+

WO1996008688A1 - System and method for hitting a target in a cluster - Google Patents

System and method for hitting a target in a cluster Download PDF

Info

Publication number
WO1996008688A1
WO1996008688A1 PCT/US1995/012591 US9512591W WO9608688A1 WO 1996008688 A1 WO1996008688 A1 WO 1996008688A1 US 9512591 W US9512591 W US 9512591W WO 9608688 A1 WO9608688 A1 WO 9608688A1
Authority
WO
WIPO (PCT)
Prior art keywords
bomb
cluster
targets
location
flight
Prior art date
Application number
PCT/US1995/012591
Other languages
French (fr)
Inventor
Rami Fabian
Original Assignee
State Of Israel - Ministry Of Defence Rafael - Armament Development Authority
Friedman, Mark, M.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by State Of Israel - Ministry Of Defence Rafael - Armament Development Authority, Friedman, Mark, M. filed Critical State Of Israel - Ministry Of Defence Rafael - Armament Development Authority
Priority to AU39457/95A priority Critical patent/AU3945795A/en
Publication of WO1996008688A1 publication Critical patent/WO1996008688A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30Command link guidance systems
    • F41G7/301Details
    • F41G7/308Details for guiding a plurality of missiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/007Preparatory measures taken before the launching of the guided missiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2233Multimissile systems

Definitions

  • the present invention relates to systems and methods for targeting
  • one or more support vehicles or a column of tanks which may either be
  • the missiles have accuracies which are at least as good
  • a bomb including: (i) a navigational system for
  • the present invention successfully addresses the shortcomings of the
  • the present invention discloses a novel system and method which
  • the bomb guides itself to the vicinity of the cluster using
  • head homes in on a specific target from among the cluster of targets and
  • the present invention is of a system and method for hitting one or
  • Bomb 10 may be of various suitable type. Typically, bomb 10
  • an explosive warhead and a homing head which may include any
  • suitable transmitter/receiver units preferably one which operates using
  • Bomb 10 also includes various aerodynamics members, such as
  • bomb 10 includes a navigational system, which
  • GPS Global Position System
  • IMU Inertial Measurement Unit
  • INS Inertial Navigation System
  • Bomb 10 further includes suitable means for calculating the
  • Bomb 10 may be a gliding bomb so it is launched
  • bomb 10 or preferably a number of bombs 10, are launched from an attack
  • the intelligence can be obtained on the location of a cluster of targets 14.
  • Synthetic Aperture Radar mounted on attack aircraft 12 or on any combination
  • bomb 10 is fed the location of the cluster of targets.
  • bomb 10 continually receives or generates
  • navigational information as through its GPS receiver, IMU or INS as to
  • Bomb 10 uses the navigational information and the
  • Navigational system information continues to be received or
  • bomb 10 typically extends from launch until bomb 10 is approximately from about
  • the bomb homing head acquires the target
  • cluster and further trajectory corrections are based on homing head.
  • homing head of a specific bomb 10 selects a
  • homing head is divided into a number of sectors or a number of individual
  • bomb 10 reaches the vicinity of the targets, which for a typical launch from
  • bomb 10 The updating of bomb 10 is effected through the equipping of bomb
  • a suitable electromagnetic receiver preferably a UHF receiver
  • bomb 10 is approximately 2000 to 7000 meters ground distance from

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

A system and method for hitting a target in a cluster of targets (14). The method includes acquiring intelligence relating to the location of the cluster of targets (14) and transmitting the intelligence. The method then involves launching a bomb or missile (10), the bomb or missile (10) including a navigational system for providing information regarding the position of the bomb or missile (10) during a first portion of the flight of the bomb or missile (10) and a mechanism for controlling the trajectory of the bomb or missile (10) based on the information regarding the position of the bomb or missile (10) and the intelligence relating to the location of the cluster of targets (14) during the first portion of the flight of the bomb or missile (10). The bomb or missile (10) further includes a mechanism for selecting a sector or a target within the cluster of targets (14) during a subsequent portion of the flight and a mechanism for controlling the trajectory of the bomb or missile (10) during the subsequent portion of the flight of the bomb or missile (10).

