CN109398709A - External fire control system and application method - Google Patents
External fire control system and application method Download PDFInfo
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- CN109398709A CN109398709A CN201811468076.1A CN201811468076A CN109398709A CN 109398709 A CN109398709 A CN 109398709A CN 201811468076 A CN201811468076 A CN 201811468076A CN 109398709 A CN109398709 A CN 109398709A
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- 238000000034 method Methods 0.000 title claims abstract description 25
- 238000007726 management method Methods 0.000 claims abstract description 123
- 238000004891 communication Methods 0.000 claims abstract description 26
- 230000006855 networking Effects 0.000 claims abstract description 8
- 238000013439 planning Methods 0.000 claims abstract description 7
- 238000002360 preparation method Methods 0.000 claims description 26
- 238000010304 firing Methods 0.000 claims description 16
- 238000012360 testing method Methods 0.000 claims description 11
- 230000005540 biological transmission Effects 0.000 claims description 9
- 239000000725 suspension Substances 0.000 claims description 8
- 238000004364 calculation method Methods 0.000 claims description 4
- 230000003993 interaction Effects 0.000 claims description 4
- 230000004044 response Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 13
- 230000006978 adaptation Effects 0.000 abstract description 4
- 238000013461 design Methods 0.000 description 9
- 230000008569 process Effects 0.000 description 5
- 230000005611 electricity Effects 0.000 description 4
- 230000010354 integration Effects 0.000 description 4
- 241000208340 Araliaceae Species 0.000 description 2
- 235000005035 Panax pseudoginseng ssp. pseudoginseng Nutrition 0.000 description 2
- 235000003140 Panax quinquefolius Nutrition 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 235000008434 ginseng Nutrition 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000003032 molecular docking Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000003786 synthesis reaction Methods 0.000 description 2
- 238000012384 transportation and delivery Methods 0.000 description 2
- 239000011469 building brick Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
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- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012857 repacking Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bomb doors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B15/00—Systems controlled by a computer
- G05B15/02—Systems controlled by a computer electric
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/02—Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Selective Calling Equipment (AREA)
Abstract
This application discloses a kind of external fire control systems, comprising: and general bomb rack is removably attached to aircraft exterior to be adapted to, meanwhile, general bomb rack controlled is launched weapon for hanging weapon to be carried；Control management subsystem, is removably attached to aircraft exterior to be adapted to, and is configured to equipment by wireless communication and receives manipulation instruction and/or data information, and controls weapon and launched；Ground-based mission management equipment, treats adaptation aircraft and weapon carries out ground-based mission planning, and generates preplanned mission data and configuration parameter；Wireless controlling equipment, for sending manipulation instruction, generating aircraft type and hanging point quantity and carrying out networking configuration.Disclosed herein as well is a kind of external fire control system application methods.The external fire control system of the application is the independent fire control system of a set of external, can fast implement different operational aircrafts to the installation and use demand of weapon.
Description
Technical field
The application belongs to operational aircraft Weapon Fire-Control-System development and design and adds repacking field, in particular to a kind of external
Fire control system and application method.
Background technique
In traditional operational aircraft use process, pilot is directly by the matched air weapon fire control of aircraft itself
System realizes controling and useing to weapon, for example, the weapon type of control and display aircraft institute carry, hanging point position and
The information such as quantity, weapon working condition.
And for some external fire control systems, it is two sets complete with traditional fire control system
Mutually independent control, display system, this either manipulates the still use to weapon to aircraft for pilot,
It is all a huge challenge.
Thus, it is desirable to have a kind of technical solution overcomes or at least mitigates at least one drawbacks described above of the prior art.
Summary of the invention
The purpose of the application there is provided a kind of external fire control system and application method, with solve it is above-mentioned extremely
The problem of few one side.
In a first aspect, this application discloses a kind of external fire control systems, comprising:
General bomb rack, the general bomb rack are removably attached to aircraft exterior to be adapted to, meanwhile, the general extension
Firing mount controlled is launched the weapon for hanging weapon to be carried；
Control management subsystem, the control management subsystem are removably attached to the aircraft exterior to be adapted to, institute
It states control management subsystem and is configured to equipment reception manipulation instruction and/or data information by wireless communication, and referred to according to manipulation
It enables and/or data information carries out corresponding manipulation, the weapon is launched including the general bomb rack is controlled；
Ground-based mission management equipment, the ground-based mission management equipment, which is used to be in ground in the aircraft to be adapted to, to be prepared
When the stage, ground-based mission planning is carried out to the aircraft to be adapted to and the weapon, and generate preplanned mission data and configuration
Parameter；
Wireless controlling equipment, the wireless controlling equipment send the behaviour to control management subsystem for controlled
Control instruction and/or data information, the preplanned mission data for being also used to be generated according to the ground-based mission management equipment and configuration ginseng
Number configures corresponding aircraft type and hanging point quantity, and with the wireless telecom equipment in the control management subsystem that matches into
Row networking configuration.
According at least one embodiment of the application, the top structure of the general bomb rack, be configured to it is described to
The suspension interface of adaptation aircraft hanging point level-one hanger is adapted, and fixation is suspended on level-one hanger lower part, the general extension bullet
Frame is configured with bomb shackle compatible with the weapon.
