初次提交,只有想定基本结构
This commit is contained in:
218
weapons/aam/aa_mrm.txt
Normal file
218
weapons/aam/aa_mrm.txt
Normal file
@@ -0,0 +1,218 @@
|
||||
# ****************************************************************************
|
||||
# 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
|
||||
# This air to air missile boilerplate is an example
|
||||
# to create air to air missiles.
|
||||
# For the baseline, it is loosly modeled after the R-77 / AA-12 ADDER
|
||||
# All sources came from the internet:
|
||||
# Janes / wikipedia / sinodefence / globalsecurity / fas / deagel etc.
|
||||
# Even aviation.ru provided spec information.
|
||||
# The missile is similiar to the AIM-120 AMRAAM and has been
|
||||
# nicknamed "amraamski". It is a launch and forget type missile
|
||||
# such that it has its own inertial system and terminal guidance radar.
|
||||
|
||||
# From global security:
|
||||
# Length 3.60 m
|
||||
# Body diameter 200 mm
|
||||
# Wingspan 0.35 m
|
||||
# Launch weight 175 kg
|
||||
# Warhead 30 kg HE fragmentation
|
||||
# Fuze Active radar
|
||||
# Guidance Inertial, command and active radar
|
||||
# Propulsion Solid propellant
|
||||
# Range 50 km
|
||||
|
||||
# From aviation.ru/missiles.htm:
|
||||
# launch mass = 175 kg.
|
||||
# warhead mass = 21 kg.
|
||||
# max hit range = 50 km.
|
||||
# min hit range = 300 m.
|
||||
# max target overload = 12.
|
||||
# hit probability = 0.7.
|
||||
# length = 3600 mm.
|
||||
# body diameter = 200 mm.
|
||||
# wing span = 750 mm.
|
||||
# max target speed = 3600 km/h.
|
||||
# altitude range = 20m..25km.
|
||||
# max altitude difference = 10 km (can only climb 10 km from launch).
|
||||
# no carrier overload limitation.
|
||||
# can be loaded in conform mode or in an internal weapon bay.
|
||||
# active radar self-guidance head and inertial navigation system with radio correction.
|
||||
# "fire-and-forget" mode.
|
||||
|
||||
# From deagel.com
|
||||
# Dimensions: Diameter 200 mm, Length 3.6 m, Width 350 mm
|
||||
# Weights: Max Weight 175 kg (386 lb), Warhead 30 kg (66.1 lb)
|
||||
# Performance: Ceiling 25,000 m (82,021 ft), Max Range 90,000 m (295,276 ft), Top Speed 1,328 mps (Mach 4)
|
||||
# Inertial nav / optional inflight midcourse updates / Radar turn on 20km from target
|
||||
|
||||
# From enemysources.com
|
||||
# Range against closing target 150 km
|
||||
# Range against receding target 50 - 90 km
|
||||
# Weight 175 kg
|
||||
# Weight of warhead 30 kg
|
||||
# Type of warhead expanding rod
|
||||
# Speed Mach 4+
|
||||
# Guidance active radarhoming
|
||||
# Length 3.6 m
|
||||
# Diameter 0.2 m
|
||||
|
||||
# From fas.org
|
||||
# Length 3.60 m
|
||||
# Body diameter 200 mm
|
||||
# Wingspan 0.35 m
|
||||
# Launch weight 175 kg
|
||||
# Warhead 30 kg HE fragmentation
|
||||
# Fuze Active radar
|
||||
# Guidance Inertial, command and active radar
|
||||
# Propulsion Solid propellant
|
||||
# Range 50 km
|
||||
|
||||
# From sinodefense
|
||||
# Length: 3.60m
|
||||
# Diameter: 0.200m
|
||||
# Wingspan: 0.350m
|
||||
# Launch weight: 175kg
|
||||
# Propellant: Solid fuel rocket motor
|
||||
# Guidance: Inertial + mid-course command + terminal active radar
|
||||
# Range: 50~80km
|
||||
# Warhead: 30kg HE-fragment
|
||||
# Fuse: Laser proximity fuse
|
||||
|
||||
# From Australian Defence Annual Report 2002-3 dated July 4, 2004
|
||||
# A more recent development is the Vympel R-77 RVV-AE, dubbed the
|
||||
# "Amraamski" by Western observers94. The Vympel R-77 (AA-12 Adder) is an active
|
||||
# radar guided BVR AAM and is designed to engage 12 G targets. It employs fuselage
|
||||
# strakes for enhanced body lift at an AoA in excess of 40<34>, and unique electrically actuated
|
||||
# "grid" control surfaces to achieve additional control force at high AoA. This is
|
||||
# claimed to provide a 150<35>/sec turn rate. The R-77 weighs in at 386 lb and Vympel quote
|
||||
# an A-pole range at altitude of up to 54 NMI, with a minimum range of about 1000 ft. A
|
||||
# 48.5 lb continuous rod warhead is initiated by a laser proximity fuse.
|
||||
# This missile, like the US AIM-120, uses digital datalink/inertial midcourse
|
