CN106915452A - A kind of composite aircraft landing system - Google Patents
A kind of composite aircraft landing system Download PDFInfo
- Publication number
- CN106915452A CN106915452A CN201710139377.9A CN201710139377A CN106915452A CN 106915452 A CN106915452 A CN 106915452A CN 201710139377 A CN201710139377 A CN 201710139377A CN 106915452 A CN106915452 A CN 106915452A
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- CN
- China
- Prior art keywords
- wing aircraft
- fixed wing
- aerial vehicle
- unmanned aerial
- rotor unmanned
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
Abstract
A kind of composite aircraft landing system, category vehicle technology field, more particularly to a kind of composite aircraft landing system；Including fixed wing aircraft, multi-rotor unmanned aerial vehicle, master control terminal, mobile terminal, APP software modules and airplane parking area；Fixed wing aircraft includes fuselage, wheeled tripod, route planning functional module, GPS module, radar, optical pickocff and mechanical handle；Multi-rotor unmanned aerial vehicle includes body, route planning functional module, GPS module, radar, optical pickocff and mechanical gripper；Master control terminal includes computer and GPRS；Mobile terminal is smart mobile phone, the mobile radio-based electronic devices such as flat board and proprietary remote control equipment；Airplane parking area is used to park fixed wing aircraft and multi-rotor unmanned aerial vehicle.The present invention combines fixed wing aircraft and multi-rotor unmanned aerial vehicle connection, and multi-rotor aerocraft provides the aerial runway of landing for fixed wing aircraft, reduces runway construction, is conducive to the popularization of fixed-wing.
Description
Technical field
The present invention relates to technical field of aerospace, more particularly to a kind of composite aircraft landing system.
Background technology
Traditional fixed wing aircraft advantage is fast flying speed, and voyage and cruise time are long, have the disadvantage landing distance,
Seek high-quality runway.The advantage of multi-rotor unmanned aerial vehicle is less landing site, and energy VTOL, hovering has the disadvantage
Power consumption is big, speed is slow, cruising time is short.
The content of the invention
The purpose of the present invention is the shortcoming for overcoming traditional fixed wing aircraft and multi-rotor unmanned aerial vehicle, with reference to respective excellent
Point, invents a kind of composite aircraft landing system.
A kind of technical scheme of composite aircraft landing system that the present invention is provided is as follows.
A kind of composite aircraft landing system, including fixed wing aircraft, multi-rotor unmanned aerial vehicle, master control terminal, movement are eventually
End, APP software modules and airplane parking area.
The fixed wing aircraft includes fuselage, wheeled tripod, route planning functional module, GPS module, radar, optics
Sensor and the mechanical handle directly over fixed wing aircraft.
The multi-rotor unmanned aerial vehicle include body, route planning functional module, GPS module, radar, optical pickocff and
Mechanical gripper immediately below multi-rotor unmanned aerial vehicle.
The master control terminal is arranged on operator backstage, and master control terminal includes computer and GPRS, master control terminal
Tracking, monitoring and scheduling for fixed wing aircraft and multi-rotor unmanned aerial vehicle, master control terminal are used with mobile terminal and wirelessly connected
Connect.
The mobile terminal is smart mobile phone, mobile flat board or proprietary remote control equipment.
The APP software modules insertion is in the runtime of mobile terminal.
The airplane parking area is used to park fixed wing aircraft and multi-rotor unmanned aerial vehicle.