According at least one embodiment of the application, the control management subsystem includes:
Weapon management module, the weapon management module receive the wireless controlling equipment by the wireless telecom equipment
The manipulation instruction and/or data information of transmission, and corresponding behaviour is carried out to the weapon according to manipulation instruction and/or data information
Control launches the weapon including the general bomb rack is controlled；
Power-supply device, the power-supply device are used for as the weapon management module, wireless telecom equipment and described general
Bomb rack power supply.
According at least one embodiment of the application, the control management subsystem includes:
Navigation equipment, the navigation equipment are connect with the weapon management module；
Satellite signal receiving antenna, the satellite signal receiving antenna respectively with the weapon management module and the navigation
Equipment connection；Wherein
The weapon management module is configured to according to receiving aligned instructions or navigation instruction, control the navigation equipment into
Enter alignment or navigational state；
The wireless controlling equipment refers to for controlled to the weapon management module transmission aligned instructions or navigation
It enables；
The power-supply device is connect with the navigation equipment, for powering for the navigation equipment.
According at least one embodiment of the application, the navigation equipment is inertia/combinations of satellites navigation equipment.
According at least one embodiment of the application, the weapon management module includes:
Upper electric unit, the upper electric unit receive the upper of the wireless controlling equipment transmission by the wireless telecom equipment
Electricity instruction, and be that the weapon is powered on according to the instruction control power-supply device that powers on；Wherein
The wireless controlling equipment powers on instruction to described in weapon management module transmission for controlled.
According at least one embodiment of the application, the weapon management module includes:
Preparatory unit, the preparatory unit receive the standard that the wireless controlling equipment is sent by the wireless telecom equipment
Standby instruction, and controlled according to the preparation instruction and prepare to operate before the weapon is emitted；
Parameter stapling unit, the parameter stapling unit receive the force that the controlling equipment is sent by the communication equipment
Device operational version and target data binding instructio, and target data is carried out to the weapon according to the target data binding instructio
The wireless controlling equipment of stapling operation parameter stapling unit parameter stapling unit；
Emit solving unit, the transmitting solving unit completes weapon attacking envelope curve and launching condition resolves, and ties resolving
Fruit is reported to the controlling equipment by the communication equipment, while receiving the firing order that the controlling equipment is sent, and root
It is single that the dispensing operation transmitting solving unit transmitting resolving that the suspension arrangement is completed to the weapon is controlled according to the firing order
First wireless controlling equipment；
The wireless controlling equipment is for controlled to the weapon management module sends the preparation instruction, weapon uses
Scheme, target data binding instructio and firing order.
According at least one embodiment of the application, the weapon management module includes:
State reporting unit, the state reporting unit are used for the weapon management module in response to the wireless manipulation
State when equipment manipulation instruction reports to the wireless controlling equipment by the wireless telecom equipment (31).
According at least one embodiment of the application, the control management subsystem is fixed at the general extension bullet
Inside frame.
Second aspect, this application discloses a kind of external fire control system application method, including it is winged wait be adapted to
Preparation process and mission phase step before machine takes off, wherein
It is described take off before preparation process include:
S10 step: ground-based mission management equipment carries out ground-based mission planning, Yi Jisheng to the aircraft to be adapted to and weapon
At preplanned mission data and configuration parameter；
S11 step: according to the task data and configuration parameter complete to wireless controlling equipment, control management subsystem with
And prepare operation before the taking off of weapon；
The mission phase step includes:
S20 step: weapon to be launched is determined by the wireless controlling equipment；
S21 step: subsystem and described is managed by the wireless controlling equipment and wireless telecom equipment and the control
Weapon carries out manipulation instruction and/or data information interaction；
S22 step: control management subsystem according to manipulation instruction control the general bomb rack to the weapon into
Row is launched.
According at least one embodiment of the application, the S11 step includes:
S111 step: the wireless controlling equipment carries out parameter configuration according to ground configuration parameter；
S112 step: the wireless controlling equipment after the completion of parameter configuration is according to the task data and configuration parameter pair
Corresponding aircraft type and hanging point quantity are configured；
S113 step: the wireless controlling equipment by the wireless telecom equipment with match it is single or multiple other
The wireless telecom equipment carries out networking configuration；
S114 step: equipment will be sent to control pipe to the wireless controlling equipment to target of attack parameter by wireless communication
It manages subsystem and carries out target information configuration；
S115 step: aligned instructions, the weapon management are sent to weapon management module by the wireless controlling equipment
Module controls navigation equipment according to the aligned instructions and enters inertial navigation alignment；
S116 step: sending weapon to the weapon management module by the wireless controlling equipment and power on instruction, described
Weapon management module powers on instruction according to the weapon and carries out power on operation to the weapon, and the weapon after powering on is completed
It is described to take off preceding preparation process completion wait be adapted to after power-on self-test operation.
According at least one embodiment of the application, between the S113 step and S114 step, further includes:
S1131 step: the state reporting unit by wireless communication equipment by the ID of the general bomb rack and force
Device carry location information reports to the wireless controlling equipment.
According at least one embodiment of the application, the weapon described in the S116 step after powering on is complete
After being operated at power-on self-test, further includes:
S1161 step: equipment will be in the self-test status information of the weapon by wireless communication for the state reporting unit
It reports to the wireless controlling equipment.