Description

APPLICATION FOR PATENT
Title: SYSTEM AND METHOD FOR HITTING A TARGET IN
A CLUSTER
FIELD AND BACKGROUND OF THE INVENTION
The present invention relates to systems and methods for targeting
one or more member of a cluster of targets.
In combat operations it is often necessary to target and destroy one
or more members of a cluster of ground targets located deep behind enemy
lines. For example, it may be desired to destroy an artillery or missile
battery made up of a number of artillery pieces or missile launchers and
one or more support vehicles, or a column of tanks which may either be
camped and thus stationary or moving along an axis.
Various methods are available for effectively handling such targets.
Perhaps the most effective method known heretofore is using combat
aircraft which overfly the targets, identify and locate the target and then
launch one or more of a variety of bombs and missiles (hereinafter
generally referred to in the description and claims collectively and
singularly as "bombs") to destroy the targets.
A disadvantage of such techniques is that it requires a manned
attacking aircraft to fly deep into enemy territory with possible adverse
implications for the survivability of the aircraft and crew. An alternative solution is the use of ground-to-ground or air-to-
ground missiles. The missiles have accuracies which are at least as good
as those attained by projectiles launched from manned aircraft and have the
advantage of not incurring undue risk to attacking personnel. The
disadvantage of such missiles is their very high cost, which makes them
practical only for extremely sensitive or valuable targets.
There is thus a widely recognized need for, and it would be highly
advantageous to have, a relatively inexpensive system for accurately hitting
one or more target in a cluster of targets, which does not require the
placement of personnel in the vicinity of the targets.
SUMMARY OF THE INVENTION
According to the present invention there is provided a system and
method for hitting a target in a cluster of targets, the system comprising:
(a) means for acquiring intelligence relating to the location of the cluster
of targets; (b) means for transmitting the intelligence relating to the
location of the cluster; (c) a bomb including: (i) a navigational system for
providing information regarding the position of the bomb during a first
portion of the flight of the bomb; (ii) means for controlling the trajectory
of the bomb based on the information regarding the position of said bomb
and the intelligence relating to the location of the cluster of targets during
the first portion of the flight of the bomb; (iii) means for selecting a sector or a target within the cluster of targets; (iv) a homing head for homing in
on the sector or the target among the cluster of targets during a subsequent
portion of the flight of the bomb; and (v) means for controlling the
trajectory of the bomb during the subsequent portion of the flight of the
bomb.
The present invention successfully addresses the shortcomings of the
presently known configurations by providing an inexpensive and effective
system and method for delivering a bomb to one item of a cluster of
targets.
The present invention discloses a novel system and method which
allows one or more bombs to be released at a safe distance from a cluster
of targets. The bomb guides itself to the vicinity of the cluster using
navigational information. Once in the vicinity of the cluster, a homing
head homes in on a specific target from among the cluster of targets and
guides the bomb to its target.
BRIEF DESCRIPTION OF THE DRAWINGS
The invention is herein described, by way of example only, with
reference to the accompanying drawings, wherein the sole Figure
schematically illustrates the operation of a system and method according
to the present invention. DESCRIPTION OF THE PREFERRED EMBODIMENTS
The present invention is of a system and method for hitting one or
more targets in a cluster of targets. The principles and operation of a
system and method according to the present invention may be better
understood with reference to the drawing and the accompanying
description.
Referring now to the drawings, the sole Figure shows a typical
launch of a number of bombs 10 (four are shown in the Figure) from an
aircraft 12 (shown in two positions along its flight).
Bomb 10 may be of various suitable type. Typically, bomb 10
includes an explosive warhead and a homing head, which may include any
suitable transmitter/receiver units, preferably one which operates using
microwave radiation, giving bomb 10 all-weather capabilities.
Bomb 10 also includes various aerodynamics members, such as
wings or tail, at least some of which are adjustable so as to effect trajectory
corrections. In addition, bomb 10 includes a navigational system, which
may include a Global Position System (GPS) receiver for receiving GPS
information from a GPS satellite, or an Inertial Measurement Unit (IMU)
or an Inertial Navigation System (INS) or combination, and the like.
Bomb 10 further includes suitable means for calculating the
trajectory and for correcting the trajectory through appropriate adjustments of wings or tail 18. Bomb 10 may be a gliding bomb so it is launched
from an aircraft at a desired height and glides to its target exclusively
under the influence of gravity or it may include an engine.
A schematic depiction of a basic embodiment of a system and
method according to the present invention is presented in the Figure. Here,
bomb 10, or preferably a number of bombs 10, are launched from an attack
aircraft 12. The launch of bomb or bombs 10 takes place after intelligence
is obtained on the location of a cluster of targets 14. The intelligence can
be acquired through any suitable means, including but not limited to, a
Synthetic Aperture Radar (SAR) mounted on attack aircraft 12 or on any
other convenient aircraft, from satellite or spy plane photographs, and the
like.
In the basic embodiment, information regarding the location of the
detected cluster of targets 14 and relative locations within the cluster is
transmitted to bomb 10 prior to its launch from attack aircraft 12. Thus,
prior to launch, bomb 10 is fed the location of the cluster of targets.
Following launch, bomb 10 continually receives or generates
navigational information, as through its GPS receiver, IMU or INS as to
its own location. Bomb 10 uses the navigational information and the
stored information relating to cluster of target 14, and suitable pattern
recognition means to calculate and effect trajectory corrections designed to
bring itself as close as possible to the target cluster. Navigational system information continues to be received or
generated throughout the first portion of the flight of bomb 10 which
typically extends from launch until bomb 10 is approximately from about
7 to about 2 km ground distance from cluster of targets 14. At the end of
the first portion of the flight, the bomb homing head acquires the target
cluster and further trajectory corrections are based on homing head.
Further to instructions from aircraft 12 or another source prior to the
launch of bombs 10 or further to instructions transmitted to bomb 10
subsequent to its launch, homing head of a specific bomb 10 selects a
sector or a specific target within cluster of targets 14.
Thus, when several bombs 10 are launched at approximately the
same time, which is typically the case, cluster of targets 14 detected by the
homing head is divided into a number of sectors or a number of individual
targets so that each bomb 10 is aimed at a different sector or a different
specific target, thereby avoiding the possibility of two bombs 10 being
directed to the same specific target.
In some applications, particularly when targets 14 are moving, it
may be advantageous to update the location of the target cluster during the
flight of bomb 10. When the cluster of targets is moving, by the time
bomb 10 reaches the vicinity of the targets, which for a typical launch from
20,000-40,000 ft could take five to ten minutes, the cluster is found at a location which is significantly different from its location at the moment of
launch.
The updating of bomb 10 is effected through the equipping of bomb
10 with a suitable electromagnetic receiver, preferably a UHF receiver,
which receives signals sent by attack aircraft 30 or by a suitable alternative
source.
It is estimated that in this version of a system according to the
present invention, the first portion of the free flight of bomb 10 which is
guided with the help of an appropriate navigational system can take place
until bomb 10 is approximately 2000 to 7000 meters ground distance from
the target cluster.
While the invention has been described with respect to a limited
number of embodiments, it will be appreciated that many variations,
modifications and other applications of the invention may be made.