A kind of composite aircraft landing System Working Principle is：User is entered by mobile terminal in APP software modules
Row interface operation fixed wing aircraft and multi-rotor unmanned aerial vehicle send departure information, and departure information is wirelessly transmitted to by mobile terminal
Master control terminal, master control terminal sends the signal that takes off by wireless signal to fixed wing aircraft and multi-rotor unmanned aerial vehicle, is parked in
The multi-rotor unmanned aerial vehicle of airplane parking area flies to the surface of fixed wing aircraft when instruction is received, fixed wing aircraft and many rotors without
Man-machine utilization radar and optical pickocff calculate mutual distance, and fixed wing aircraft is remained stationary as, and multi-rotor unmanned aerial vehicle is from top
Slowly near fixed wing aircraft, the mechanical gripper immediately below multi-rotor unmanned aerial vehicle is caught solid under the manipulation of control system
Determine the mechanical handle directly over wing aircraft, when holding solid, multi-rotor unmanned aerial vehicle flies upper aerial certain altitude with fixed wing aircraft,
Now fixed wing aircraft power set start and fly forward, while the mechanical gripper of multi-rotor unmanned aerial vehicle unclamps the machine of fixed unmanned plane
Tool handle, or multi-rotor unmanned aerial vehicle together with fixed wing aircraft it is preceding fly a segment distance after mechanical gripper release mechanism handle, many rotors
Unmanned plane makes a return voyage to takeoff setting automatically, and fixed wing aircraft flies to destination；When fixed wing aircraft needs landing, fixed-wing flies
Machine flies to the capture range in level point position overhead, is parked in the multi-rotor unmanned aerial vehicle of airplane parking area according to the path planning for having set
Fly to the capture range in overhead, fixed wing aircraft and multi-rotor unmanned aerial vehicle using radar and optical pickocff measuring and calculating it is mutual away from
From, guide fixed wing aircraft and multi-rotor unmanned aerial vehicle be slowly close to, when multi-rotor unmanned aerial vehicle flight in fixed wing aircraft just
Top and very close to when, the mechanical gripper of multi-rotor unmanned aerial vehicle catches rapidly the mechanical handle on fixed wing aircraft, now fixed-wing
Aircraft and multi-rotor unmanned aerial vehicle are flown with same speed and identical direction on corresponding track, the power of fixed wing aircraft
Device stops, and multi-rotor unmanned aerial vehicle is flown to airplane parking area with fixed wing aircraft, when multi-rotor unmanned aerial vehicle is returned with fixed wing aircraft
When going back to airplane parking area, the mechanical gripper of multi-rotor unmanned aerial vehicle slowly unclamps the mechanical grip end of fixed wing aircraft automatically, many rotors nobody
Machine flies back to stand automatically.
Therefore, a kind of composite aircraft landing system of the invention can overcome lacking for traditional fixed-wing and many rotors
Point, reduces runway construction, is conducive to the popularization of fixed-wing.
Brief description of the drawings
Fig. 1 is the structural representation of composite aircraft landing system of the present invention, and Fig. 2 is composite aircraft landing system of the present invention
The block diagram of system, Fig. 3 is the top view of fixed wing aircraft, and Fig. 4 is the side view of many gyroplanes.
In Fig. 1 ~ 4,1- multi-rotor unmanned aerial vehicles, 11- bodies, 12- route planning functional modules, 13-GPS modules, 14- thunders
Reach, 15- optical pickocffs, 16- mechanical grippers, 2- fixed wing aircrafts, 21- fuselages, the wheeled tripods of 22-, 23- route planning work(
Can module, 24-GPS modules, 25- radars, 26- optical pickocffs, 27- machinery handles.
Specific embodiment
Specific embodiment of the invention provides a kind of composite aircraft landing system, the system include fixed wing aircraft 2,
Multi-rotor unmanned aerial vehicle 1, master control terminal, mobile terminal, APP software modules, airplane parking area.
The fixed wing aircraft 2 include fuselage 21, wheeled tripod 22, route planning functional module 23, GPS module 24,
Radar 25, optical pickocff 26 and the mechanical handle 27 directly over fixed wing aircraft.
The multi-rotor unmanned aerial vehicle 1 includes fuselage 11, route planning functional module 12, GPS module 13, radar 14, optics
Sensor 15 and the mechanical gripper immediately below multi-rotor unmanned aerial vehicle 16.
The master control terminal is arranged on operator backstage, and master control terminal includes computer and GPRS, master control terminal
Track In Track, monitoring and scheduling for fixed wing aircraft 2 and multi-rotor unmanned aerial vehicle 1, master control terminal are used with mobile terminal
Wireless connection.
The mobile terminal is smart mobile phone, mobile flat board or proprietary remote control equipment.
The APP software modules insertion is in the runtime of mobile terminal.