According at least one embodiment of the application, the S21 step includes:
S211 step: aligned instructions, the weapon are sent to the weapon management module by the wireless controlling equipment
Management module controls the weapon according to the aligned instructions and enters alignment；
S212 step: preparation instruction, the weapon are sent to the weapon management module by the wireless controlling equipment
Management module is controlled according to the preparation instruction to be prepared to operate before the weapon is emitted；
S213 step: weapon application scheme and target are sent to the weapon management module by the wireless controlling equipment
Data binding instructio, the weapon management module carry out target data dress to the weapon according to the target data binding instructio
Order operation；
S214 step: firing order is sent to the transmitting solving unit by the wireless controlling equipment.
At least there are following advantageous effects in the application:
The external fire control system and application method of the application passes through single wireless control apparatus comprehensive integration
Multiple independent external Weapon Fire-Control-Systems and weapon information realize that " people exists for automation control management process and key signal
The safety Design of ring ", the comprehensive function for being based on " key operation " are shown, can flexibly realize that system function operates
Switching, significantly reduces the operating burden of pilot, has good scalability and versatility.
Detailed description of the invention
Fig. 1 is the system composition block diagram of the application external fire control system；
Fig. 2 is the flow chart of the application external fire control system application method.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application implementation clearer, below in conjunction in the embodiment of the present application
Attached drawing, technical solutions in the embodiments of the present application is further described in more detail.In the accompanying drawings, identical from beginning to end or class
As label indicate same or similar element or element with the same or similar functions.Described embodiment is the application
A part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to use
In explanation the application, and it should not be understood as the limitation to the application.Based on the embodiment in the application, ordinary skill people
Member's all other embodiment obtained without creative efforts, shall fall in the protection scope of this application.Under
Face is described in detail embodiments herein in conjunction with attached drawing.
In the description of the present application, it is to be understood that term " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown is merely for convenience of description the application and simplifies description, rather than the dress of indication or suggestion meaning
It sets or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as protecting the application
The limitation of range.
1 to Fig. 2 the application external fire control system and application method are done further in detail with reference to the accompanying drawing
It describes in detail bright.
This application discloses a kind of external fire control systems, may include general bomb rack 1, control management point
System 3, ground-based mission management equipment 5 and wireless controlling equipment 4.
General bomb rack 1 is removably attached to aircraft exterior to be adapted to, meanwhile, general bomb rack 1 is for hanging wait take
The weapon 2 of load, and controlled launch weapon 2.
Control management subsystem 3 is removably attached to aircraft exterior to be adapted to, and control management subsystem 3 is configured to pass through
Wireless telecom equipment 31 receive manipulation instruction (may include such as powering on instruction, firing order) and/or data information (such as
Weapon application scheme information), and according to manipulation instruction and/or data information carry out corresponding manipulation (such as subsequent alignment, on
The manipulations such as electricity, dispensing, target data bookbinding)；Here, manipulation includes to weapon 2 and other equipment such as inertial navigation equipment；Cause
This, launches weapon 2 including general bomb rack 1 is controlled.
Ground-based mission management equipment 5 is used for when being in the ground preparation stage wait be adapted to aircraft, treats adaptation aircraft and force
Device carries out ground-based mission planning, and generates preplanned mission data (can be for example including to target of attack parameter) and configuration ginseng
Number.
Wireless controlling equipment 4 sends manipulation instruction to control management subsystem 3 for controlled, is also used to be appointed according to ground
The preplanned mission data and configuration parameter that management equipment 5 of being engaged in generates configure corresponding aircraft type and hanging point quantity, Yi Jiyu
Wireless telecom equipment 31 in the control management subsystem 3 of aircraft that matches carries out networking configuration.
It should be noted that above-mentioned control manages subsystem 3 and leads in the external fire control system of the application
It is usually to correspond with each hanging point of aircraft with bomb rack 1, i.e. one control of setting manages subsystem 3 and controls at a hanging point
Weapon 2 on one general bomb rack 1.And ground-based mission management equipment 5 and the quantity of wireless controlling equipment 4 can according to need
Suitable setting is carried out, ground-based mission management equipment 5 can be used as a platform, and more aircrafts share.Wireless controlling equipment 4 can be with
It is that multiple controls management subsystem 3 on the same aircraft shares one, i.e., is realized by a wireless controlling equipment 4 and respectively
A independent external fire control system synthesis display of hanging point and control management.
The external fire control system of the application, can be multiple solely by single wireless control apparatus comprehensive integration
Vertical external Weapon Fire-Control-System and weapon information realizes the peace of automation control management process and key signal " people is in ring "
Full property design；Also, the system can fast implement different operational aircrafts with the original Weapon Fire-Control-System concurrent working of aircraft
To the installation and use demand of weapon, the normal work and fight capability for not influencing original machine system after installation are played.
Further, the top structure of general bomb rack 1 is configured to connect with the suspension of aircraft hanging point level-one hanger to be adapted to
Mouth is adapted, fixed to be suspended on level-one hanger lower part, and general bomb rack 1 is configured with bomb shackle compatible with weapon 2.
