BEGIN GEOM type plane match x y z phi theta pitch stpang xwid maxstp yrot zrot lb-n 1 2 0. 0. 0. 0. 0. 0.0075 0.04 6.0 768 0. 0. lb-n 2 1 0. 0. 0. 0. 0. 0.0075 0. 6.0 768 0. 0. att-n 3 0 0. 0. 2.5 0. 0. 0.0075 0. 6.0 128 0. 0. lb-n 4 5 5. 0. 9.75 0. 0. 0.0050 0.08 3.4 640 5.5 11. lb-p 5 4 5. 0. 9.75 0. 0. 0.0050 0. 3.4 640 5.5 11. att-n 6 0 5. 0. 12.3 0. 0. 0.0075 0. 6.0 256 0. 0. lb-n 7 8 0. 0. 19.3 0. 0. 0.0075 0.04 6.0 768 0. 0. lb-n 8 7 0. 0. 19.3 0. 0. 0.0075 0. 6.0 768 0. 0. att-p 9 0 0. 0. 21.8 0. 0. 0.0075 0.0 6.0 256 0. 0. END GEOM BEGIN DSP 4 plane0 plane1 plane2 plane3 upkalg0 upkalg1 upkalg2 upkalg3 nchips hi sysfile trigfile 9 -999 -999 -999 1 1 1 1 2 1 sys_main.asc TrigControl.dat 2 -999 -999 -999 1 1 1 1 5 1 sys_main.asc TrigControl.dat 2 2 -999 -999 1 1 1 1 6 1 sys_main.asc TrigControl.dat 1 -999 -999 -999 1 1 1 1 2 1 sys_main_ox.asc Control_run_ox.com 32227 3 == Run and num_tim_buc END DSP BEGIN DAC dsp Vatt(float) Vref(float) Vthn(int) Vth(int) 0 1.0 0.75 60 60 1 0.0 0.775 110 110 2 0.0 0.75 110 110 3 0.0 0.75 110 110 END DAC