The airplane parking area is for parking fixed wing aircraft 2 and multi-rotor unmanned aerial vehicle 1.
A kind of composite aircraft landing System Working Principle：User is carried out by mobile terminal in APP software modules
The departure information of interface operation fixed wing aircraft 2 and multi-rotor unmanned aerial vehicle 1, departure information is wirelessly transmitted to master control by mobile terminal
Terminal processed, master control terminal sends the signal that takes off by wireless signal to fixed wing aircraft 2 and multi-rotor unmanned aerial vehicle 1, is parked in
The multi-rotor unmanned aerial vehicle 1 on machine level ground flies to the surface of fixed wing aircraft 2, fixed wing aircraft 2 and many rotors when instruction is received
Unmanned plane 1 calculates mutual distance using radar and optical pickocff, and fixed wing aircraft 2 is remained stationary as, and multi-rotor unmanned aerial vehicle 1 is slow
Slowly near fixed wing aircraft 2, the mechanical gripper 16 immediately below multi-rotor unmanned aerial vehicle is caught under the manipulation of control system
Mechanical handle 27 directly over fixed wing aircraft 2, when holding solid, multi-rotor unmanned aerial vehicle 1 flies upper aerial one with fixed wing aircraft 2
Fixed height, now the power set of fixed wing aircraft 2 start and fly forward, while the mechanical gripper 11 of multi-rotor unmanned aerial vehicle 1 unclamps solid
Determine the mechanical handle 12 of unmanned plane, or multi-rotor unmanned aerial vehicle 1 is preceding together with fixed wing aircraft 2 flies mechanical gripper 11 after a segment distance
Release mechanism handle 12, multi-rotor unmanned aerial vehicle 1 automatically returns to stand, and route planning function mould is provided with fixed wing aircraft 2
Block 23, fixed wing aircraft 2 flies to destination according to the route for having set.When fixed wing aircraft 2 needs landing, fixed-wing
Aircraft 2 flies to the capture range in level point overhead, is parked in the multi-rotor unmanned aerial vehicle 1 of airplane parking area according to the path planning for having set
Fly to the capture range in overhead, and fixed wing aircraft 2 and multi-rotor unmanned aerial vehicle 1 are calculated each other using radar 25 and optical pickocff 26
Distance, guide fixed wing aircraft 2 and multi-rotor unmanned aerial vehicle 1 be slowly close to, when multi-rotor unmanned aerial vehicle 1 fly fixed-wing fly
The surface of machine 2 and very close to when, the mechanical gripper 16 of multi-rotor unmanned aerial vehicle 1 is rapid catch on fixed wing aircraft 2 mechanical handle
27, now fixed wing aircraft 2 and multi-rotor unmanned aerial vehicle 1 flown on corresponding track with same speed and identical direction,
The power set of fixed wing aircraft 2 stop, and multi-rotor unmanned aerial vehicle 1 is flown to airplane parking area with fixed wing aircraft 2, when many rotors nobody
When machine 1 returns to airplane parking area with fixed wing aircraft 2, slowly the automatic fixed-wing that unclamps flies the mechanical gripper 16 of multi-rotor unmanned aerial vehicle 1
The mechanical grip end 27 of machine 2, multi-rotor unmanned aerial vehicle 1 automatically returns to stand.
A kind of composite aircraft landing system of the present invention can overcome the shortcoming of traditional fixed-wing and many rotors, reduce
Runway is built, and is conducive to the popularization of fixed-wing.
Claims (8)
1. a kind of composite aircraft landing system, it is characterised in that：Including fixed wing aircraft（2）, multi-rotor unmanned aerial vehicle（1）With stop
Machine level ground；Fixed wing aircraft includes fuselage（21）, wheeled tripod（22）With mechanical handle（27）；Multi-rotor unmanned aerial vehicle（1）Including machine
Body（11）And mechanical gripper（16）.
2. a kind of composite aircraft landing system according to claim 1, it is characterised in that：Mechanical gripper（16）In manipulation
Mechanical handle is caught under the manipulation of system（27）, make fixed wing aircraft（2）And multi-rotor aerocraft（1）Connection is combined, side
Just fixed wing aircraft（2）Take off or land.
