function set_suspensionA2L( Suspension, Act, FitServo_0dB, Cav)

Servo = containers.Map;
% Servo model
IN1GAIN = mn_CMSgain(-20);
K1IMC_MCL_SERVO_GAIN = -0.1;
Servo('CMS_AOM') = FitServo_0dB('CMS_AOM')*10^(IN1GAIN/20);
Servo('CMS_SUS') = FitServo_0dB('CMS_SUS_analog')*FitServo_0dB('CMS_SUS_digital')*10^(IN1GAIN/20)*K1IMC_MCL_SERVO_GAIN;

OLG_AOM = Servo('CMS_AOM')*Act('AOM')*Cav('Opgain_IMC_1124');
OLG_SUS = Servo('CMS_SUS')*Act('MCEsus')*Cav('Opgain_IMC_1124');

sup = 1/(1+OLG_AOM+OLG_SUS)*Cav('Opgain_IMC_1124')*Servo('CMS_SUS');
sup_5Hz = abs(mnbode_list(sup,4.3,'c'));
sup_1Hz = abs(mnbode_list(sup,1,'c'));
Oplev2MCLout_pitch = 456; %@4.3Hz;
Oplev2MCLout_yaw = 86; %@1Hz



Suspension('P2f_MCE') = Oplev2MCLout_pitch/sup_5Hz;
Suspension('P2f_MCI') = 0;
Suspension('P2f_MCO') = 0;
Suspension('Y2f_MCE') = Oplev2MCLout_yaw/sup_1Hz;
Suspension('Y2f_MCI') = 0;
Suspension('Y2f_MCO') = 0;

end