified see Consumed Power Expression x
Pdiss (dBm) Total power dissipated by the DUT 10*log10((Pdc(W) +P in delivered(W))-P out (W))+30 x(2)
Gt (dB) Transducer gain from the DUT input plane to the DUT output plane 10.log(Pout (W)/ Pin_available (W)) x
Gt PEAK (dB) Transducer gain PEAK from the DUT input plane to the DUT output plane 10.log(Pout PEAK (W)/ Pin_available PEAK (W)) x
Gp (dB) Power gain from the DUT input plane to the DUT output plane 10.log(Pout(W)/ Pin_delivered (W)) x(2)
Gt Compression (Max) (dB) Compression transducer gain refer to the linear gain Gt max value-Gt measured x
Gt PEAK Compression (Max) (dB) Compression transducer gain PEAK refer to the linear gain Gt PEAK max value-Gt PEAK measured x
Gp Compression (Max) (dB) Compression power gain with respect to the linear gain Gp max value-Gp measured x(2)
Gt Compression (Linear) (dB) Compression transducer gain refer to the maximum gain Gt linear value-Gt measured x
Gt PEAK Compression (Linear) (dB) Compression transducer gain PEAK refer to the maximum gain Gt PEAK linear value-Gt PEAK measured x
Gp Compression (Max) (dB) Compression power gain with respect to the linear gain Gp max value-Gp measured x(2)
Transducer (%) Efficiency Transducer Efficiency, efficiency calculated using “Pin_available (Pout (W)- Pin_available (W))/ Pdc (W) *100 x
Drain Efficiency (%) Drain Efficiency is the efficiency on the output side Pout (W) / Pdc (W) *100 x
PAE (%) PAE, efficiency calculated using “Pin_delivered” (Pout (W)- Pin_delivered (W))/ Pdc (W) *100 x(2)
Input Return Loss Input return loss between the DUT and the source impedance Zsource 10*log10(Preflect(W)/Pin_available(W))+30 x(2)
Tmonitor (°C) Temperature measure by monitor from Thermal Station Measured by the instrument x
Tsensor n (°C) Temperature measure by sensor n from Thermal Station Measured by the instrument x
Psensor n (Pa) Pressure measure by sensor n from Thermal Station Measured by the instrument x
Ppm n (dBm) Power level measure by power meter n from Power Meter Matrix Measured by the instrument x

(2) using three power sensors

Table 10. Spectrum sub-trace: available data
Name Description Formula Level Span Zero-span
Index Index values Spectrum x x
Frequency (GHz) Frequency values Measured by the instrument Spectrum x
Normalized frequency (GHz) Frequency values -(span / 2.0) to (span / 2.0) Spectrum x
Time (s) Time values Measured by the instrument Spectrum x
Raw power (dBm) Measured powers Measured by the instrument Spectrum x x
Table 11. CCDF sub-trace: available data
Name Description Formula Level
Index Index values CCDF
PAP (dB) Peak to Average Power Measured by the instrument CCDF
Probability (%) Probability values Measured by the instrument CCDF

Related Information:

I/Q Data

Refer to I/Q Measurements

Table 12. Available I/Q data
Name Description Formula Vectorial Scalar
Index Index values x
Time (s) Measurement time x
Ii (A) Current at port i Measured by the instrument x
Vi (V) Voltage at port i Measured by the instrument x
ACPRi lower or iupper (dBc) Adjacent Channel Power Ratio, so it's the ratio between carrier and ith adjacent channel on the lower or upper frequency side Pi lower or iupper(dBm)-Pcarrier(dBm) x
EVM AverageRMS Root-Mean-Square of the Error vector magnitude Normalized on Average Power

x
EVM Averagepeak Peak value of the Error vector magnitude Normalized on Average Power

x
EVM ReferenceRMS Root-Mean-Square of the Error vector magnitude Reference Normalized on Reference Power

x
EVM Referencepeak Peak value of the Error vector magnitude Reference Normalized on Reference Power

x
EVM PeakRMS Root-Mean-Square of the Error vector magnitude Normalized on Peak Power