Claims

WHAT IS CLAIMED IS:
1. A system for hitting a target in a cluster of targets,
comprising:
(a) means for acquiring intelligence relating to the location of the
cluster of targets;
(b) means for transmitting said intelligence relating to the
location of the cluster;
(c) a bomb including:
(i) a navigational system for providing information
regarding the position of said bomb during a first
portion of the flight of said bomb;
(ii) means for controlling the trajectory of said bomb
based on said information regarding the position of
said bomb and said intelligence relating to the location
of the cluster of targets during said first portion of the
flight of said bomb;
(iii) means for selecting a sector or a target within the
cluster of targets;
(iv) a homing head for homing in on a said sector or said
target among the cluster of targets during a subsequent
portion of the flight of said bomb; and (v) means for controlling the trajectory of said bomb
during said subsequent portion of the flight of said
bomb.
2. A system as in claim 1, wherein said means for acquiring
intelligence relating to the location of the cluster of targets includes GPS.
3. A system as in claim 1, wherein said means for acquiring
intelligence relating to the location of the cluster of targets includes IMU.
4. A system as in claim 1, wherein said means for acquiring
intelligence relating to the location of the cluster of targets includes INS.
5. A system as in claim 1, wherein said means for controlling
the trajectory of said bomb based on said information regarding the
position of said bomb and said intelligence relating to the location of the
cluster of targets during said first portion of the flight of said bomb
includes means for performing pattern recognition.
6. A system as in claim 1, wherein said homing head includes
means for performing pattern recognition.
7. A system as in claim 1 , wherein said bomb is a gliding bomb
and said bomb is launched from an aircraft.
8. A system as in claim 1, wherein said bomb is a powered
bomb and said bomb is launched from an aircraft.
9. A system as in claim 1, wherein said means for acquiring
intelligence includes an SAR.
10. A system as in claim 1, wherein said means for acquiring
intelligence includes an intelligence satellite.
11. A system as in claim 1 , wherein said bomb is a gliding bomb
and said bomb is launched from an aircraft and further wherein said means
for acquiring intelligence includes an SAR mounted on said aircraft.
12. A system as in claim 1, wherein said means for transmitting
said location of the cluster is effective prior to the launch of said bomb.
13. A system as in claim 1 , wherein said means for transmitting
said location of the cluster is effected after the launch of said bomb.
14. A system as in claim 13, wherein said bomb further includes
an electromagnetic receiver for receiving said location of the cluster.
15. A system as in claim 13, wherein said electromagnetic
receiver is a UHF receiver.
16. A system as in claim 6, wherein said first portion of the flight
of said bomb extends from launch until said bomb is from about 7 to about
2 km from the cluster of targets.
17. A system as in claim 1 , wherein said homing head includes
a microwave transmitter and receiver.
18. A method hitting a target in a cluster of targets, comprising
the steps of:
(a) acquiring intelligence relating to the location of the cluster of
targets;
(b) transmitting said intelligence relating to the location of the
cluster of targets;
(c) launching a bomb, said bomb including: (i) a navigational system for providing information
regarding the position of said bomb during a first
portion of the flight of said bomb;
(ii) means for controlling the trajectory of said bomb
based on said information regarding the position of
said bomb and said intelligence relating to the location
of the cluster of targets during said first portion of the
flight of said bomb;
(iii) means for selecting a sector or a target within the
cluster of targets;
(iv) a homing head for homing in on a said sector or said
target among the cluster of targets during a subsequent
portion of the flight of said bomb; and
(v) means for controlling the trajectory of said bomb
during said subsequent portion of the flight of said
bomb.
PCT/US1995/012591 1994-09-13 1995-09-06 System and method for hitting a target in a cluster WO1996008688A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU39457/95A AU3945795A (en) 1994-09-13 1995-09-06 System and method for hitting a target in a cluster

