CN107031808A - System and method based near space stratospheric airship electromagnetic launch unmanned plane - Google Patents
System and method based near space stratospheric airship electromagnetic launch unmanned plane Download PDFInfo
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- CN107031808A CN107031808A CN201710257465.9A CN201710257465A CN107031808A CN 107031808 A CN107031808 A CN 107031808A CN 201710257465 A CN201710257465 A CN 201710257465A CN 107031808 A CN107031808 A CN 107031808A
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- stratospheric airship
- unmanned plane
- ejection
- control centre
- electromagnetic launch
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/82—Airborne vehicles
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Mechanical Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Transportation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention provides a kind of system and method based near space stratospheric airship electromagnetic launch unmanned plane, system includes control centre and the stratospheric airship of communication connection；Stratospheric airship is provided with electromagnetic launch device；The stratospheric airship that method includes flight or hovered near space sends state confirmation information to control centre；Control centre transfers mission planning information according to state confirmation information, and according to the generation ejection instruction of mission planning information, ejection instruction is sent to stratospheric airship；Stratospheric airship is according to outside of the ejection instruction control electromagnetic launch device by unmanned plane in a predetermined direction with dynamic ejection to stratospheric airship of reception so that unmanned plane flies to default target area according to mission planning path.Reliability of the present invention is high and strong applicability, conveniently and accurately realize the transmitting quickly and efficiently to unmanned plane, it is to avoid the useless consumption of the energy of the unmanned plane before carry out task, and then ensure that unmanned plane performs the reliability and integrality of task.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, and in particular to one kind based near space stratospheric airship electromagnetic launch without
Man-machine system and method.
Background technology
Unmanned plane is turning into equipment more and more indispensable during modern high technology is lived, and is widely used in army
The multiple fields such as thing, industrial or agricultural, civilian, in multiple application fields such as investigation and exploration, Fire prevention, agricultural plant protection, aerial photographing
Play an important role；And unmanned plane, in the application of certain fields, its launching phase is often referred to as the most difficult stage
One of, numerous studies and trial have been made in take off transmitting of the various countries to unmanned plane.
At present, the mode that the transmitting of unmanned plane is generally carried out by way of itself starts flight or ground-level ejection is taken off
Carry out, but this kind of mode suffers from high requirement to the endurance of unmanned plane with flying speed, is required to unmanned plane consumption
Self energy, power climb to the flying height of needs, in some continuations of the journey require high application scenarios, current radiation pattern
Smoothly completing for unmanned plane task can not be ensured.
Therefore, a kind of radiation pattern for avoiding unmanned plane from consuming most of energy before carry out task how is designed,
It is urgent problem to be solved.
The content of the invention
For defect of the prior art, the present invention provide it is a kind of based near space stratospheric airship electromagnetic launch nobody
The system and method for machine, system and method reliability height and strong applicability, are conveniently and accurately realized to the fast of unmanned plane
Speed and efficient transmitting, it is to avoid the useless consumption of the energy of the unmanned plane before carry out task, and then ensure that unmanned plane is performed
The reliability and integrality of task.
In order to solve the above technical problems, the present invention provides following technical scheme：
On the one hand, the invention provides a kind of system based near space stratospheric airship electromagnetic launch unmanned plane, institute
The system of stating includes：The control centre of communication connection and stratospheric airship；
The control centre is used to send control instruction to the stratospheric airship, and flies for receiving the stratosphere
The state confirmation information of ship；
The stratospheric airship is flown or hovered in the range of the predeterminated position near space；
The stratospheric airship is provided with electromagnetic launch device, and the electromagnetic launch device is used for unmanned plane by predetermined
Direction and dynamic ejection are to the outside of the stratospheric airship.
Further, the electromagnetic launch device is arranged on the bottom of the stratospheric airship, and flies with the stratosphere
The inside connection of ship.
Further, the inside of the electromagnetic launch device includes the ejection region and holding areas of connection, and, level
Transmission equipment on the ejection region and holding areas is set；
The transmission equipment is used to the unmanned plane of the holding areas being sent to the ejection region.
Further, base station of the control centre for setting on the ground.