Further, in some alternative embodiments, general bomb rack 1 is internally provided with installation space, control pipe
Each equipment in reason subsystem 3 is all fixedly disposed in the installation space of general bomb rack 1；Wherein, installation space (or peace
Behave affectedly body) quantity, size, structure suitable setting can be carried out according to the specific pre- equipment that accommodates.General bomb rack 1 is military
The installation carrying platform of device/hanger and system equipment, for aircraft hanging point interface dock and hang deliver weapon delivery/hang
Object is hung, for installing power-supply device (battery), control management equipment (weapon fire control computer), sensor (inertial navigation/satellite group
Close navigation equipment) etc. equipment.At this point, hanging rack structure need to have enough intensity and toughnesses and profile space, to meet mounting arrangements
Bomb shackle, system equipment and suspension deliver weapon delivery/hanger demand, and interface need to have and different form aircraft one on hanger
The general-purpose interface ability of grade hanger interface docking, bomb shackle are hung away from or compound are hung away from (hanging away from optional with structure type) shape using single
Formula, to meet the docking of distinct interface weapon/hanger and suspension dispensing demand.
Further, control management subsystem 3 may include weapon management module 32, navigation equipment 34 and satellite-signal
Receiving antenna 35 (such as GPS antenna).
Weapon management module 32 equipment 31 can receive the manipulation instruction that wireless controlling equipment 4 is sent by wireless communication
And/or data information, and corresponding manipulation is carried out to weapon 2 according to manipulation instruction and/or data information, it is logical including control
The weapon 2 is launched with bomb rack 1.
Wherein, weapon management module 32 can be weapon Fire control calculation machine equipment；Weapon fire control computer is using miniaturization
Highly integrated technology, mainly by cabinet, computer module, bus communication module, acquisition and recording module, wireless radiofrequency module, from
The composition such as interface module, power supply and monitoring module, bus mother board is dissipated, software uses open architecture and modularized design, can expand
Exhibition ability is strong.The functions of the equipments can be merged into portable radio controller and battery feed when necessary.
Power-supply device 33 is used to power for weapon management module 32, wireless telecom equipment 31 and general bomb rack 1.Its
In, power-supply device 33 can be set using known a variety of suitable battery or powers, in the present embodiment, preferably battery feed；
Battery feed is mainly by groups such as single battery group, shell mechanism, jumper, electric connector, breaker, insulating layer and fasteners
At using real time monitoring and quick despatch interface, between long cruise duration, resistance to wide mild complex work environment, maintenance period
Every long the features such as.
The quantity of navigation equipment 34 is one, is connect with weapon management module 32.Further, preferably navigation equipment 34 is used
Property/combinations of satellites navigation equipment, be mainly made of cabinet, inertia sensing assembly and electronic building brick three parts, have pure inertia and
The combinations of satellites navigation mode of operation such as GPS, Beidou has high-precision position, speed, posture information for providing.
The quantity of satellite signal receiving antenna 35 is one, is connect respectively with weapon management module 32 and navigation equipment 34；
Satellite signal receiving antenna 35 is for receiving repeater satellite signal to inertia/combinations of satellites navigation equipment and weapon management module
32, have GPS and Big Dipper satellite signal receives ability.
Wherein, weapon management module 32 is configured to control navigation equipment according to the aligned instructions or navigation instruction that receive
34 enter alignment or navigational state.Correspondingly, wireless controlling equipment 4 is for controlled to the transmission pair of weapon management module 32
Quasi instruction or navigation instruction.Further, above-mentioned power-supply device 33 can also be connect with navigation equipment 34, to be navigation equipment 34
Power supply.
Further, weapon management module 32 may include upper electric unit, preparatory unit, parameter stapling unit, transmitting again
Solving unit and state reporting unit.
Upper electric unit equipment 31 can receive the instruction that powers on that wireless controlling equipment 4 sends by wireless communication, and according to
Powering on instruction control power-supply device 33 is that weapon 2 is powered on；Wherein, wireless controlling equipment 4 is for controlled to weapon management
The transmission of module 32 powers on instruction.
Preparatory unit equipment 31 can receive the preparation instruction that wireless controlling equipment 4 is sent by wireless communication, and according to
Preparation instruction control weapon 2 prepares operation before being emitted.
Parameter stapling unit equipment 31 can receive the weapon application scheme that wireless controlling equipment 4 is sent by wireless communication
With target data binding instructio, and according to target data binding instructio to weapon 2 carry out target data stapling operation.
Transmitting solving unit can complete weapon attacking envelope curve and launching condition resolves, and calculation result is passed through communication equipment
31 are reported to controlling equipment 4, while receiving the firing order of the transmission of controlling equipment 4, and control suspension arrangement 1 according to firing order
The dispensing to weapon 2 is completed to operate.
Wherein, wireless controlling equipment 4 sends preparation instruction, target data bookbinding to weapon management module 32 for controlled
Instruction and firing order.
State reporting unit can be used for weapon management module 32 in response to wireless 4 manipulation instruction of controlling equipment and/or
State when data information, equipment 31 reports to wireless controlling equipment 4 by wireless communication.