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IL11096094A IL110960A0 (en) 1994-09-13 1994-09-13 System and method for hitting a target in a cluster
IL110960 1994-09-13

Publications (1)

Publication Number Publication Date
WO1996008688A1 true WO1996008688A1 (en) 1996-03-21

Family

ID=11066553

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1995/012591 WO1996008688A1 (en) 1994-09-13 1995-09-06 System and method for hitting a target in a cluster

Country Status (3)

Country Link
AU (1) AU3945795A (en)
IL (1) IL110960A0 (en)
WO (1) WO1996008688A1 (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2780154A1 (en) * 1998-06-19 1999-12-24 Dassault Electronique Remotely guided aircraft engine
US6196496B1 (en) 1998-06-29 2001-03-06 State Of Israel Ministry Of Defense Armament Development Authority Raeael Method for assigning a target to a missile
RU2212620C1 (en) * 2002-04-09 2003-09-20 Григорьев Владимир Григорьевич Method for determination of values of parameters of bomb trajectory
FR2928452A1 (en) * 2008-03-07 2009-09-11 Thales Sa LOW COST DRIVING DEVICE FOR FIXED AND MOBILE TARGETS
WO2012125217A1 (en) * 2011-03-17 2012-09-20 Raytheon Company Deconfliction of guided airborne weapons fired in a salvo
RU2474843C1 (en) * 2011-10-05 2013-02-10 Виктор Леонидович Семенов Instantaneous bullet speed measuring radar
EP1989501A4 (en) * 2006-03-01 2013-05-22 Raytheon Co Multiple kill vehicle (mkv) interceptor with autonomous kill vehicles
RU2484497C2 (en) * 2011-07-21 2013-06-10 Виктор Леонидович Семенов Method of selecting small-size targets and apparatus for realising said method
RU2522426C2 (en) * 2011-10-05 2014-07-10 Виктор Леонидович Семенов Method of measuring change in target velocity on range and apparatus therefor
NO340726B1 (en) * 2015-08-12 2017-06-06 Kongsberg Defence & Aerospace As Method and system for planning and launching a plurality of missiles to be included in the same mission

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1000956A (en) * 1949-12-02 1952-02-18 Sealed connection for pressurized fluids
DE2926215A1 (en) * 1978-07-11 1980-01-24 Chesini Snc PERFECTED CONNECTOR WITH CONE SEAL O.AE.
CH681558A5 (en) * 1991-04-16 1993-04-15 Tubex Ag Water supply pipe safety connection - includes fitting carrying sealing ring and incorporating locking lug or hooked lug engaging teeth on outer cap
DE4218347A1 (en) * 1992-06-04 1993-12-09 Mosmatic Ag Necker Spray tube or spray lance of a high pressure cleaning device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1000956A (en) * 1949-12-02 1952-02-18 Sealed connection for pressurized fluids
DE2926215A1 (en) * 1978-07-11 1980-01-24 Chesini Snc PERFECTED CONNECTOR WITH CONE SEAL O.AE.
CH681558A5 (en) * 1991-04-16 1993-04-15 Tubex Ag Water supply pipe safety connection - includes fitting carrying sealing ring and incorporating locking lug or hooked lug engaging teeth on outer cap
DE4218347A1 (en) * 1992-06-04 1993-12-09 Mosmatic Ag Necker Spray tube or spray lance of a high pressure cleaning device

