FIELD OF THE INVENTION
[0001] The present invention relates to a remote weapon station according to the precharacterising
part of claim 1. The present invention relates, but not limited, to industries making
remotely controlled weapon stations, machine-guns, automatic grenade launchers, missile
firing equipment etc.
BACKGROUND OF THE INVENTION
[0002] Remote weapon stations of the type indicated in the introduction are available on
the market today. A three axes remote weapon station comprises a gun being turnable
about a first transverse axis and a second elevation axis and a sight unit rotatable
about a third elevation axis, wherein the third axis is primary used when firing grenade
launcher type weapons. The four axes weapon stations is provided for that the line
of sight can be controlled independently of the bore axis of the weapon, wherein the
bore axis weapon is stabilised in two axes. However, in such a station according to
prior art the freedom of movement of the sight unit is limited, since the sight unit
must be moved together with the gun, limiting the usage of the sight and weapon station
when the relative speed between the target and the weapon station is high since a
high relative speed requires large offset angles between the line of sight and the
bore axis of the gun in order to hit the target. Also the use of such prior art systems
is limited when the platform on which the weapon station is mounted is performing
a roll motion relative to the bore axis of the gun when the gun is directed to hit
the target. Furthermore prior art weapon stations with three or four axes all make
a change of silhouette when the sight unit and thus the weapon support rotates.
[0003] Known systems having four axes stabilizing arrangements are bulky in width or height.
This since the sight unit is placed above or attached onto the side of the weapon
support. Prior art systems with the sight unit attached onto the side of the weapon,
wherein the concentration of masses asymmetrically will cause the station to be unbalanced,
are also difficult to stabilise without the use of undesired counter weights or larger
and thus heavier drives. Also prior art systems being three axes stabilizing arrangements,
wherein the bore axis of the weapon is stabilised in two axes and the line of sight
line of the sight unit is stabilised in one axis, suffer from the disadvantages that
an image generating sensor (such as TV, IR etc.) field of vision must be adapted for
holding the target within said field of vision, which is extremely difficult when
a vehicle comprising the station is moving since the system must be directed towards
the target for facilitating the determination of the distance to the target, requiring
a long time.
[0004] Prior art systems having four axes arrangement wherein solely the weapon's bore axis
is two axes stabilized, involve that the field of vision must be selected such that
the target remain within the field of vision when the vehicle is moving (roll/pitch/heading).
Also this means that it is difficult to measure the distance to the target when the
vehicle moves, especially when angles for super elevation and lead angles are added
to compensate for relative motion between the target and the weapon station. Furthermore,
prior art systems wherein solely the sight unit's line of sight is two axes stabilized
involve that it is difficult to hit the target with fired ammunition.
[0005] US 5273236 discloses an apparatus provided for designating a plurality of objects within a field
of view and thereafter simultaneously tracking each of the objects. A further document,
US 4576346, describes a seeker head for a target seeking missile, which comprises a seeker adapted
to be directed to a target.
[0006] The object of the present invention is to overcome the drawbacks of known techniques.
SUMMARY OF THE INVENTION
[0007] This has been solved by a remote weapon station being defined in the introduction,
the remote weapon station is characterised by the features of claim's 1 characterising
part.
