# **************************************************************************** # CUI # # The Advanced Framework for Simulation, Integration, and Modeling (AFSIM) # # The use, dissemination or disclosure of data in this file is subject to # limitation or restriction. See accompanying README and LICENSE for details. # **************************************************************************** ############################################################################### # Launch computer generator for RED_ICBM_1. ############################################################################### # # This is a three step process: # # 1) Run once with a large loft angle sweep and no burn time constraint. Examine # the output file to determine the loft angle that results in the maximum range. # # 2) Rerun with a finer loft angle sweep that brackets the maximum range. Again # examine the output file to determine the loft angle that results in the # maximum range. # # 3) Run one more time, specifying a single loft angle equal to the maximum loft # angle equal to the value from step 2 that resulted in the maximum range. # Also specify a burn time range that encompasses the second stage. # the loft angle ############################################################################### include red_icbm_1.txt platform_type LAUNCH_PLATFORM_TYPE WSF_PLATFORM side red weapon red_icbm_1 RED_ICBM_1 end_weapon end_platform_type tool BALLISTIC_MISSILE_LAUNCH_COMPUTER_GENERATOR # ballistic_missile_launch_computer_generator tool_debug # altitude 1 m choosen to correspond with typical scenario altitudes #position 0n 0e altitude 1 m position 50:19n 123:51e heading 40 deg altitude 1 m surface_target_file red_icbm_1_launch_data.txt # Step 1 #loft_angles from 70 deg to 80 deg by 2 deg # Step 2 #loft_angles from 72.0 deg to 73.0 deg by 0.05 deg # Step 3 loft_angle 72.1 deg burn_times from 151 sec to 250 sec by 0.5 sec end_tool #event_pipe # file replay.aer #end_event_pipe