CN109334973A - A kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing - Google Patents
A kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing Download PDFInfo
- Publication number
- CN109334973A CN109334973A CN201811353516.9A CN201811353516A CN109334973A CN 109334973 A CN109334973 A CN 109334973A CN 201811353516 A CN201811353516 A CN 201811353516A CN 109334973 A CN109334973 A CN 109334973A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- control system
- flight control
- wing
- visual angle
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
-
- 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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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
Abstract
The invention discloses a kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing, including flight control system, for providing the automatic control of plumbness and horizontality for aircraft；Aerial image acquisition device is connect with ground image reception device, for providing the Image Acquisition carried out in the air to ground, and returns to ground image reception device in real time using radio；GPS module is connect with flight control system, for providing location information to flight control system；Remote-receiver is connect with flight control system, the telecommand of the flight controller for receiving ground surface end, and returns the partial information at aircraft end to the flight controller；Dynamical system is connect with the flight control system, for providing power for aircraft.The present invention provides new landing modes, joined GPS module, provide effective guarded by location and limitation function, effectively reduce requirement of fixed-wing the first visual angle aircraft to place and operation.
Description
Technical field
The present invention relates to the technical fields of model airplane more particularly to a kind of using the of tail sitting posture VTOL fixed-wing
One visual angle aircraft.
Background technique
Currently, there are following several features in most of the first visual angle of fixed-wing aircraft:
1, generally using pure fixed-wing plus the form of video acquisition transmission reception device, for simple fixed-wing first
For the aircraft of visual angle, the mode of taking off can only take hand throwing, ejection, sliding race etc., and landing modes can only take downhill race, parachuting etc..
The manipulation of aircraft is for landing site and manipulator's requirement all with higher.
2, there is no GPS module, protected above in flight, enough defencive functions cannot be provided, protected without geography fence,
It makes a return voyage without a key, without protection out of control of making a return voyage.
Easy position steer mode cannot be provided to new hand in manipulation, cannot utmostly reduce manipulation difficulty.
Summary of the invention
Based on the above the deficiencies in the prior art, technical problem solved by the invention is to provide a kind of vertical using tail sitting posture
First visual angle aircraft of straight landing fixed-wing, has GPS module and flight controller, effectively reduces the view of fixed-wing first
Requirement of the angle aircraft to place and operation.
In order to solve the above-mentioned technical problem, the present invention is achieved through the following technical solutions: the present invention provides a kind of use
First visual angle aircraft of tail sitting posture VTOL fixed-wing, comprising:
Flight control system, for providing the automatic control of plumbness and horizontality for aircraft；
Aerial image acquisition device is connect, for providing sky with the flight control system and ground image reception device
In Image Acquisition that ground is carried out, and return to using radio the ground image reception device of ground surface end in real time；
GPS module is connect with the flight control system, for providing location information to flight control system；
Remote-receiver is connect with the flight control system, the remote control of the flight controller for receiving ground surface end
Instruction, and the partial information at aircraft end is returned to the flight controller；
Dynamical system is connect with the flight control system, for providing power for aircraft.
Embodiment as a preferred embodiment of the above technical solution, it is provided in an embodiment of the present invention solid using the VTOL of tail sitting posture
The the first visual angle aircraft for determining the wing further comprises some or all of following technical characteristic:
As an improvement of the above technical solution, the flight control system includes for providing gesture feedback information to winged
Row device carries out the inertial sensor unit of gesture stability, the location information for providing according to the GPS module to aircraft
Carry out the position control unit of position control.
As an improvement of the above technical solution, the dynamical system includes two motors and two steering engines, and the motor is used
In providing the flying power of aircraft, the steering engine is for providing the gesture stability of aircraft.
Compared with prior art, technical solution of the present invention has the following beneficial effects: that the present invention vertically rises in tail sitting posture
New landing mode is provided inside first visual angle aircraft of drop fixed-wing, GPS module is joined, provides effective position
Protection and restriction function provides simple position control mode, and solve the first visual angle of fixed-wing aircraft can not original place
The problem of landing, and solve the first visual angle of fixed-wing aircraft and can not carry out GPS location control, a key can not be carried out and maked a return voyage,
There is no the problem of geography fence.The present invention has GPS module and flight controller, effectively reduces the first visual angle of fixed-wing and flies
Requirement of the row device to place and operation.
