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Table 4 \(\frac {\mathbb {E}[\text {SNR}_{det}]}{E_{\text {tr}}/N_{0}}\) (dB) and \(\mathbb {E}[\rho _{C}]\) when optimizing rotation angles θ for 2-PAM

From: SNR maximization and modulo loss reduction for Tomlinson-Harashima precoding

 

Terrestrial

Satellite

 

\(\frac {\mathbb {E}[\text {SNR}_{det}]}{E_{\text {tr}}/N_{0}}\) (dB)

\(\mathbb {E}[\rho _{C}]\)

\(\frac {\mathbb {E}[\text {SNR}_{det}]}{E_{\text {tr}}/N_{0}}\) (dB)

\(\mathbb {E}[\rho _{C}]\)

θ=0

1.14

0.62

−4.20

0.8

(SNR,R)RC

1.60

0.79

−3.75

0.91

(MoL,R)RC

1.49

0.84

−4.08

0.95

(MoL+SNR,R)RC

1.52

0.84

−3.81

0.95