In the external aircraft mounted control system of the application, weapon management module 32 (i.e. weapon fire control computer) is control core
The heart has the satellite navigation informations such as GPS, Beidou and receives processing capacity, navigates respectively with battery feed, inertial navigation/combinations of satellites
The crosslinking such as equipment, wireless controlling equipment 4 (i.e. portable radio controller), by carrying out information friendship with portable radio controller
Mutually, it completes to report the logic controls such as the power supply of weapon, alignment, resolving, transmitting, weapon switching, hanging point switching and status display.
Further, wireless controlling equipment 4 can be plate, mobile phone in such as portable intelligent wireless display control terminal
Deng correspondingly, wireless telecom equipment 31 is wireless telecom equipment, such as wireless router, radio antenna.It is some can
In the embodiment of choosing, portable intelligent wireless display control terminal is integrated with miniaturization board and wireless antenna, working frequency range
It can set adjustable, be worked at the same time with 24 wireless controllers may be implemented in region, single wireless controller can be same with signal strength
Time control tubulation manages 10 wireless communication terminals；Using anti-emergency light reflex touch display screen, mode round the clock is supported, it can under strong sunlight
Depending on；Work rechargeable battery when long using small-sized efficient, and the working time is not less than 4 hours.It is electric with being realized by physical button
The functions such as source switch, screen locking, arm discharge, jury launch.The four limbs or cockpit in people can be reliably fixed by modes such as bandages
On equipment mounting frame, have the characteristics that small-sized, portable, image clearly, processing capacity are strong.
Also, self-powered ability when wireless controlling equipment 4 has long, by between antenna and system weapon fire control computer
Wireless communication is established, it is aobvious to provide the important informations such as system mode, weapons status, attack situation, attack area for pilot/operator
Show and resolve, the human/machine control interfaces such as weapon power supply, Transfer Alignment, arm discharge and emergency firing order are provided.
So as to be realized by a portable radio controller and the independent external air weapon of each hanging point
Fire control system carries out data interaction, obtains the working condition of each system and power-up, alignment, preparation, the fire control of each hanging point weapon
The relevant informations such as resolving, for synthesis display and control management.In addition, in the man-machine interface design side of portable radio controller
Face, all control operational orders require to issue from wireless controller, as the initial setting up of type and hanging point, inertial navigation boresight are joined
The bookbinding and modification, the quick-fried control setting of bomb, weapon power supply/aligned instructions/preparation instruction starting of several setting, task data
With the emission control etc. that stops, emitting and meet an urgent need.
Further, security interlock security design can also be carried out to the system of portable radio controller；Only ensure own
Safety interlocking condition when all meeting, system could start the transmitting and emergency transmitting of weapon.Due to external airborne fire control system
It unites mutually indepedent with aircraft system, portable radio controller can not really obtain true safety interlocking relevant information, such as
Operational state, undercarriage etc. can only be arranged, to ensure to pacify on the display control interface of wireless controller by operator
Entirely, information above is all defaulted as safe condition.
Further, ground-based mission management equipment is mainly by groups such as portable computer, transit cable, task management softwares
At for plane-generating target data, weapon bookbinding parameter, working frequency points information.Ground-based mission management equipment can be also used to
Plane-generating weapon application scheme, attack parameter, attack air route, resolving weapons program are resolved in advance according to operational design on ground
Attack area etc., and result is bound into portable radio controller and weapon fire control computer, as practical flight and attack
The reference frame of resolving.
The external aircraft mounted control system of the application is the independent fire control system of external, and energy and aircraft
Original Weapon Fire-Control-System concurrent working can fast implement different operational aircrafts to the installation and use demand of weapon；Also,
It is only mechanically connected with aircraft, the normal work and fight capability for not influencing original machine system after installation play；Further, be by
The system itself provides work electricity consumption and realizes to the power supply of weapon/hanger, control, display and information exchange, does not need to fly
Machine provides power supply and carries out control interconnection of signals；Further, which is mounted on aircraft hanging point level-one by universal machine interface
It under hanger, does not need to carry out software and hardware change to aircraft, a variety of operational aircraft platforms can be adapted to, can satisfy different fight and fly
Machine can quickly form fight capability to the installation and use demand of weapon.
Further, the external aircraft mounted control system of the application, it is multiple solely by single wireless control apparatus comprehensive integration
Vertical external Weapon Fire-Control-System and weapon information realizes the peace of automation control management process and key signal " people is in ring "
Full property design, the comprehensive function for being based on " key operation " are shown, can flexibly realize system function operation switching, greatly
The operating burden of pilot is alleviated greatly, and there is good scalability and versatility.
Second aspect, this application discloses a kind of external fire control system application method, including it is winged wait be adapted to
Preparation process and mission phase step before machine takes off.
Wherein, the preparation process before taking off may include:
S10 step: ground-based mission management equipment 5 treats adaptation aircraft and weapon 2 carries out ground-based mission planning, and generates
Preplanned mission data and configuration parameter.
S11 step: it is completed according to preplanned mission data and configuration parameter to wireless controlling equipment 4, control management subsystem 3
And prepare operation before the taking off of weapon 2.