[0008] In such a way a not bulky remote weapon station is achieved at the same time as the
operator of the remote weapon station is able to perform targeting and surveillance
without changing the remote weapon station's silhouette and thus reducing the risk
of being detected by visual means. The concentration of masses will also be symmetrically
arranged which will make the remote weapon station possible to stabilise without adding
extra weight in the form of undesired counter weights or larger drives. Thereby increase
the usage of the weapon station when the platform on which the weapon station is mounted
is moving. Therby is also achieved a possibility to utilise the sensor without pointing
a gun directly at the object of interest. Also there is a possibility to start searching
for a new target while firing the gun at the first acquired target. A positive effect
is that a weapon station can be provided with a high precision stabilised system having
a sighting function with an unitary installation of a sight unit matching the performance
of the weapon and at the same time providing a sufficient performance for e.g. missile
guidance. Thereby is also achieved that the sight unit in an effective manner can
follow a target by controlling the weapon via a control unit for aiming-off, at the
same time as compensation means provides for compensation of eventual uneven motion
of the remote weapon station, for example being mounted at a gun boat. This is achieved
by that the control unit can control the sight unit independently of the gun aiming
by means of the arrangement of the remote weapon station according to the present
invention. A compact remote weapon station is thus achieved having a sight unit with
a totally independent line of sight relatively the pointing of the gun having the
sight unit correctly balanced relatively the weapon and providing an exact line of
sight. Thus is also achieved a remote weapon station having a sight unit, which weapon
station can be used utilizing the sight unit without the need of other kinds of compensation
for lead angles and/or super elevation.
[0009] Thus, the objects of the invention is to provide a compact remote weapon station,
wherein the assembly permits that the angle between the bore axis of the weapon and
the line of sight of the sight in a controllable manner can be made independently
of each other. The weapon's bore axis being stabilized in two axes and the sight unit's
line of sight being stabilized in two axes.
[0010] The effects being provided by such an arrangement is for example that the target
can be placed in the centre of a image generating display and the distance to the
target continuously can be measured by a laser range finder etc, wherein the weapon's
bore axis can be directed in such a way that the fired ammunition hits the target
with precision. Also is achieved that the bore axis of the weapon and the line of
sight of the sight unit can be oriented relative each other in such a way that the
sight unit can be used without the need of directing the weapon towards the target.
[0011] Also is achieved the advantage that the sight unit's line of sight can be stabilized
and directed with a higher accuracy than being provided by systems only stabilising
the weapon's bore axis.
[0012] Preferably, the weapon support is rotatable about the first transverse axis independently
of the rotatable motion of the sight unit about the third transverse axis such that
the weapon can be directed essentially in another direction relatively the search
direction of the sight unit.
[0013] In such a way is achieved that the weapon can be rotated to the opposite direction
relatively to the sight unit's target tracking(or search) direction. This is also
a beneficial feature for shortening the time when for example a supporting leg of
the weapon carriage covers the line of sight, by controlling the weapon support's
and sight unit's relative rotation.
[0014] Suitably, the weapon support also is arranged to be controlled to rotate about the
first transverse axis dependent upon the rotatable motion of the sight unit about
the third transverse axis.
[0015] Thereby is provided an alternative mode for controlling the weapon support to follow
the sight unit's rotational movement, at the same time as the weapon support can be
disconnected from following the target.
[0016] Suitably, the first axis coincides with the third axis.
[0017] Thereby is provided a remote weapon station being capable to utilize a compact motor
driving system using the same axis for the transverse rotations.
[0018] Preferably, the sight unit comprises a first essentially spherical, hollow body which
interacts with a second essentially rotationally symmetrical body, both bodies being
rotatable in relation to one another about the transverse axis, the spherical body
accommodating at least one electro-optical sensor, being rotatable about the fourth
elevation axis.
[0019] Thus is also achieved that the sight unit can be independently stabilised, thereby
making the remote weapon station optimized for high precision sensor systems, e.g.
laser illumination at long ranges. The use of a sensor sight system with a spherical
form arranged in the remote weapon station provides independent 360° traverse operation
with an optimal configuration of the remote weapon station with regard to overall
volume, interior sensor volume utilisation, ballistic protection, signature management,
and weapon dumping/elevation angles.
[0020] Alternatively, the weapon support comprises a tiltable leg arrangement supporting
the weapon attachment device, the leg arrangement being tiltable over the first essentially
spherical, hollow body.
[0021] In such a way the remote weapon station can be made lower for transportation purposes
by tilting the weapon attachment device over the sight unit. The tilting action performing
an imaginary circular arc essentially with the same radius as the radius of the first
essentially spherical, hollow body.