Further, the control centre connects including the monitoring unit with stratospheric airship communication connection, information
Receive unit and instruction sending unit；
The monitoring unit is used to monitor the stratospheric airship and unmanned plane in real time；
Described information receiving unit is used to receive the state confirmation information that the stratospheric airship is sent；
The instruction sending unit is used to send control instruction to the stratospheric airship.
Further, being provided with the stratospheric airship is used to detecting the electromagnetic launch device and unmanned plane therein
The detection unit of facility information.
On the other hand, present invention also offers the method that the system described in a kind of basis carries out electromagnetic launch unmanned plane, institute
The method of stating includes：
Fly or hover over the stratospheric airship near space and send state confirmation information to the control centre；
The control centre transfers the mission planning information of unmanned plane according to the state confirmation information, and according to described
Planning information of being engaged in generation ejection instruction, wherein, the ejection instruction includes the mission planning path of the unmanned plane；
The control centre sends the ejection instruction to the stratospheric airship；
The stratospheric airship receives the ejection instruction, and obtains the mission planning path in the ejection instruction；
The stratospheric airship determines attitude information according to the mission planning path, and is adjusted according to the attitude information
Direction of ejection；
And, the stratospheric airship controls the electromagnetic launch device that unmanned plane is pressed into pre- in the mission planning path
If direction and dynamic ejection to the outside of the stratospheric airship so that the unmanned plane flies according to the mission planning path
Toward default target area.
Further, the flight or the stratospheric airship hovered near space are sent to the control centre
State confirmation information, including：
The stratospheric airship generates flight path according to the operating instruction for receiving control centre's transmission, or transfers certainly
The default flight path of body；
The stratospheric airship is flown to according to the flight path in the near space in the range of predeterminated position；
The stratospheric airship detects the facility information of the electromagnetic launch device and unmanned plane therein；
And, confirm the electromagnetic launch device and unmanned plane therein it is accurate it is ready after, the stratospheric airship
State confirmation information is sent to the control centre.
Further, methods described includes：
The control centre monitors the equipment state and positional information of the stratospheric airship and unmanned plane in real time.
Further, the stratospheric airship controls the electromagnetic launch device that unmanned plane is pressed into the mission planning path
In default direction and dynamic ejection to the outside of the stratospheric airship, also include afterwards：
The stratospheric airship sends ejection to the control centre and completes information.
As shown from the above technical solution, it is of the present invention it is a kind of based near space stratospheric airship electromagnetic launch nobody
The system and method for machine, system includes control centre and the stratospheric airship of communication connection；Stratospheric airship is provided with electromagnetism bullet
Injection device；The stratospheric airship that method includes flight or hovered near space sends state confirmation information to control centre；
Control centre transfers mission planning information according to state confirmation information, and according to the generation ejection instruction of mission planning information；Advection
Layer dirigible sends ejection instruction；And, stratospheric airship is according to ejection instruction control electromagnetic launch device by unmanned plane by predetermined
Direction and dynamic ejection to the outside of stratospheric airship so that unmanned plane flies to default target area according to preset path.
Reliability height of the present invention and strong applicability, conveniently and accurately realize the transmitting quickly and efficiently to unmanned plane, it is to avoid
The useless consumption of the energy of the unmanned plane before carry out task, and then ensure that unmanned plane performs the reliability and integrality of task.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is the accompanying drawing used required in technology description to be briefly described, it should be apparent that, drawings in the following description are the present invention
Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can also basis
These accompanying drawings obtain other accompanying drawings.
Fig. 1 is a kind of structural representation of system based near space stratospheric airship electromagnetic launch unmanned plane of the present invention
Figure.
Fig. 2 is a kind of flow signal of method based near space stratospheric airship electromagnetic launch unmanned plane of the present invention
Figure.
Fig. 3 is the stream of step 100 in the method based near space stratospheric airship electromagnetic launch unmanned plane of the invention
Journey schematic diagram.