3. a kind of composite aircraft landing system according to claim 1, it is characterised in that：Also include master control terminal,
Mobile terminal and APP software modules；The fixed wing aircraft（2）Also include GPS module（13）, radar（14）And optical pickocff
（26）；The multi-rotor unmanned aerial vehicle（1）GPS module（13）, radar（14）And optical pickocff（15）；Master control terminal includes meter
Calculation machine and GPRS, master control terminal use wireless connection with mobile terminal；Fortune of the APP software modules insertion installed in mobile terminal
In row system.
4. a kind of composite aircraft landing system according to claim 3, it is characterised in that：Mobile terminal is intelligent hand
Machine, mobile flat board or proprietary remote control equipment.
5. a kind of composite aircraft landing system according to claim 3 or 4, it is characterised in that：The fixed wing aircraft
（2）Also include route planning functional module（23）.
6. a kind of composite aircraft landing system according to claim 3 or 4, it is characterised in that：Many rotors nobody
Machine（1）Also include route planning functional module（12）.
7. a kind of composite aircraft landing system according to claim 3, it is characterised in that：Its mode of taking off is：User
Interface operation fixed wing aircraft is carried out in APP software modules by mobile terminal（2）And multi-rotor unmanned aerial vehicle（1）Rise Fetion
Breath, departure information is wirelessly transmitted to master control terminal by mobile terminal, and master control terminal is by wireless signal to fixed wing aircraft
（2）And multi-rotor unmanned aerial vehicle（1）Transmission is taken off signal, is parked in the multi-rotor unmanned aerial vehicle of airplane parking area（1）Fly when instruction is received
To fixed wing aircraft（2）Surface, fixed wing aircraft（2）And multi-rotor unmanned aerial vehicle（1）Surveyed using radar and optical pickocff
Calculate mutual distance, fixed wing aircraft（2）Remain stationary as, multi-rotor unmanned aerial vehicle（1）Slowly near fixed wing aircraft（2）, install
Mechanical gripper immediately below multi-rotor unmanned aerial vehicle（16）Fixed wing aircraft is caught under the manipulation of control system（2）Surface
Mechanical handle（27）, when holding solid, multi-rotor unmanned aerial vehicle（1）With fixed wing aircraft（2）Fly upper aerial certain altitude, it is now solid
Determine wing aircraft（2）Power set start and fly forward, while multi-rotor unmanned aerial vehicle（1）Mechanical gripper（11）Unclamp fixed unmanned plane
Mechanical handle（12）, or multi-rotor unmanned aerial vehicle（1）With fixed wing aircraft（2）It is preceding together to fly mechanical gripper after a segment distance（11）
Release mechanism handle（12）, multi-rotor unmanned aerial vehicle（1）Automatically return to stand, fixed wing aircraft（2）Fly to alone destination.