[0022] Preferably, the sight unit comprises a first essentially cylindrical, hollow body
accommodating at least one electro-optical sensor.
[0023] Thereby is achieved a large volume for sight equipment even still performing an optimal
signature management, that is having essentially the same silhouette independently
the sensor transverse motion about the third axis.
[0024] Alternatively, the hollow body encloses all interior movable parts, such as electro-optical
sensors, of the sight unit for hiding said parts. The body is preferably armour cased
and transparent and/or partly transparent.
[0025] In such a way, on one hand the interior equipment is protected from splinters, small
arms fire or ricochets etc., and on the other hand hidden from being detected by the
object/target.
[0026] Alternatively, the weapon support being comprised in a motorized gun control system.
[0027] Thereby is achieved that the remote weapon station is applicable to an available
platform, such as a truck, an armoured car, gun boat, tank, helicopter etc.
[0028] Suitably, the sight unit is arranged for controlling at least one weapon disposed
at a distance from the remote weapon station.
BRIEF DESCRIPTION OF THE DRAWINGS
[0029] The present invention will now be described by way of example with reference to the
accompanying schematic drawings of which:
FIG. 1a schematically illustrates a remote weapon station in a front view,
FIG. 1b schematically illustrates the station in FIG. 1a in a side view,
FIG. 1c schematically illustrates the station in FIG. 1a in a plane view,
FIGS 2a-2c schematically illustrate the station in FIG. 1c in motion,
FIGS. 3a-3c schematically illustrate a remote weapon station according to a second
embodiment,
FIGS 3d-3f schematically illustrate a remote weapon station according to a further
embodiment,
FIG. 4 schematically illustrates parts of a sight unit shown in FIGs 1a-2c,
FIGS. 5a-5b schematically illustrate a leg arrangement of a remote weapon station,
FIG. 6 schematically illustrates a motor driving system of the remote weapon station
in FIG. 4, and
FIG. 7 schematically illustrates the aiming of the remote weapon station at a moving
target.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0030] Hereinafter, embodiments of the present invention will be described in detail with
reference to the accompanying drawings related to the embodiments, wherein for the
sake of clarity and understanding of the invention some details of no importance are
deleted from the drawings.
[0031] Referring to FIGS. 1a, 1b, 1c, a remote weapon station 1 is schematically illustrated.
The remote weapon station 1 is mountable onto a gun boat (not shown) or the like.
The remote weapon station 1 comprises a weapon support 3 adapted for rotatable motion
about a first transverse axis X1.
[0032] The weapon support 3 supports a weapon attachment device 5 being rotatable about
a second elevation axis X2. The second elevation axis X2 comprises an U-shaped part
7 for accommodation of a gun 9. The gun 9 is mounted onto the weapon attachment device
5, such as a bayonet fitting (not shown) connected to the second elevation axis X2,
wherein the gun 9 easily can be disconnected from the weapon attachment device 5.
[0033] The weapon support 3 supports two legs 11 extending from a platform 13 of the weapon
support 3, which platform 13 being rotatable about the axis X1. Between the legs 11
and at their upper ends 15 is the U-shaped part 7 mounted. One of the legs 11 accommodates
an ammunition belt guide (not shown).
[0034] The remote weapon station 1 comprises a sight unit 17 for observation of the surroundings
and for measuring in a detected target, tracking, classifying the type of target,
identifying the target etc. The sight unit 17 is rotatable about a third transverse
axis X3 and about a fourth elevation axis X4. The sight unit 17 has at least one electro-optical
sensor 19 with associated apertures 21 arranged in the sight unit's 17 spherical hollow
body 23. The sight unit 17 is mounted between the weapon support 3 (platform or fundament)
and the weapon (gun) attachment device 5, whereby is achieved a compact remote weapon
station 1 having a sight unit 17 with a totally independent line of sight relatively
the bore axis of the gun 9. It also means that the sight unit 17 can be correctly
stabilized/directed relatively the gun 9 and providing an exact line of sight. Since
the gun 9 is dispensed in a vertical plane comprising the first transverse axis X1
and essentially the third transverse axis X3, an optimal aiming can be achieved. A
control unit 25 is arranged remote from the weapon station 1 and is adapted to control
a weapon driving means 27 for rotating the gun 9 about the first transverse axis X1
and the second elevation axis X2 and also to control a sight unit driving means 29
for rotation about the third transverse axis X3 and the fourth elevation axis X4.