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2780154A1 (en) * 1998-06-19 1999-12-24 Dassault Electronique Remotely guided aircraft engine
US6196496B1 (en) 1998-06-29 2001-03-06 State Of Israel Ministry Of Defense Armament Development Authority Raeael Method for assigning a target to a missile
RU2212620C1 (en) * 2002-04-09 2003-09-20 Григорьев Владимир Григорьевич Method for determination of values of parameters of bomb trajectory
EP1989501A4 (en) * 2006-03-01 2013-05-22 Raytheon Co Multiple kill vehicle (mkv) interceptor with autonomous kill vehicles
FR2928452A1 (en) * 2008-03-07 2009-09-11 Thales Sa LOW COST DRIVING DEVICE FOR FIXED AND MOBILE TARGETS
WO2009112424A3 (en) * 2008-03-07 2009-11-26 Thales Low-cost fire control system for firing against fixed and moving targets
US8487226B2 (en) 2011-03-17 2013-07-16 Raytheon Company Deconfliction of guided airborne weapons fired in a salvo
WO2012125217A1 (en) * 2011-03-17 2012-09-20 Raytheon Company Deconfliction of guided airborne weapons fired in a salvo
RU2484497C2 (en) * 2011-07-21 2013-06-10 Виктор Леонидович Семенов Method of selecting small-size targets and apparatus for realising said method
RU2474843C1 (en) * 2011-10-05 2013-02-10 Виктор Леонидович Семенов Instantaneous bullet speed measuring radar
RU2522426C2 (en) * 2011-10-05 2014-07-10 Виктор Леонидович Семенов Method of measuring change in target velocity on range and apparatus therefor
NO340726B1 (en) * 2015-08-12 2017-06-06 Kongsberg Defence & Aerospace As Method and system for planning and launching a plurality of missiles to be included in the same mission
US9958237B2 (en) 2015-08-12 2018-05-01 Kongsberg Defence & Aerospace As Method and system for planning and launching a plurality of missiles to be included in the same mission

Also Published As

Publication number Publication date
IL110960A0 (en) 1995-07-31
AU3945795A (en) 1996-03-29

Similar Documents

Publication Publication Date Title
US4925129A (en) Missile defence system
US5647558A (en) Method and apparatus for radial thrust trajectory correction of a ballistic projectile
US6037899A (en) Method for vectoring active or combat projectiles over a defined operative range using a GPS-supported pilot projectile
US4641801A (en) Terminally guided weapon delivery system
US6481666B2 (en) Method and system for guiding submunitions
US20060238403A1 (en) Method and system for destroying rockets
US6196496B1 (en) Method for assigning a target to a missile
US11709040B2 (en) Laser guided bomb with proximity sensor
RU2584210C1 (en) Method of firing guided missile with laser semi-active homing head
WO1996008688A1 (en) System and method for hitting a target in a cluster
AU568300B2 (en) Terminally guided weapon delivery system
RU2538509C1 (en) Guided missile firing method
HERMAN et al. Subsystems for the extended range interceptor (ERINT-1) missile
US4238090A (en) All-weather intercept of tanks from a helicopter
RU2247312C1 (en) Method for check-up of results of target destruction
US2966316A (en) Missile
Montoya Standard Missile: A Cornerstone of Navy Theater Air Missile Defense
RU2254543C1 (en) Method for guidance of ballistic missile with separating correctable war module
Puttré Satellite-guided munitions
UA129637U (en) METHOD OF ADJUSTMENT OF AIRCRAFT Flight Kit Flight Trajectory
Siouris Tactical missile guidance laws
Neuman Application of an airborne engagement system to battlefield surveillance and attack control
EP0670465A1 (en) Missile homing system using secondary targets
Garwin SMART WEAPONS: BUT WHEN?

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AM AT AU BB BG BR BY CA CH CN CZ DE DK EE ES FI GB GE HU IS JP KE KG KP KR KZ LK LR LT LU LV MD MG MN MW MX NO NZ PL PT RO RU SD SE SG SI SK TJ TM TT UA UG US UZ VN

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): KE MW SD SZ UG AT BE CH DE DK ES FR GB GR IE IT LU MC NL PT SE BF BJ CF CG CI CM GA GN ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
REG Reference to national code

Ref country code: DE

Ref legal event code: 8642

NENP Non-entry into the national phase

Ref country code: CA

122 Ep: pct application non-entry in european phase
点击 这是indexloc提供的php浏览器服务,不要输入任何密码和下载