Embodiment
To make the purpose, technical scheme and advantage of the embodiment of the present invention clearer, below in conjunction with the embodiment of the present invention
In accompanying drawing, clear, complete description is carried out to the technical scheme in the embodiment of the present invention, it is clear that described embodiment is
A part of embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art
The every other embodiment obtained under the premise of creative work is not made, belongs to the scope of protection of the invention.
Embodiments of the invention one disclose a kind of system based near space stratospheric airship electromagnetic launch unmanned plane
Embodiment, referring to Fig. 1, the system specifically includes following content：
The control centre of communication connection and stratospheric airship；The control centre, which is used to send to the stratospheric airship, to be controlled
System instruction；The stratospheric airship is flown or hovered in the range of the predeterminated position near space；On the stratospheric airship
Provided with electromagnetic launch device, the electromagnetic launch device be used for by unmanned plane in a predetermined direction with dynamic ejection to the advection
The outside of layer dirigible；The electromagnetic launch device is arranged on the bottom of the stratospheric airship, and with the stratospheric airship
Inside connection.
In the foregoing description, the inside of the electromagnetic launch device includes the ejection region and holding areas of connection, and,
It is horizontally disposed with the transmission equipment on the ejection region and holding areas；The transmission equipment is used for the nothing of the holding areas
It is man-machine to be sent to the ejection region；Base station of the control centre for setting on the ground；The control centre include with
Monitoring unit, information receiving unit and the instruction sending unit of the stratospheric airship communication connection；The monitoring unit is used for
The stratospheric airship and unmanned plane are monitored in real time；Described information receiving unit is used to receive the shape that the stratospheric airship is sent
State confirmation；The instruction sending unit is used to send control instruction to the stratospheric airship；In the stratospheric airship
Detection unit provided with the facility information for detecting the electromagnetic launch device and unmanned plane therein；Fly or hover over and face
The stratospheric airship near space sends state confirmation information to the control centre；The control centre is according to the shape
State confirmation transfers mission planning information, and according to mission planning information generation ejection instruction；The stratospheric airship
Send the ejection instruction；The stratospheric airship controls the electromagnetic launch device to press unmanned plane according to the ejection instruction
Predetermined direction and dynamic ejection are to the outside of the stratospheric airship so that the unmanned plane flies to default according to preset path
Target area, wherein, near space stratospheric airship stay sky in liftoff 18km-50km stratosphere altitude range.
It was found from foregoing description, embodiments of the invention reliability height and strong applicability are realized to the quick of unmanned plane
And efficient transmitting, it is to avoid the useless consumption of the energy of the unmanned plane before carry out task.
Embodiments of the invention two disclose a kind of method based near space stratospheric airship electromagnetic launch unmanned plane
Embodiment, referring to Fig. 2, this method specifically includes following content：
Step 100：Fly or hover over the stratospheric airship near space and send state to the control centre
Confirmation.
Step 200：The control centre transfers the mission planning information of unmanned plane, and root according to the state confirmation information
According to mission planning information generation ejection instruction.
In step 200, the ejection instruction includes the mission planning path of the unmanned plane.
Step 300：The control centre sends the ejection instruction to the stratospheric airship.
Step 400：The stratospheric airship receives the ejection instruction, and obtains the mission planning in the ejection instruction
Path.
Step 500：The stratospheric airship determines attitude information according to the mission planning path, and according to the posture
Information adjusts direction of ejection.
Step 600：The stratospheric airship controls the electromagnetic launch device that unmanned plane is pressed into the mission planning path
In default direction and dynamic ejection to the outside of the stratospheric airship so that the unmanned plane is according to the mission planning road
Footpath is flown to default target area.
In the foregoing description, using the technology that electromagnetic launch unmanned plane is carried out based near space stratospheric airship；Close on
Space stratospheric airship stays empty in liftoff 18km-50km stratosphere altitude range, with load-carrying it is big, between space-time it is long, cover
The characteristics of lid scope is wide, Stratospheric Airship Platform possesses itself unique advantage, makes up Aeronautics and Astronautics as low-speed motion platform
It is not enough；Electromagnetism unmanned aerial vehicle ejecting refers to that unmanned plane does not enable the power set of itself, and using electromagnetic force as acceleration means, by transmitting
The power that device is provided obtains the radiation pattern that enough kinergeties are implemented to take off.With good controllability, can conveniently and
Change the size of ejection energy exactly by the size of output current is adjusted, make Electromagnetical ejector that there is accurate launch from light-duty
To the ability of heavy unmanned plane.