By arranging the sight unit 17 between the weapon support 3 (fundament or platform)
and the weapon (gun 9) cables and wires can be hidden and protected and easy to mount
during the manufactory of the station.
[0035] In FIGS. 2a, 2b, 2c are shown in a plane view the remote weapon station 1 performing
a sight unit rotation towards a target/object 31 while pointing the gun 9 in a somewhat
opposite direction. In FIG. 2a both the gun 9 and the sight unit 17 are directed in
the same direction. In FIG. 2b the sight unit 17 has started it's rotation r for localising
the target 31 without pointing the gun 9 at the target 31. In some cases this performance
can be beneficial since pointing a gun at an object may result in a non-desirable
reaction.
[0036] Meanwhile the sight unit 17 rotates, the sight unit's 17 sensors 19 perform a scanning
of the surroundings. In FIG. 2b is shown how the sight line L will be covered by one
of the legs 11 of the weapon support 3. This problem is partly solved by using e.g.
two sensors or two in pair arranged sensors 19, such as one TV- and one IR-sensor
or two in pair arranged TV- and IR-sensors. Meanwhile the first sensor or pair of
sensors observes the surroundings, the second sensor or pair of sensors instantaneously
will lose contact with the target 31 since the sight line L is covered by the leg
11. When the first sensor or pair of sensors has lost contact with the target 31,
the second sensor or pair of sensors pick up the line of sight to the target L. For
even more shortening the time, when the leg 11 covers the sensors 19, the control
unit 25 (see FIG. 1a) controls the weapon support 3 to rotate in an opposite direction
marked with arrow r2, see FIG. 2c (an overlapping function). For even better visibility
of the sensors 19, the legs 11 can be arranged as a system of framework. For protection
of the sensors the apertures and sensors can be parked occasionally behind one of
the legs 11.
[0037] The sight unit 17 is rotatable about the third transverse axis X3 and about, perpendicular
to the third axis X3, the fourth elevation axis X4, independently of the position
or rotation of the weapon support 3 about the first transverse axis X1 and the second
elevation axis X2. By using a spherical hollow body 23 embodying the sight sensors
19, an independent 360° traverse operation of the sight unit 17 is possible without
moving the gun 9, wherein the silhouette of the remote weapon station 1 not being
changed, thus minimizing the risk of being detected by the object/target 31 by visual
means.
[0038] Whereas the FIGS. 1 and 2 show a sight unit 17 comprising an spherical hollow body
23 embodying the sensors 19, as an alternative the sight unit 17 may comprise a first
essentially cylindrical or cubical, hollow body 23 accommodating at least one electro-optical
sensor 19. Such an embodiment is shown in FIGS. 3a, 3b, 3c. Thereby is achieved a
large volume for sight equipment even still performing an optimal signature management,
that is having essentially the same silhouette independently of the sensor transverse
motion about the third axis X3. The FIG. 3c shows the sight unit 17 directed to the
opposite direction relatively the gun 9 in a horizontal action.
[0039] The embodiment of FIGS. 3a, 3b, 3c is arranged such that the first transverse axis
X1 coincides with the third transverse axis X3 of the sight unit 17, whereby is provided
a remote weapon station 1 being capable to utilize a compact motor driving system
using the same axis for the transverse rotations as being described below with reference
to FIG. 6.
[0040] A cylindrical hollow body 33 encloses all interior movable parts, such as electro-optical
sensors, of the sight unit for protecting said parts. The body is transparent and
armour cased. In such a way, on one hand the interior equipment is protected from
splinters, small arms fire or ricochets etc., and on the other hand hidden from being
detected by the object/target.