x
EVM Peakpeak Peak value of the Error vector magnitude Normalized on Peak Power

x
MER RMS Root-Mean-Square of the Modulation Error Ratio

x
MER peak Peak value of the Modulation Error Ratio

x
PAPR Peak to Average Power Ratio Max(Pout (dBm))-Mean(Pout (dBm)) x
Praw (dBm) Power applied to RF source Measured by the instrument x
Pin available (dBm) Total power available from the drive sources at the DUT plane Measured by the instrument x
Pin available PEAK (dBm) Peak power available from the drive sources at the DUT plane Pin available AVG (dBm) + PAPRreference(dB) x
P in delivered (dBm) Total power delivered to the DUT at the DUT input plane Measured by the instrument x(2)
Pout (dBm) Total power delivered to the load at the DUT output plane. Measured by the instrument x
Pout PEAK (dBm) Peak power delivered to the load at the DUT output plane. Pout AVG (dBm) + PAPRout(dB) x
Pdc (dBm) Total DC power consumed by the DUT Default : (Vin.Iin)+(Vout.Iout) Could be modified see Consumed Power Expression x
Pdiss (dBm) Total power dissipated by the DUT 10*log10((Pdc(W) +P in delivered(W))-P out (W))+30 x(2)
Gt (dB) Transducer gain from the DUT input plane to the DUT output plane 10.log(Pout (W)/ Pin_available (W)) x
Gt PEAK (dB) Transducer gain PEAK from the DUT input plane to the DUT output plane 10.log(Pout PEAK (W)/ Pin_available PEAK (W)) x
Gp (dB) Power gain from the DUT input plane to the DUT output plane 10.log(Pout(W)/ Pin_delivered (W)) x(2)
Gt Compression (Max) (dB) Compression transducer gain refer to the linear gain Gt max value-Gt measured x
Gt PEAK Compression (Max) (dB) Compression transducer gain PEAK refer to the linear gain Gt PEAK max value-Gt PEAK measured x
Gp Compression (Max) (dB) Compression power gain with respect to the linear gain Gp max value-Gp measured x(2)
Gt Compression (Linear) (dB) Compression transducer gain refer to the maximum gain Gt linear value-Gt measured x
Gt PEAK Compression (Linear) (dB) Compression transducer gain PEAK refer to the maximum gain Gt PEAK linear value-Gt PEAK measured x
Gp Compression (Max) (dB) Compression power gain with respect to the linear gain Gp max value-Gp measured x(2)
Transducer (%) Efficiency Transducer Efficiency, efficiency calculated using “Pin_available (Pout (W)- Pin_available (W))/ Pdc (W) *100 x
Drain Efficiency (%) Drain Efficiency is the efficiency on the output side Pout (W) / Pdc (W) *100 x
PAE (%) PAE, efficiency calculated using “Pin_delivered” (Pout (W)- Pin_delivered (W))/ Pdc (W) *100 x(2)
Input Return Loss Input return loss between the DUT and the source impedance Zsource 10*log10(Preflect(W)/Pin_available(W))+30 x(2)
Tmonitor (°C) Temperature measure by monitor from Thermal Station Measured by the instrument x
Tsensor n (°C) Temperature measure by sensor n from Thermal Station Measured by the instrument x
Psensor n (Pa) Pressure measure by sensor n from Thermal Station Measured by the instrument x
Ppm n (dBm) Power level measure by power meter n from Power Meter Matrix Measured by the instrument x

(2) using three power sensors

Table 13. I/Q sub-trace: available data
Name Description Formula Level Reference Waveform Measured Waveform DPD Waveform
Index Index values All x x x
Time (s) Waveform duration Measured by the instrument I/Q; EVM x x x
I (V) I values Measured by the instrument I/Q x x x
Q (V) Q values Measured by the instrument I/Q x x x
Abs(envelope) (V) Abs(envelope) i2+q2 I/Q x x x
Phase(envelope) (°) Phase(envelope) atan2(i,q) I/Q x x x
Mag(envelope) (dBm) Magnitude(envelope) 10log10(i2+q2) I/Q x
Constellation Reference constellation values (only unique values) (1) Computed using waveform information Constellation x
Demodulated constellation (1) Measured I/Q demodulated Computed based on measured waveform using reference waveform information Constellation x x
Normalized frequency (GHz) Frequency values -(sampling rate / 2.0) to (sampling rate / 2.0) Spectrum x x x
Raw power (dBm) Raw power levels Spectrum x x x
Normalized raw power (dBm) Raw power levels normalized to 0 Spectrum x x x
PAP (dB) Peak to Average Power Linear step (0 to PAPR maximum) CCDF x x x
Probability (%) Probability values 10log10(env(PAPR) - env(mean(PAPR)) CCDF x x x
Pin Available (dBm) I/Q values corrected by measure Pin Available power AM/AM; AM/PM x x
Pout (dBm) I/Q values corrected by measure Pout power AM/AM; AM/PM x x
AM/AM (dB) Instantaneous gain conversion AM/AM x x
AM/PM (°) Instantaneous phase conversion AM/PM x x
Symbol (1) Symbol values Measured by the instrument EVM x x x
EVM Average [On Signal] EVM RMS sample per sample in function of time EVM x x x
EVM Peak [On Signal] EVM Peak sample per sample in function of time EVM x x x
EVM Average [On Symbol Carrier n] (1) EVM RMS symbol per symbol in function of time (n = 1 to 10) EVM x x x
EVM Peak [On Symbol Carrier n] (1) EVM Peak symbol per symbol in function of time (n = 1 to 10) EVM x x x

