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