[0041] In FIG. 4 is shown the sight unit 17 in FIGS. 1a, 1b, 1c more in detail. The sight
unit 17 comprises an essentially spherical body 23 adjacent to one end of a rotationally
symmetrical body 35, preferably of circular cylindrical shape. The spherical body
23 comprises a circular central section 37 surrounded by two peripheral half sections
39 on each side (only one section 39 is illustrated with broken line). Each peripheral
half section is provided with two apertures 21. Of course can according to other embodiments
the sections each only have one aperture.
[0042] The spherical hollow body 23 is rotatable in relation to the rotationally symmetrical
body 35 about the third transverse axis X3. By the rotation about the third transverse
axis X3 it is possible to bring about 360° rotation. The two peripheral half sections
39 are rigidly mechanically interconnected and arranged rotatable so as to be capable
of being rotated about the fourth elevation axis A4. The elevation can be limited
to a range wherein the apertures 21 are in one end position oriented at an angle downwards
relative to the horizontal plane and, in the other end position, oriented at an angle
upwards relative to the horizontal plane.
[0043] The electro-optical sensors 19 can be selected from a variety of sensors, e.g. TV,
IRV, laser rangefinder and laser illuminator.
[0044] The use of the sight unit 17 with a spherical form arranged in the remote weapon
station 1 provides independent 360° traverse operation with an optimal configuration
of the remote weapon station 1 with regard to overall volume, interior sensor volume
utilisation, ballistic protection, signature management, and weapon dumping/elevation
angles.
[0045] In FIG. 5a and 5b are shown an embodiment of the remote weapon station 1, wherein
the weapon support 3 comprises a tiltable leg arrangement 41 supporting the weapon
attachment device 5. The leg arrangement 41 comprises two legs 11 being tiltable about
a tilting point p over the essentially spherical, hollow body 23 being also shown
in FIG. 4. In such a way the remote weapon station 1 can be made lower for transportation
purposes by tilting the weapon attachment device 5 over the sight unit 17. The tilting
action of the weapon attachment device 5 over the sight unit 17 performs an imaginary
circular arc c essentially with the same radius as the radius of the circumference
of the essentially spherical, hollow body 23. Thereby is achieved that the remote
weapon station 1 can be made lower in a transportation mode without the need of making
the volume of the sight equipment smaller.
[0046] In FIG. 6 is schematically illustrated a compact motor driving system 43 using the
same axis X1, X3 for the transverse rotations of both the sensor unit 17 and the weapon
support 3. The first axis X1 coincides with the third axis X3. A first rotor 45 is
arranged rotatable about the common transverse axis X1 and X3 and is connected to
the legs 11 of the weapon support 3 and via a first bearing 47 connected to the weapon
carrier 49, such as a gun boat.
[0047] A first stator 51 actuates the first rotor 45 for transverse rotation of the gun
9. A further second bearing 53 is arranged between the first rotor 45 and a second
rotor 55 carrying the circular central section 37, within which the electro-optical
sensors 19 are rotatable arranged for elevation rotation about the fourth elevation
axis X4. A second stator 57 actuates the second rotor 55 for the transverse rotation
of the circular central section 37 and the peripheral sections (not shown) of the
sight unit 17.
[0048] In FIG. 7 is shown schematically the aiming of the remote weapon station 1 at a moving
target 31. The gun's 9 pointing direction and the sight line L of the sight unit 17
is broken for sake of clarity and the target 31 is drawn smaller than the remote weapon
station 1 for the sake of illustration. An aiming-off angle α is required as the target
31 is moving. The compact remote weapon station's 1 sight unit 17 detecting the target
31 is rotated independently of the gun's 9 motion. By means of the control unit 25
is estimated the required aiming-off angle α, dependent upon the velocity of the target
31 and eventually the velocity of the carrier carrying the remote weapon station 1.