(1) only available if reference waveform is a PSK/QAM/LTE/NR5G

Related Information:

NPR

Refer to NPR Measurements

Table 14. Available NPR data
Name Description Formula Vectorial Scalar
Index Index values x
Time (s) Measurement time x
Ii (A) Current at port i Measured by the instrument x
Vi (V) Voltage at port i Measured by the instrument x
NPRx Ai (dBc) Noise Power Ratio, so it's the ratio between carrier and xth notch for incident wave at port i Px notch(dBm)-Pcarrier(dBm) x
NPRx Bi (dBc) Noise Power Ratio, so it's the ratio between carrier and xth notch for reflected wave at port i Px notch(dBm)-Pcarrier(dBm) x
ACPRi lower or iupper (dBc) Adjacent Channel Power Ratio, so it's the ratio between carrier and ith adjacent channel on the lower or upper frequency side Pi lower or iupper(dBm)-Pcarrier(dBm) x
Praw (dBm) Power applied to RF source Measured by the instrument x
Pin available (dBm) Total power available from the drive sources at the DUT plane Measured by the instrument x
P in delivered (dBm) Total power delivered to the DUT at the DUT input plane Measured by the instrument x
Pout (dBm) Total power delivered to the load at the DUT output plane. Measured by the instrument x
Pdc (dBm) Total DC power consumed by the DUT Default : (Vin.Iin)+(Vout.Iout) Could be modified see Consumed Power Expression x
Pdiss (dBm) Total power dissipated by the DUT 10*log10((Pdc(W) +P in delivered(W))-P out (W))+30 x
Gt (dB) Transducer gain from the DUT input plane to the DUT output plane 10.log(Pout (W)/ Pin_available (W)) x
Gp (dB) Power gain from the DUT input plane to the DUT output plane 10.log(Pout(W)/ Pin_delivered (W)) x
Gt Compression (Max) (dB) Compression transducer gain refer to the linear gain Gt max value-Gt measured x
Gp Compression (Max) (dB) Compression power gain with respect to the linear gain Gp max value-Gp measured x
Gt Compression (Linear) (dB) Compression transducer gain refer to the maximum gain Gt linear value-Gt measured x
Gp Compression (Max) (dB) Compression power gain with respect to the linear gain Gp max value-Gp measured x
Transducer (%) Efficiency Transducer Efficiency, efficiency calculated using “Pin_available (Pout (W)- Pin_available (W))/ Pdc (W) *100 x
Drain Efficiency (%) Drain Efficiency is the efficiency on the output side Pout (W) / Pdc (W) *100 x
PAE (%) PAE, efficiency calculated using “Pin_delivered” (Pout (W)- Pin_delivered (W))/ Pdc (W) *100 x
Gamma Load Reflection coefficient presented at the output DUT reference plane b2/a2 x(1)
Gamma Source Reflection coefficient presented at the input DUT reference plane 0 x
Gamma In Reflection coefficient presented by the input of the DUT b1/a1 x
Zload (Ω) Impedance presented at the output DUT reference plane Z0.(1+Γload/1-Γload) x(1)
Zsource (Ω) Impedance presented at the input DUT reference plane by the source 50 ohms x
Zin (Ω) Impedance presented by the input of the DUT Z0.(1+Γin/1-Γin) x
AM/PM (°) Phase Wave ratio between the device input and output angle(B2/A1) x
AM/PM (Normalized) (°) Normalized phase wave ratio between the maximum and the minimum phase shift max(AMPM)-min(AMPM) x
Offset AM/PM Relative phase wave ratio shifts between the device input and output (AMPM)-first(AMPM) x
Input Return Loss Input return loss between the DUT and the source impedance Zsource insource*|/|1-(Γinsource| or 10*log10(Preflect(W)/Pin_available(W))+30 x
Tmonitor (°C) Temperature measure by monitor from Thermal Station Measured by the instrument x
Tsensor n (°C) Temperature measure by sensor n from Thermal Station Measured by the instrument x
Psensor n (Pa) Pressure measure by sensor n from Thermal Station Measured by the instrument x
Ppm n (dBm) Power level measure by power meter n from Power Meter Matrix Measured by the instrument x

(1) using Full 2-Ports Calibration

Table 15. NPR sub-traces: available data
Name Description Formula Level
Index Index values All
Normalized frequency (GHz) Frequency values -(span / 2.0) to (span / 2.0) All
Spectrum A1 Available A1 spectrum Measured by the instrument A1
Spectrum B1 Available B1 spectrum Measured by the instrument B1
Spectrum A2 Available A2 spectrum Measured by the instrument A2
Spectrum B2 Available B2 spectrum Measured by the instrument B2