Further, S11 step may include:
S111 step: wireless controlling equipment 4 carries out parameter configuration according to ground configuration parameter；
S112 step: the wireless controlling equipment 4 after the completion of parameter configuration is according to configuration parameter to corresponding aircraft type
It is configured with hanging point number；
S113 step: wireless controlling equipment 4 carries out networking configuration with the wireless telecom equipment 31 on the aircraft to match；Tool
Body, wireless controlling equipment 4 is switched on searches for the wireless telecom equipment 31 of attachment automatically, searches wireless telecom equipment 31ID and shows
In lists, corresponding ID and hanging point are matched according to practical carry situation by terrestrial operation person, after networking success, is led to
It will intuitively be shown over the display with the ID of bomb rack and physics carry position.
Further, after S113 step further include:
S1131 step: state reporting unit by wireless communication equipment 31 by the ID and weapon carry of general bomb rack 1
Location information reports to wireless controlling equipment 4；
S114 step: equipment 31 will be sent to control pipe to wireless controlling equipment 4 to target of attack parameter by wireless communication
It manages subsystem 3 and carries out target information configuration；Specifically, single goal/Bi-objective attack mode may be selected, while target can be known
Number, target type, longitude and latitude height, bullet number, template number edited；When Bi-objective attack mode, wireless controlling equipment 4 is according to mesh
Mark priority binds the parameter of two targets respectively gives two fire control computers (weapon management module 32).
S115 step: aligned instructions, weapon management module 32 are sent to weapon management module 32 by wireless controlling equipment 4
Navigation equipment 34, which is controlled, according to aligned instructions enters inertial navigation alignment；Specifically, the high information of initial longitude and latitude can be bound, is controlled
Alignment is completed in inertial navigation.
S116 step: weapon is sent to weapon management module 32 by wireless controlling equipment 4 and powers on instruction, weapon manages mould
Block 32 powers on instruction according to weapon and carries out power on operation to weapon 2 by power-supply device 33, and the completion of weapon 2 after powering on powers on
After self-test operations, preceding preparation process completion is taken off wait be adapted to；Also, power-on self-test is carried out simultaneously in weapon, Fire control calculation
Machine can automatically identify weapon type, and weapon type, weapon self-test state are simultaneously displayed in picture.
Further, after the weapon after powering on of S116 step completes power-on self-test operation, further includes:
S1161 step: state reporting unit by wireless communication equipment 31 by the self-test state information report of weapon 2 to nothing
Line controlling equipment 4.
Mission phase step includes:
S20 step: weapon 2 to be launched is determined by wireless controlling equipment 4；Wherein, if the force of this flight carry
Device type more than one, there is selective key in weapon picture, and pilot selects the weapon type that this to be emitted；
S21 step: it is carried out by wireless controlling equipment 4 and wireless telecom equipment 31 and control management subsystem 3 and weapon 2
Manipulation instruction and/or data information interaction；
Further, S21 step can also include:
S211 step: aligned instructions, weapon management module 31 are sent to weapon management module 32 by wireless controlling equipment 4
Weapon 2, which is controlled, according to aligned instructions enters alignment；
S212 step: preparation instruction, weapon management module 32 are sent to weapon management module 32 by wireless controlling equipment 4
It is controlled before weapon 2 is emitted according to preparation instruction and prepares operation；Preparing operation before transmitting for example can be progress weapon occupy-place,
Specifically, if the quantity more than one of the weapon type currently selected, wireless controlling equipment 4 can be automatic according to the sequence of default
1 piece of weapon as next secondary emission is selected, certainly, pilot can also manually select other by wireless controlling equipment 4
Occupy-place.
S213 step: weapon application scheme and target data are sent to weapon management module 32 by wireless controlling equipment 4
Binding instructio, weapon management module 32 carry out target data stapling operation to weapon 2 according to target data binding instructio；
S214 step: firing order is sent to transmitting solving unit by wireless controlling equipment 4.
S22 step: control management subsystem 3 controls general bomb rack 1 according to manipulation instruction and launches to weapon (2)；
Transmitting solving unit i.e. in control management subsystem 3 carries out dispensing control to weapon 2 according to firing order generation.When weapon standard
After getting ready, pilot can enter solution of fire control picture can operate on wireless controlling equipment 4 after meeting launching condition
Firing button implements arm discharge.After arm discharge, corresponding weapon symbol disappears on wireless controlling equipment 4, flies for prompting
Office staff's weapon is from beam.
Further, it can also be set including safety interlocking in the external fire control system application method of the application
It sets；Wherein, in the state of ground or state of flight, different states can be shown in safety interlocking setting screen.
Equally, the external fire control system application method of the application is the independent air weapon of external
Fire control system application method, and different operational aircrafts can be fast implemented with the original Weapon Fire-Control-System concurrent working of aircraft
To the installation and use demand of weapon；Also, it is only mechanically connected with aircraft, is not influenced the normal work of original machine system after installation
Make and fight capability plays；Further, be by the system itself provide work electricity consumption and realize to the power supply of weapon/hanger,
Control, display and information exchange do not need aircraft and provide power supply and interconnection of signals；Further, which is connect by universal machine
Mouth is mounted under aircraft hanging point level-one hanger, is not needed aircraft and is carried out software and hardware change, can be adapted to a variety of operational aircraft platforms,
Different operational aircrafts be can satisfy to the installation and use demand of weapon, and can quickly form fight capability.
