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lab1/weapons/ssm/blue_cruise_missile.txt

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2025-09-12 15:20:28 +08:00
# ****************************************************************************
# 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.
# ****************************************************************************
#UNCLASSIFIED
# Tomahawk surfaced launched version (has a booster)
# All data from internet sources
#
# No terminal sensor for now.
infrared_signature BLUE_CRUISE_MISSILE_INFRARED_SIGNATURE
constant 1 watts/steradian
end_infrared_signature
optical_signature BLUE_CRUISE_MISSILE_OPTICAL_SIGNATURE
constant 1 m^2
end_optical_signature
radar_signature BLUE_CRUISE_MISSILE_RADAR_SIGNATURE
constant 1 m^2
end_radar_signature
aero BLUE_CRUISE_MISSILE_AERO WSF_AERO
cd_zero_subsonic 0.1
cd_zero_supersonic 0.25
mach_begin_cd_rise 0.95
mach_end_cd_rise 1.3
mach_max_supersonic 4
reference_area 0.21237 m2 #0.52 meter diameter
cl_max 10
aspect_ratio 16.0
end_aero
weapon_effects BLUE_CRUISE_MISSILE_LETHALITY WSF_GRADUATED_LETHALITY
radius_and_pk 30 m 0.85
end_weapon_effects
platform_type BLUE_CRUISE_MISSILE WSF_PLATFORM
icon CALCM
category cruise-missile
infrared_signature BLUE_CRUISE_MISSILE_INFRARED_SIGNATURE
optical_signature BLUE_CRUISE_MISSILE_OPTICAL_SIGNATURE
radar_signature BLUE_CRUISE_MISSILE_RADAR_SIGNATURE
mover WSF_GUIDED_MOVER
#show_status
update_interval .5 sec
integration_timestep 0.05 sec
stage 1 # Booster
initial_mass 550 lbs
fuel_mass 440 lbs
thrust 7418 lbf
thrust_duration 12 sec
aero BLUE_CRUISE_MISSILE_AERO
end_stage
stage 2 # Turbofan
initial_mass 2650 lb
fuel_mass 500 lb # guess
thrust 696.9 lbf
burn_rate 350 lb/hr
aero BLUE_CRUISE_MISSILE_AERO
thrust_delay 1.0 sec # no idea how long before it fires off after the booster falls off...
end_stage
end_mover
processor guidance WSF_GUIDANCE_COMPUTER
#show_status
#show_evaluations
#debug
guide_to_truth true # for testing
phase LAUNCH
commanded_altitude 5000 ft
commanded_flight_path_angle 60 deg
next_phase CRUISE when phase_time > 16 sec
end_phase
phase CRUISE
commanded_altitude 500 ft agl
commanded_speed 910 fps
maximum_commanded_g 2 g
next_phase TERMINAL if target_slant_range < 1 miles
end_phase
phase TERMINAL
commanded_speed 800 fps
proportional_navigation_gain 40
maximum_pitch_angle 90 deg
maximum_commanded_g 10 g
end_phase
end_processor
processor fuse WSF_GROUND_TARGET_FUSE
end_processor
comm uplink WSF_COMM_TRANSCEIVER
internal_link data_mgr
end_comm
processor task_mgr WSF_TASK_PROCESSOR
end_processor
processor data_mgr WSF_TRACK_PROCESSOR
purge_interval 4000 seconds
end_processor
end_platform_type
weapon BLUE_CRUISE_MISSILE WSF_EXPLICIT_WEAPON
launched_platform_type BLUE_CRUISE_MISSILE
weapon_effects BLUE_CRUISE_MISSILE_LETHALITY
quantity 1
firing_delay 0.0 sec
salvo_interval 2 sec
slew_mode azimuth
azimuth_slew_limits -180 deg 180 deg
tilt 88.9 deg
end_weapon