Also parameters as wind direction and speed etc. are considered. An uniaxial rate
gyro is stabilizing the gun 9 via an elevation drive unit 27 and a transverse drive
unit arranged at the second elevation axis X2 and the transverse axis, and the electro-optical
sensors 19 are stabilized via a sensor unit elevation drive system (not shown) of
an elevation drive system and transverse drive system arranged within the circular
central section 37 of the sight unit 17.
[0049] The remote weapon station 1 is according to one embodiment of the invention provided
with a weapon support 3 being comprised in a motorized gun control system. Thereby
is achieved that the remote weapon station 1 is applicable to an available carrier,
such as a truck, car, gun boat, tank, helicopter etc.
[0050] The sight unit 17 of the remote weapon station 1 can control at least one separate
weapon 60 placed at a distance from the remote weapon station 1.Control is achieved
by means of being directly connected to the weapon, illuminating the target for the
weapon or providing in-the-air guidance to the weapon or a combination of any of these
means.
[0051] The invention is not limited to a specific embodiment herein, but may also consist
of several combinations of the presented embodiments. For example, only one peripheral
half section can provide an aperture and none in the other section. Alternatively,
the elevation drive system and transverse drive system may be arranged in one of the
supports of the sight unit. For example, the sight unit's hollow body can have a central
section being rotatable and two outer section acting as supports (fork-shaped assembly)
or the section being supported by only one peripheral support. Of course, the sigh
unit may be placed between the weapon support and the weapon attachment device by
mounting the sight unit "hanging" under the weapon attachment device or adjacent the
same.
1. A remote weapon station comprising a weapon support (3) adapted for rotatable motion
about a first transverse axis (X1), the weapon support (3) supporting a weapon attachment
device (5) being rotatable about a second elevation axis (X2), the remote weapon station
(1) comprises a sight unit (17), characterised in that the sight unit (17) is rotatable about a third transverse axis (X3) and about, perpendicular
to the third transverse axis, a fourth elevation axis (X4), independently of the position
or rotation of the weapon support (3) about the first transverse axis (X1) and the
second elevation axis (X2), and the sight unit (17) is mounted between the weapon
support (3) and the weapon attachment device (5).
2. The remote weapon station according to claim 1, wherein the weapon support (3) is
rotatable about the first transverse axis (X1) independently of the rotatable motion
of the sight unit (17) about the third transverse axis (X3) such that the weapon (9)
can be directed in essentially another direction relatively the line of sight of the
sight unit (17).
3. The remote weapon station according to any of claims 1 or 2, wherein the weapon support
(3) also is arranged to be controlled to rotate about the first transverse axis (X1)
dependent upon the rotatable motion of the sight unit (17) about the third transverse
axis (X3).
4. The remote weapon station according to any of the preceding claims, wherein the first
axis (X1) coincides with the third axis (X3).
5. The remote weapon station according to any of the preceding claims, wherein the sight
unit (17) comprises a first essentially spherical, hollow body (23) electro-optical
sensor 19), the sensor (19) is rotatable about the fourth elevation axis (X4).
6. The remote weapon station according to claim 5, wherein the weapon support (3) comprises
a tiltable leg arrangement (41) supporting the weapon attachment device (5), the leg
arrangement (41) being tiltable over the first essentially spherical, hollow body
(23).
7. The remote weapon station according to any of claims 1-4, wherein the sight unit (17)
comprises a first essentially cylindrical, hollow body (33) accommodating at least
one electro-optical sensor (19).
8. The remote weapon station according to any of the preceding claims, wherein an essentially
transparent hollow body (23, 33) encloses all interior movable parts, such as electro-optical
sensors, of the sight unit (17) for protecting and hiding said parts.
9. The remote weapon station according to any of the preceding claims, wherein the weapon
support (3) being comprised in a gun control system.
10. The remote weapon station according to any of the preceding claims, wherein the sight
unit (17) is adapted for controlling/guiding at least one weapon (60) disposed at
a distance from the remote weapon station (1).