== cmdfile.20 ==
    $GLIDE_SLOPE,30
    $D_TGT,45
    $T_DIVE,15
    $T_MISSION,20
    $C_VBD,2275
    $SM_CC,250
    $MAX_BUOY,300
    $C_PITCH,2750
    $PITCH_GAIN,15
    $C_ROLL_DIVE,1950
    $C_ROLL_CLIMB,1880
    $ROLL_DEG,50
    $ALTIM_PING_DEPTH,100
    $ALTIM_PING_DELTA,5
    $ALTIM_SENSITIVITY,3
    $ALTIM_PULSE,3
    $ALTIM_BOTTOM_TURN_MARGIN,20
    $QUIT
== cmdfile.20.1 ==
    $GLIDE_SLOPE,30
    $D_TGT,45
    $T_DIVE,15
    $T_MISSION,20
    $C_VBD,2275
    $SM_CC,250
    $MAX_BUOY,300
    $C_PITCH,2750
    $PITCH_GAIN,15
    $C_ROLL_DIVE,1950
    $C_ROLL_CLIMB,1880
    $ROLL_DEG,50
    $ALTIM_PING_DEPTH,100
    $ALTIM_PING_DELTA,5
    $ALTIM_SENSITIVITY,3
    $ALTIM_PULSE,3
    $ALTIM_BOTTOM_TURN_MARGIN,20
    $QUIT
== cmdfile.20.2 ==
    $GLIDE_SLOPE,30
    $D_TGT,45
    $T_DIVE,15
    $T_MISSION,20
    $C_VBD,2275
    $SM_CC,250
    $MAX_BUOY,300
    $C_PITCH,2750
    $PITCH_GAIN,15
    $C_ROLL_DIVE,1950
    $C_ROLL_CLIMB,1880
    $ROLL_DEG,50
    $ALTIM_PING_DEPTH,100
    $ALTIM_PING_DELTA,5
    $ALTIM_SENSITIVITY,3
    $ALTIM_PULSE,3
    $ALTIM_BOTTOM_TURN_MARGIN,20
    $QUIT