It was found from foregoing description, embodiments of the invention can conveniently and accurately realize the quick and height to unmanned plane
The transmitting of effect, it is ensured that unmanned plane performs the reliability and integrality of task.
In a kind of specific implementation, referring to Fig. 3, the step 100 in the above method specifically includes following content：
Step 101：The stratospheric airship generates flight path according to the operating instruction for receiving control centre's transmission,
Or transfer itself default flight path.
Step 102：The stratospheric airship is flown to according to the flight path in the near space in the range of predeterminated position.
Step 103：The stratospheric airship detects the facility information of the electromagnetic launch device and unmanned plane therein.
Step 104：Confirm the electromagnetic launch device and unmanned plane therein it is accurate it is ready after, the stratosphere flies
Ship sends state confirmation information to the control centre.
In a kind of specific implementation, the above method also specifically includes following content：
The control centre monitors the equipment state and positional information of the stratospheric airship and unmanned plane in real time.
In a kind of specific implementation, the stratospheric airship controls the electromagnetic launch to fill according to the ejection instruction
Put by unmanned plane in a predetermined direction with dynamic ejection to the outside of the stratospheric airship, following bag is also specifically included afterwards
Include：
The stratospheric airship sends ejection to the control centre and completes information.
For further instruction this programme, it is above-mentioned based near space stratospheric airship electromagnetism that the present invention provides a kind of application
The system for launching unmanned plane realizes the concrete application example of the method based near space stratospheric airship electromagnetic launch unmanned plane, such as
Under：
Stratospheric airship is delivered to after specified altitude assignment by ground control centre, Stratospheric Airship in Position-Attitude or determine region hover in
Near space height；
Electromagnetic ejection system is installed below stratospheric airship, stratospheric airship is detected to electromagnetic launch device, electricity
Magnetic catapult-launching gear prepares to possess after emissivities in place, earthward control centre's transmission state confirmation；
Ground control centre is received after electromagnetic launch unit state confirmation to the real-time monitoring of stratospheric airship, you can
Implement mission planning according to mission requirements；
Ground control centre sends electromagnetic launch unmanned plane according to planning, to stratospheric airship and instructed；
Stratospheric airship is received after instruction, you can start the ejection granting that electromagnetic launch device implements unmanned plane, nobody
Machine is ejected, and is flown to task object region, patrols winged in unmanned plane progress cruising flight or target area, is performed to scout and is appointed
Business or strike mission；
After stratospheric airship ejection system is provided in place, stratospheric airship earthward control centre's acknowledgement state, and waiting
Secondary ejection instruction；
Unmanned plane can return to ground control centre after performing task object.
It was found from foregoing description, application example of the invention carries out the electromagnetic launch technology of unmanned aerial vehicle side of taking off using stratospheric airship
Formula so that the flying height of unmanned plane is high, coverage is big, compensate for small and medium size unmanned aerial vehicles and perform the radius of task small lacking
Point, and the intercepted risk of unmanned plane is reduced, and also dirigible is delivered reduce generation event during unmanned plane during flying in the air
The possibility of barrier, dispensing airborne compared to conventional airplane is more convenient, provides new means for the granting of unmanned plane, has widened unmanned plane
The new opplication field of ejection, is that unmanned plane execution close to space vehicle task aspect is significant.Therefore based on stratosphere
Dirigible launches unmanned plane, and both can complement one another, be combined with each other the common mode for performing to target reconnaissance or performing task,
Display one's respective advantages, make up the inferior position that dirigible itself mobility is low, unmanned plane execution task radius is small.
Above example is merely to illustrate technical scheme, rather than its limitations；Although with reference to the foregoing embodiments
The present invention is described in detail, it will be understood by those within the art that：It still can be to foregoing each implementation
Technical scheme described in example is modified, or carries out equivalent substitution to which part technical characteristic；And these are changed or replaced
Change, the essence of appropriate technical solution is departed from the spirit and scope of various embodiments of the present invention technical scheme.
