70 lines
2.5 KiB
Plaintext
70 lines
2.5 KiB
Plaintext
# ****************************************************************************
|
|
# 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 BLUE_SR_SAM.
|
|
###############################################################################
|
|
|
|
file_path ../../../base_types
|
|
include blue_sr_sam_simple.txt
|
|
|
|
platform_type LAUNCH_PLATFORM_TYPE WSF_PLATFORM
|
|
side red
|
|
weapon blue_sr_sam BLUE_SR_SAM
|
|
|
|
# Override the firing delay because we are using the firing delay during
|
|
# the real simulation to overcome a problem with ballistic intercept
|
|
# prediction not accounting for drag.
|
|
|
|
firing_delay 0.0 sec
|
|
end_weapon
|
|
end_platform_type
|
|
|
|
tool BALLISTIC_MISSILE_LAUNCH_COMPUTER_GENERATOR # ballistic_missile_launch_computer_generator
|
|
tool_debug
|
|
|
|
frame_step 0.5 sec # sample time of trajectory
|
|
|
|
# altitude 1 m choosen to correspond with typical scenario altitudes
|
|
position 0n 0e altitude 1 m
|
|
|
|
air_target_file blue_sr_sam_launch_data.txt
|
|
#gnuplot_file blue_sr_sam_trajectory.plt
|
|
|
|
loft_angles from 20 deg to 85 deg by 0.2 deg
|
|
|
|
############################################################################
|
|
# All of the remaining data is used to keep the launch computer dataset
|
|
# small and to only enable solutions that are doctrinally allowed.
|
|
#
|
|
# If you change these values, also review the weapon fuse definitions in
|
|
# blue_sr_sam.txt. It has limits that will cause the weapon to self-destruct in
|
|
# certain cases.
|
|
############################################################################
|
|
|
|
# 'minimum_output_time' should be greater than or equal to the burn time.
|
|
# (No intercept during boost)
|
|
minimum_output_time 10 sec
|
|
|
|
# Jane's says the max range is 15-20km, but may be more things like
|
|
# fighters or cruise missiles.
|
|
#
|
|
# (MJM) Missiles were fusing on min mach for low trajectories; setting range
|
|
# to just over 20 km.
|
|
maximum_output_range 22.5 km
|
|
|
|
# Jane's says the max intercept altitude is 15 km, but we may need to
|
|
# go past apogee, so we'll set it higher.
|
|
maximum_output_altitude 20 km
|
|
|
|
end_tool
|
|
|
|
event_pipe
|
|
#file replay.aer
|
|
end_event_pipe
|