||||
# guidance and active terminal homing, supports an LOBL off-the-rail active launch mode
|
||||
# and is claimed to have a Home-On-Jam (HOJ) capability. Carried by the Flanker and Fulcrum,
|
||||
# the missile requires the APU-170 pylon adaptor, and a late model AI radar such as
|
||||
# the Phazotron Zhuk or N-011.
|
||||
# AGAT 9B-1103M/9B-1348E(R-77 Seeker) 25 NMI 1 squared meter detection track range
|
||||
# AGAT 9B-1103M/9B-1348E(R-77 Seeker) 7 NMI 1 squared meter detection lock range
|
||||
|
||||
|
||||
include sensors/radar/aa_mrm_radar.txt # For now, just put a simple x-band radar on it
|
||||
|
||||
aero AA_MRM_AERO WSF_AERO
|
||||
# Values estimated from Hoerner's Drag book
|
||||
cd_zero_subsonic 0.30
|
||||
cd_zero_supersonic 0.50
|
||||
mach_begin_cd_rise 0.95
|
||||
mach_end_cd_rise 1.3
|
||||
mach_max_supersonic 4.0 # Ref
|
||||
reference_area 0.125 m2 # 200mm body dia
|
||||
cl_max 3.5
|
||||
|
||||
end_aero
|
||||
|
||||
platform_type AA_MRM WSF_PLATFORM
|
||||
icon Missile
|
||||
|
||||
mover WSF_GUIDED_MOVER
|
||||
total_mass 175 kg # all of the sources say this
|
||||
fuel_mass 80 kg # guess - 30 kg warhead, sensor weight, and body weight
|
||||
thrust 6500 lbf # to make it go 1300 mps as stated above
|
||||
thrust_duration 95 sec # sources say several seconds
|
||||
update_interval 0.05 sec
|
||||
aero AA_MRM_AERO
|
||||
end_mover
|
||||
|
||||
comm uplink WSF_COMM_TRANSCEIVER
|
||||
internal_link data_mgr
|
||||
internal_link task_mgr
|
||||
end_comm
|
||||
|
||||
processor data_mgr WSF_WEAPON_TRACK_PROCESSOR
|
||||
end_processor
|
||||
|
||||
processor task_mgr WSF_TASK_PROCESSOR
|
||||
end_processor
|
||||
|
||||
processor computer WSF_GUIDANCE_COMPUTER
|
||||
proportional_navigation_gain 455.0
|
||||
# velocity_pursuit_gain 1.0
|
||||
g_bias 1.1
|
||||
maximum_commanded_g 12.0 g
|
||||
update_interval 0.05 s
|
||||
end_processor
|
||||
|
||||
processor fuse WSF_AIR_TARGET_FUSE
|
||||
max_time_of_flight_to_detonate 100.0 sec
|
||||
end_processor
|
||||
|
||||
sensor seeker AA_MRM_RADAR
|
||||
# on # testing only - it gets turned on by the Weapon Track Processor
|
||||
ignore_same_side
|
||||
processor data_mgr
|
||||
internal_link task_mgr
|
||||
end_sensor
|
||||
|
||||
script_variables
|
||||
bool mTrackFromE2C = false;
|
||||
bool mTrackFromE2CSet = false;
|
||||
end_script_variables
|
||||
|
||||
processor seeker_turn_on WSF_WEAPON_TRACK_PROCESSOR
|
||||
# turn_on_sensor seeker 20.0 sec after_launch
|
||||
turn_on_sensor seeker at_range 20000.0 m before_intercept
|
||||
update_interval 1 sec
|
||||
on_update
|
||||
extern bool mTrackFromE2CSet;
|
||||
extern bool mTrackFromE2C;
|
||||
if (! mTrackFromE2CSet)
|
||||
{
|
||||
if (PLATFORM.Sensor("seeker").IsTurnedOn())
|
||||
{
|
||||
WsfTrack extTrack = PLATFORM.CurrentTargetTrack();
|
||||
if (extTrack.IsValid() && (extTrack.OriginatorType() == "e2c"))
|
||||
{
|
||||
mTrackFromE2C = true;
|
||||
}
|
||||
mTrackFromE2CSet = true;
|
||||
}
|
||||
}
|
||||
end_on_update
|
||||
end_processor
|
||||
|
||||
script void on_weapon_target_engagement(WsfWeaponEngagement aEngagement, WsfPlatform aTarget)
|
||||
writeln_d("*********** on_weapon_target_engagement");
|
||||
if (mTrackFromE2C)
|
||||
{
|
||||
aEngagement.SetPkDegrade(0.6);
|
||||
}
|
||||
end_script
|
||||
end_platform_type
|
||||
|
||||
|
||||
weapon_effects AA_MRM_EFFECT WSF_GRADUATED_LETHALITY # unknown
|
||||
radius_and_pk 100.0 m 0.7 #radius is unknown pk of .7 documented
|
||||
end_weapon_effects
|
||||
|
||||
weapon AA_MRM WSF_EXPLICIT_WEAPON
|
||||
aux_data
|
||||
double LARmeters = 100000
|
||||
end_aux_data
|
||||
launched_platform_type AA_MRM
|
||||
weapon_effects AA_MRM_EFFECT
|
||||
automatic_target_cueing true
|
||||
quantity 1
|
||||
firing_delay 0.2 sec # unknown
|
||||
salvo_interval 5.0 sec # unknown
|
||||
firing_interval 15.0 sec # unknown
|
||||
slew_mode azimuth_and_elevation
|
||||
azimuth_slew_limits -15.0 deg 15.0 deg # allows for off boresight target slewing
|
||||
elevation_slew_limits -35.0 deg 15.0 deg # allow some super-elevation for low-alt targets
|
||||
|
||||
end_weapon
|
||||
Reference in New Issue
Block a user