The above description is only an overview of the technical scheme of the present invention, in order to better understand the technical means of the present invention,
And it can be implemented in accordance with the contents of the specification, and in order to allow above and other objects, features and advantages of the invention can
It is clearer and more comprehensible, below in conjunction with preferred embodiment, and cooperates attached drawing, detailed description are as follows.
Detailed description of the invention
In order to illustrate the technical solution of the embodiments of the present invention more clearly, the attached drawing to embodiment is simply situated between below
It continues.
Fig. 1 is the structural schematic diagram of the first visual angle aircraft of the invention using tail sitting posture VTOL fixed-wing.
Specific embodiment
The embodiment of the invention will now be described in detail with reference to the accompanying drawings, and as part of this specification passes through
Embodiment illustrates the principle of the present invention, and other aspects of the present invention, feature and its advantage will become by the detailed description
It is very clear.In the attached drawing of institute's reference, the same or similar component is indicated using identical drawing reference numeral in different figures.
As shown in Figure 1, the first visual angle aircraft using tail sitting posture VTOL fixed-wing of the preferred embodiment of the present invention
Structural schematic diagram, the first visual angle aircraft of the invention using tail sitting posture VTOL fixed-wing include aerial image acquisition dress
1, GPS module 2, flight control system 3, remote-receiver 4 and dynamical system 5 are set, the invention also includes be located at ground surface end
Flight controller 6 and ground image reception device 7.
Wherein, flight control system 3 provides the automatic control of plumbness and horizontality, root for aircraft of the invention
Gesture stability is carried out to aircraft according to the gesture feedback information that the inertial sensor unit of 3 the inside of flight control system provides, with
And the location information provided according to GPS, position control is carried out to aircraft according to the position control unit of 3 the inside of flight control system
System.
The aerial image acquisition device 1 is connect with the flight control system 3 and ground image reception device 7, is used for
The Image Acquisition carried out in the air to ground is provided, and returns to the ground image reception device 7 of ground surface end in real time using radio.
The GPS module 2 is connect with the flight control system 3, for providing location information to flight control system 3,
Position-force control can be carried out to aircraft, provide spatial position feedback for position-force control, make a return voyage for a key and position is provided
Set reference point.
The remote-receiver 4 is connect with the flight control system 3, for receiving the flight controller 6 of ground surface end
Telecommand, and return the partial information at aircraft end to the flight controller 6.
The dynamical system 5 is connect with the flight control system 3, for providing power for aircraft.Dynamical system 5 is divided
For two motors and two steering engines, motor is used to provide aircraft power, and two steering engines are used to provide the gesture stability of aircraft.
The present invention is a kind of the first novel visual angle aircraft, and pervious is all fixed-wing, the first visual angle of the invention
Aircraft is VTOL, after the aircraft of already existing tail sitting posture VTOL is loaded onto image acquisition and transmission device, is used
The first visual angle aircraft is made, radio image collecting transmitting device is loaded onto, on the control program of aircraft, joined GPS
Position control mode.
The present invention provides new landing mode inside the first visual angle aircraft, joined GPS module, provides effectively
Guarded by location and limitation function, provide simple position control mode, solve the nothing of the first visual angle of fixed-wing aircraft
The problem of method original place landing, and solve the first visual angle of fixed-wing aircraft and can not carry out GPS location control, a key can not be carried out
It makes a return voyage, there is no the problem of geography fence.
The above is a preferred embodiment of the present invention, cannot limit the right model of the present invention with this certainly
It encloses, it is noted that for those skilled in the art, without departing from the principle of the present invention, may be used also
To make several improvement and variation, these, which improve and change, is also considered as protection scope of the present invention.