Further, the fire control system application method of the application passes through single wireless control apparatus comprehensive integration
Multiple independent external Weapon Fire-Control-Systems and weapon information, realizing automation control management process key signal, " people exists
Ring " and safety Design, the comprehensive function for being based on " key operation " show, can flexibly realize system function grasp
Work switches, and significantly reduces the operating burden of pilot, has good scalability and versatility.
The above, the only specific embodiment of the application, but the protection scope of the application is not limited thereto, it is any
Within the technical scope of the present application, any changes or substitutions that can be easily thought of by those familiar with the art, all answers
Cover within the scope of protection of this application.Therefore, the protection scope of the application should be with the scope of protection of the claims
It is quasi-.
Claims (14)
1. a kind of external fire control system characterized by comprising
General bomb rack (1), the general bomb rack (1) are removably attached to aircraft exterior to be adapted to, meanwhile, it is described general
Bomb rack (1) controlled is launched the weapon (2) for hanging weapon to be carried (2)；
Control management subsystem (3), control management subsystem (3) are removably attached to the aircraft exterior to be adapted to,
Control management subsystem (3) is configured to equipment (31) by wireless communication and receives manipulation instruction and/or data information, and root
Corresponding manipulation is carried out according to manipulation instruction and/or data information, including the control general bomb rack (1) to the weapon
(2) it is launched；
Ground-based mission management equipment (5), the ground-based mission management equipment (5) are used to be in ground standard in the aircraft to be adapted to
When the standby stage, ground-based mission planning is carried out to the aircraft to be adapted to and the weapon, and generate preplanned mission data and match
Set parameter；
Wireless controlling equipment (4), the wireless controlling equipment (4) send for controlled to control management subsystem (3)
The manipulation instruction and/or data information are also used to the preplanned mission data generated according to the ground-based mission management equipment (5)
Corresponding aircraft type and hanging point quantity are configured with configuration parameter, and manages the nothing in subsystem (3) with the control that matches
Line communication equipment (31) carries out networking configuration.
2. external fire control system according to claim 1, which is characterized in that the general bomb rack (1)
Top structure, be configured to be adapted with the suspension interface of the aircraft hanging point level-one hanger to be adapted to, it is fixed be suspended on it is described
Level-one hanger lower part, the general bomb rack (1) are configured with the weapon (2) compatible bomb shackle.
3. external fire control system according to claim 1, which is characterized in that the control manages subsystem
(3) include:
Weapon management module (32), the weapon management module (32) are received described wireless by the wireless telecom equipment (31)
The manipulation instruction and/or data information that controlling equipment (4) is sent, and according to manipulation instruction and/or data information to the weapon
(2) corresponding manipulation is carried out, the weapon (2) is launched including the general bomb rack (1) is controlled；
Power-supply device (33), the power-supply device (33) are used to be the weapon management module (32), wireless telecom equipment (31)
And general bomb rack (1) power supply.
4. external fire control system according to claim 3, which is characterized in that the control manages subsystem
(3) include:
Navigation equipment (34), the navigation equipment (34) connect with the weapon management module (32)；
Satellite signal receiving antenna (35), the satellite signal receiving antenna (35) respectively with the weapon management module (32) and
Navigation equipment (34) connection；Wherein
The weapon management module (32) is configured to control the navigation equipment according to aligned instructions or navigation instruction is received
(34) enter alignment or navigational state；
The wireless controlling equipment (4) sends the aligned instructions or navigation to the weapon management module (32) for controlled
Instruction；
The power-supply device (33) connect with the navigation equipment (34), for powering for the navigation equipment (34).
5. external fire control system according to claim 4, which is characterized in that the navigation equipment (34) is
Inertia/combinations of satellites navigation equipment.
6. external fire control system according to claim 3, which is characterized in that the weapon management module
(32) include:
Upper electric unit, the upper electric unit receive the wireless controlling equipment (4) by the wireless telecom equipment (31) and send
Power on instruction, and to power on instruction to control the power-supply device (33) be that the weapon (2) are powered on according to described；Wherein
The wireless controlling equipment (4) powers on instruction to described in the weapon management module (32) transmission for controlled.
7. external fire control system according to claim 3, which is characterized in that the weapon management module
(32) include:
Preparatory unit, the preparatory unit receive the wireless controlling equipment (4) by the wireless telecom equipment (31) and send
Preparation instruction, and controlled before the weapon (2) is emitted according to the preparation instruction and prepare operation；
Parameter stapling unit, the parameter stapling unit receive the controlling equipment (4) by the communication equipment (31) and send
Weapon application scheme and target data binding instructio, and according to the target data binding instructio to the weapon carry out target
The wireless controlling equipment of data stapling operation parameter stapling unit parameter stapling unit；
Emit solving unit, the transmitting solving unit completes weapon attacking envelope curve and launching condition resolves, and calculation result is led to
It crosses the communication equipment (31) and is reported to the controlling equipment (4), while the transmitting for receiving the controlling equipment (4) transmission refers to
It enables, and the dispensing operation transmitting to the weapon (2) is completed according to the firing order control suspension arrangement (1) and resolves list
The member transmitting wireless controlling equipment of solving unit；
The wireless controlling equipment (4) sends the preparation instruction, weapon to the weapon management module (32) for controlled
Operational version, target data binding instructio and firing order.