8. a kind of composite aircraft landing system according to claim 3, it is characterised in that：Its landing modes is：When solid
Determine wing aircraft（2）When needing landing, fixed wing aircraft（2）The capture range in level point overhead is flown to, many rotations of airplane parking area are parked in
Wing unmanned plane（1）Fly to the capture range in overhead, fixed wing aircraft（2）And multi-rotor unmanned aerial vehicle（1）Using radar（25）And light
Learn sensor（26）Calculate mutual distance, guide fixed wing aircraft（2）And multi-rotor unmanned aerial vehicle（1）Slowly it is close to, when many
Rotor wing unmanned aerial vehicle（1）Flight is in fixed wing aircraft（2）Surface and very close to when, multi-rotor unmanned aerial vehicle（1）Mechanical gripper
（16）Catch on fixed wing aircraft rapidly（2）Mechanical handle（27）, now fixed wing aircraft（2）And multi-rotor unmanned aerial vehicle（1）With
Same speed and identical direction are flown on corresponding track, fixed wing aircraft（2）Power set stop, many rotors without
It is man-machine（1）With fixed wing aircraft（2）Fly to airplane parking area, works as multi-rotor unmanned aerial vehicle（1）With fixed wing aircraft（2）Return and shut down
During level ground, multi-rotor unmanned aerial vehicle（1）Mechanical gripper（16）It is slowly automatic to unclamp fixed wing aircraft（2）Mechanical grip end（27）, it is many
Rotor wing unmanned aerial vehicle（1）Automatically return to stand.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139377.9A CN106915452A (en) | 2017-03-10 | 2017-03-10 | A kind of composite aircraft landing system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139377.9A CN106915452A (en) | 2017-03-10 | 2017-03-10 | A kind of composite aircraft landing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106915452A true CN106915452A (en) | 2017-07-04 |
Family
ID=59460426
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710139377.9A Pending CN106915452A (en) | 2017-03-10 | 2017-03-10 | A kind of composite aircraft landing system |
Country Status (1)
| Country | Link |
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| CN (1) | CN106915452A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108700891A (en) * | 2017-08-30 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Control method, unmanned plane and the machine readable storage medium of unmanned plane |
| WO2019080179A1 (en) * | 2017-10-27 | 2019-05-02 | 罗伟 | Takeoff method for fixed-wing unmanned aerial vehicle |
| US20210316861A1 (en) * | 2017-09-06 | 2021-10-14 | Hood Technology Corporation | Rotorcraft-assisted system for launching and retrieving a fixed-wing aircraft into and from free flight |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083573A (en) * | 2015-09-22 | 2015-11-25 | 西华大学 | Unmanned aerial vehicle anti-collision system and anti-collision method thereof |
| CN106005351A (en) * | 2016-07-06 | 2016-10-12 | 深圳市迪西姆科技开发股份有限公司 | Flapping wing type bionic intelligent balloon and operation method thereof |
| JP2017030739A (en) * | 2015-08-03 | 2017-02-09 | ロッキード マーティン コーポレイションＬｏｃｋｈｅｅｄ Ｍａｒｔｉｎ Ｃｏｒｐｏｒａｔｉｏｎ | Release and capture of fixed-wing aircraft |
| CN106428554A (en) * | 2016-08-31 | 2017-02-22 | 天津曙光天成科技有限公司 | Takeoff and landing system and method for fixed-wing unmanned aerial vehicle |
-
2017
- 2017-03-10 CN CN201710139377.9A patent/CN106915452A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2017030739A (en) * | 2015-08-03 | 2017-02-09 | ロッキード マーティン コーポレイションＬｏｃｋｈｅｅｄ Ｍａｒｔｉｎ Ｃｏｒｐｏｒａｔｉｏｎ | Release and capture of fixed-wing aircraft |
| CN105083573A (en) * | 2015-09-22 | 2015-11-25 | 西华大学 | Unmanned aerial vehicle anti-collision system and anti-collision method thereof |
| CN106005351A (en) * | 2016-07-06 | 2016-10-12 | 深圳市迪西姆科技开发股份有限公司 | Flapping wing type bionic intelligent balloon and operation method thereof |
| CN106428554A (en) * | 2016-08-31 | 2017-02-22 | 天津曙光天成科技有限公司 | Takeoff and landing system and method for fixed-wing unmanned aerial vehicle |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108700891A (en) * | 2017-08-30 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Control method, unmanned plane and the machine readable storage medium of unmanned plane |
| CN108700891B (en) * | 2017-08-30 | 2022-06-17 | 深圳市大疆创新科技有限公司 | Control method of unmanned aerial vehicle, unmanned aerial vehicle and machine-readable storage medium |
| US20210316861A1 (en) * | 2017-09-06 | 2021-10-14 | Hood Technology Corporation | Rotorcraft-assisted system for launching and retrieving a fixed-wing aircraft into and from free flight |
| US11897628B2 (en) * | 2017-09-06 | 2024-02-13 | Hood Technology Corporation | Rotorcraft-assisted system for launching and retrieving a fixed-wing aircraft into and from free flight |
| WO2019080179A1 (en) * | 2017-10-27 | 2019-05-02 | 罗伟 | Takeoff method for fixed-wing unmanned aerial vehicle |
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Application publication date: 20170704 |
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