Claims (3)
1. a kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing characterized by comprising
Flight control system, for providing the automatic control of plumbness and horizontality for aircraft；
Aerial image acquisition device is connect with the flight control system and ground image reception device, aerial right for providing
The Image Acquisition that ground carries out, and the ground image reception device of ground surface end is returned to using radio in real time；
GPS module is connect with the flight control system, for providing location information to flight control system；
Remote-receiver is connect with the flight control system, the telecommand of the flight controller for receiving ground surface end,
And the partial information at aircraft end is returned to the flight controller；
Dynamical system is connect with the flight control system, for providing power for aircraft.
2. using the first visual angle aircraft of tail sitting posture VTOL fixed-wing as described in claim 1, it is characterised in that: institute
State flight control system include for provide gesture feedback information with to aircraft carry out gesture stability inertial sensor unit,
Location information for being provided according to the GPS module is with the position control unit to aircraft progress position control.
3. using the first visual angle aircraft of tail sitting posture VTOL fixed-wing as described in claim 1, it is characterised in that: institute
Stating dynamical system includes two motors and two steering engines, and the motor is used for providing the flying power of aircraft, the steering engine
In the gesture stability of offer aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811353516.9A CN109334973A (en) | 2018-11-14 | 2018-11-14 | A kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811353516.9A CN109334973A (en) | 2018-11-14 | 2018-11-14 | A kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109334973A true CN109334973A (en) | 2019-02-15 |
Family
ID=65315163
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811353516.9A Pending CN109334973A (en) | 2018-11-14 | 2018-11-14 | A kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing |
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| Country | Link |
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| CN (1) | CN109334973A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109857132A (en) * | 2019-03-12 | 2019-06-07 | 辽宁壮龙无人机科技有限公司 | A kind of flight control assemblies and method |
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| CN103803093A (en) * | 2014-03-03 | 2014-05-21 | 天津曙光敬业科技有限公司 | Fixed-wing unmanned aerial vehicle aerial shooting device |
| US20170101178A1 (en) * | 2015-10-07 | 2017-04-13 | Hoi Hung Herbert LEE | Flying apparatus with multiple sensors and gesture-based operation |
| CN106741820A (en) * | 2016-12-20 | 2017-05-31 | 中国科学院长春光学精密机械与物理研究所 | A kind of VTOL fixed-wing unmanned vehicle |
| CN107264813A (en) * | 2017-05-24 | 2017-10-20 | 南京理工大学 | A kind of tailstock vertical takeoff and landing vehicle flight control system |
| CN207117834U (en) * | 2017-08-14 | 2018-03-16 | 青岛智强信息产业有限公司 | A kind of unmanned plane image capturing system |
| CN207985194U (en) * | 2018-03-13 | 2018-10-19 | 清远市巨劲科技有限公司 | A kind of novel unmanned plane of taking photo by plane |
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2018
- 2018-11-14 CN CN201811353516.9A patent/CN109334973A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103803093A (en) * | 2014-03-03 | 2014-05-21 | 天津曙光敬业科技有限公司 | Fixed-wing unmanned aerial vehicle aerial shooting device |
| US20170101178A1 (en) * | 2015-10-07 | 2017-04-13 | Hoi Hung Herbert LEE | Flying apparatus with multiple sensors and gesture-based operation |
| CN106741820A (en) * | 2016-12-20 | 2017-05-31 | 中国科学院长春光学精密机械与物理研究所 | A kind of VTOL fixed-wing unmanned vehicle |
| CN107264813A (en) * | 2017-05-24 | 2017-10-20 | 南京理工大学 | A kind of tailstock vertical takeoff and landing vehicle flight control system |
| CN207117834U (en) * | 2017-08-14 | 2018-03-16 | 青岛智强信息产业有限公司 | A kind of unmanned plane image capturing system |
| CN207985194U (en) * | 2018-03-13 | 2018-10-19 | 清远市巨劲科技有限公司 | A kind of novel unmanned plane of taking photo by plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109857132A (en) * | 2019-03-12 | 2019-06-07 | 辽宁壮龙无人机科技有限公司 | A kind of flight control assemblies and method |
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| PB01 | Publication | ||
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Application publication date: 20190215 |