8. external fire control system according to claim 3, which is characterized in that the weapon management module
(32) include:
State reporting unit, the state reporting unit are used for the weapon management module (32) in response to the wireless manipulation
State when equipment (4) manipulation instruction reports to the wireless controlling equipment (4) by the wireless telecom equipment (31).
9. according to the described in any item external fire control systems of claim 2-8, which is characterized in that the control pipe
It is internal that reason subsystem (3) is fixed at the general bomb rack (1).
10. a kind of external fire control system application method, which is characterized in that including taking off preceding preparation wait be adapted to
Step and mission phase step, wherein
It is described take off before preparation process include:
S10 step: ground-based mission management equipment (5) carries out ground-based mission planning to the aircraft to be adapted to and weapon (2), and
Generate preplanned mission data and configuration parameter；
S11 step: it is to wireless controlling equipment (4), control management point according to the preplanned mission data and configuration parameter completion
Prepare operation before system (3) and the taking off of weapon (2)；
The mission phase step includes:
S20 step: weapon to be launched (2) are determined by the wireless controlling equipment (4)；
S21 step: pass through the wireless controlling equipment (4) and wireless telecom equipment (31) and control management subsystem (3)
Manipulation instruction and/or data information interaction are carried out with the weapon (2)；
S22 step: control management subsystem (3) controls the general bomb rack (1) to the weapon according to manipulation instruction
(2) it is launched.
11. external fire control system application method according to claim 10, which is characterized in that the S11
Step includes:
S111 step: the wireless controlling equipment (4) carries out parameter configuration according to ground configuration parameter；
S112 step: the wireless controlling equipment (4) after the completion of parameter configuration is according to the task data and configuration parameter pair
Corresponding aircraft type and hanging point quantity are configured；
S113 step: the wireless controlling equipment (4) by the wireless telecom equipment (31) with match it is single or multiple
Other wireless telecom equipments (31) carry out networking configuration；
S114 step: equipment (31) will be sent to control to the wireless controlling equipment (4) to target of attack parameter by wireless communication
Tubulation manages subsystem (3) and carries out target information configuration；
S115 step: aligned instructions, the weapon pipe are sent to weapon management module (32) by the wireless controlling equipment (4)
It manages module (32) and controls navigation equipment (34) into inertial navigation alignment according to the aligned instructions；
S116 step: weapon is sent by wireless controlling equipment (4) the Xiang Suoshu weapon management module (32) and powers on instruction, institute
It states weapon management module (32) and institute of the instruction to the weapon (2) progress power on operation, after powering on is powered on according to the weapon
It is described to take off preceding preparation process completion wait be adapted to after stating weapon (2) completion power-on self-test operation.
12. external fire control system application method according to claim 11, which is characterized in that described
Between S113 step and S114 step, further includes:
S1131 step: the state reporting unit by wireless communication equipment (31) by the ID of the general bomb rack (1) and
Weapon carry location information reports to the wireless controlling equipment (4).
13. external fire control system application method according to claim 11, which is characterized in that described
After the weapon after powering on of S116 step completes power-on self-test operation, further includes:
S1161 step: the state reporting unit by wireless communication equipment (31) by the self-test status information of the weapon (2)
Report to the wireless controlling equipment (4).
14. external fire control system application method according to claim 10, which is characterized in that the S21
Step includes:
S211 step: aligned instructions, the force are sent by wireless controlling equipment (4) the Xiang Suoshu weapon management module (32)
Device management module (31) controls the weapon (2) according to the aligned instructions and enters alignment；
S212 step: preparation instruction, the force are sent by wireless controlling equipment (4) the Xiang Suoshu weapon management module (32)
Device management module (32) is controlled according to the preparation instruction to be prepared to operate before the weapon (2) is emitted；
S213 step: by wireless controlling equipment (4) the Xiang Suoshu weapon management module (32) send weapon application scheme and
Target data binding instructio, the weapon management module (32) according to the target data binding instructio to the weapon (2) into
Row target data stapling operation；
S214 step: firing order is sent to the transmitting solving unit by the wireless controlling equipment (4).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811468076.1A CN109398709B (en) | 2018-12-03 | 2018-12-03 | External airborne weapon fire control system and use method |
| PCT/CN2019/122497 WO2020114362A1 (en) | 2018-12-03 | 2019-12-02 | Fire control system and use method for externally-mounted aircraft weapon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811468076.1A CN109398709B (en) | 2018-12-03 | 2018-12-03 | External airborne weapon fire control system and use method |
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| Publication Number | Publication Date |
|---|---|
| CN109398709A true CN109398709A (en) | 2019-03-01 |
| CN109398709B CN109398709B (en) | 2023-06-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811468076.1A Active CN109398709B (en) | 2018-12-03 | 2018-12-03 | External airborne weapon fire control system and use method |
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| WO (1) | WO2020114362A1 (en) |
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| CN114511212A (en) * | 2022-01-19 | 2022-05-17 | 中国航空研究院 | Integrated fire control method for multi-domain combat formation |
| CN115035764A (en) * | 2022-05-27 | 2022-09-09 | 中国航空工业集团公司沈阳飞机设计研究所 | Airborne launcher simulation transmission method |
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Also Published As
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| WO2020114362A1 (en) | 2020-06-11 |
| CN109398709B (en) | 2023-06-02 |
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