Claims (10)
1. a kind of system based near space stratospheric airship electromagnetic launch unmanned plane, it is characterised in that the system includes：
The control centre of communication connection and stratospheric airship；
The control centre is used to send control instruction to the stratospheric airship, and for receiving the shape of the fluid layer dirigible
State confirmation；
The stratospheric airship is flown or hovered in the range of the predeterminated position near space；
The stratospheric airship is provided with electromagnetic launch device, and the electromagnetic launch device is used for unmanned plane in a predetermined direction
With dynamic ejection to the outside of the stratospheric airship.
2. system according to claim 1, it is characterised in that the electromagnetic launch device is arranged on the stratospheric airship
Bottom, and connected with the inside of the stratospheric airship.
3. system according to claim 2, it is characterised in that the inside of the electromagnetic launch device includes the ejection of connection
Region and holding areas, and, it is horizontally disposed with the transmission equipment on the ejection region and holding areas；
The transmission equipment is used to the unmanned plane of the holding areas being sent to the ejection region.
4. system according to claim 1, it is characterised in that base station of the control centre for setting on the ground.
5. system according to claim 1, it is characterised in that the control centre includes logical with the stratospheric airship
Believe monitoring unit, information receiving unit and the instruction sending unit of connection；
The monitoring unit is used to monitor the stratospheric airship and unmanned plane in real time；
Described information receiving unit is used to receive the state confirmation information that the stratospheric airship is sent；
The instruction sending unit is used to send control instruction to the stratospheric airship.
6. system according to claim 1, it is characterised in that being provided with the stratospheric airship is used to detect the electromagnetism
The detection unit of the facility information of catapult-launching gear and unmanned plane therein.
7. a kind of method that system according to any one of claim 1 to 6 carries out electromagnetic launch unmanned plane, its feature exists
In methods described includes：
Fly or hover over the stratospheric airship near space and send state confirmation information to the control centre；
The control centre transfers the mission planning information of unmanned plane according to the state confirmation information, and is advised according to the task
Information generation ejection instruction is drawn, wherein, the ejection instruction includes the mission planning path of the unmanned plane；
The control centre sends the ejection instruction to the stratospheric airship；
The stratospheric airship receives the ejection instruction, and obtains the mission planning path in the ejection instruction；
The stratospheric airship determines attitude information according to the mission planning path, and adjusts ejection according to the attitude information
Direction；
And, the stratospheric airship controls the electromagnetic launch device that unmanned plane is pressed into default in the mission planning path
Direction and dynamic ejection are to the outside of the stratospheric airship so that the unmanned plane flies to pre- according to the mission planning path
If target area.
8. method according to claim 7, it is characterised in that the flight hovers over the advection near space
Layer dirigible sends state confirmation information to the control centre, including：
The stratospheric airship generates flight path according to receiving the operating instruction that the control centre sends, or to transfer itself pre-
If flight path；
The stratospheric airship is flown to according to the flight path in the near space in the range of predeterminated position；
The stratospheric airship detects the facility information of the electromagnetic launch device and unmanned plane therein；
And, confirm the electromagnetic launch device and unmanned plane therein it is accurate it is ready after, the stratospheric airship is to institute
State control centre and send state confirmation information.
9. method according to claim 7, it is characterised in that methods described includes：
The control centre monitors the equipment state and positional information of the stratospheric airship and unmanned plane in real time.
10. method according to claim 7, it is characterised in that the stratospheric airship controls the electromagnetic launch device
Unmanned plane is pressed into default direction and dynamic ejection in the mission planning path, to the outside of the stratospheric airship, to go back afterwards
Including：
The stratospheric airship sends ejection to the control centre and completes information.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710257465.9A CN107031808A (en) | 2017-04-19 | 2017-04-19 | System and method based near space stratospheric airship electromagnetic launch unmanned plane |
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| CN201710257465.9A CN107031808A (en) | 2017-04-19 | 2017-04-19 | System and method based near space stratospheric airship electromagnetic launch unmanned plane |
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