CN106774416A - Information processing method and device, control device, UAS - Google Patents
Information processing method and device, control device, UAS Download PDFInfo
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- CN106774416A CN106774416A CN201710020325.XA CN201710020325A CN106774416A CN 106774416 A CN106774416 A CN 106774416A CN 201710020325 A CN201710020325 A CN 201710020325A CN 106774416 A CN106774416 A CN 106774416A
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- Prior art keywords
- control
- motion
- unmanned plane
- rod
- preset direction
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- 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
- G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
-
- 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
Abstract
The embodiment of the invention discloses a kind of information processing method, information processor, control device and UAS, the information processing method includes：Obtain the direction of motion of first control-rod on the first preset direction；Based on the direction of motion of first control-rod on the first preset direction, the direction of motion of the control unmanned plane on the first preset direction, the direction of motion on the first preset direction is identical with the first control-rod for the direction of motion of the unmanned plane on the first preset direction.The information processing method that the embodiment of the present invention is provided, when unmanned plane during flying is controlled, the direction of motion of the direction of motion of the unmanned plane on the first preset direction all the time with the first control-rod on the first preset direction is identical, and without realizing the calibration in direction by recognizing the indicator lamp on unmanned plane, avoid when flying distance farther out when, the phenomenon for causing manipulation to be slipped up due to the indicator lamp that cannot be accurately identified on unmanned plane, reduces the manipulation fault rate during control unmanned plane during flying.
Description
Technical field
The present invention relates to unmanned aerial vehicle (UAV) control technical field, more particularly to a kind of information processing method, a kind of information processing apparatus
Put, a kind of control device and a kind of UAS.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself.With section
Development, the application of unmanned plane is more and more extensive.Current unmanned plane accesses direction and is provided with indicator lamp in its battery, works as nothing
When man-machine controller is directed at its indicator lamp, the moving direction of controller upper connecting rod and the heading of unmanned plane be it is corresponding,
I.e. when controller is just to indicator lamp, pull bar is moved forward, unmanned plane flight forward；When controller is back to indicator lamp direction,
Pull bar is moved forward, and unmanned plane flies backward.
But, in above-mentioned control method, when unmanned plane during flying is distant, the manipulator of unmanned plane cannot accurately identify
Indicator lamp, causes to be difficult to during manipulation to cause the moving direction of controller upper connecting rod and operator unmanned plane within sweep of the eye
Heading it is always consistent, manipulation probability of failure it is higher.
The content of the invention
In order to solve the above technical problems, the embodiment of the invention provides a kind of information processing method, nobody is controlled to reduce
Manipulation fault rate in machine flight course.
To solve the above problems, following technical scheme is the embodiment of the invention provides：
A kind of information processing method, is applied to unmanned plane, and the method includes：
Obtain the direction of motion of first control-rod on the first preset direction；
Based on the direction of motion of first control-rod on the first preset direction, the unmanned plane is controlled described first
The direction of motion on preset direction, the direction of motion of the unmanned plane on first preset direction and first control-rod
The direction of motion is identical on first preset direction.
Preferably, first preset direction includes：The unmanned operators fore-and-aft direction within the vision and/or
The unmanned operators left and right directions within the vision.
Preferably, the direction of motion for obtaining the first control-rod on the first preset direction includes：
The direction of motion of first control-rod that acquisition global positioning system is detected on the first preset direction.
Preferably, the method also includes：
Obtain the direction of motion of second control-rod on the second preset direction；
Based on the direction of motion of second control-rod on second preset direction, the rotation of the unmanned plane is controlled
Direction.
Preferably, when second control-rod is moved along the positive direction of second preset direction, the unmanned plane is suitable
Hour hands rotate；When second control-rod is moved along the negative direction of second preset direction, the unmanned plane revolves counterclockwise
Turn；
Wherein, the positive direction and negative direction of second preset direction are two phases parallel to second preset direction
Opposite direction.
Preferably, the method also includes：
Obtain current kinetic direction of the unmanned plane on first preset direction；
Judge current kinetic direction of the unmanned plane on first preset direction with first control-rod in institute
Whether the direction of motion stated on the first preset direction is consistent；
When current kinetic direction of the unmanned plane on first preset direction with first control-rod described
When the direction of motion on first preset direction is inconsistent, motion side of the unmanned plane on first preset direction is adjusted
To making current kinetic direction of the unmanned plane on first preset direction pre- described first with first control-rod
The direction of motion on set direction is consistent.
A kind of information processor, including：
Acquiring unit, for obtaining the direction of motion of first control-rod on the first preset direction；
Control unit, for the direction of motion based on first control-rod on the first preset direction, controls the nothing
The man-machine direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction with
First control-rod direction of motion on first preset direction is identical.
Preferably, the acquiring unit is additionally operable to obtain the direction of motion of second control-rod on the second preset direction；
Described control unit is additionally operable to based on the direction of motion of second control-rod on second preset direction, control
Make the direction of rotation of the unmanned plane.
Preferably, the acquiring unit is additionally operable to obtain current kinetic of the unmanned plane on first preset direction
Direction；
Described control unit be additionally operable to judge current kinetic direction of the unmanned plane on first preset direction with
Whether the direction of motion of first control-rod on first preset direction is consistent, when the unmanned plane is pre- described first
When the direction of motion of current kinetic direction on set direction with first control-rod on first preset direction is inconsistent,
The direction of motion of the unmanned plane on first preset direction is adjusted, makes the unmanned plane on first preset direction
The direction of motion of the current kinetic direction with first control-rod on first preset direction it is consistent.
A kind of control device, including：First control-rod, the first detecting element and processing unit, wherein, first detection
Element is used to detect the direction of motion of first control-rod on the first preset direction；
The processing unit is used to obtaining the first control-rod that first detecting element detects in the first preset direction
On the direction of motion, and the direction of motion based on first control-rod on the first preset direction controls the unmanned plane to exist
The direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction and described
One control-rod direction of motion on first preset direction is identical.
Preferably, the control device also includes the second control-rod；
First detecting element is additionally operable to the direction of motion of detection second control-rod on the second preset direction；
The processing unit is additionally operable to obtain the direction of motion of second control-rod on the second preset direction, and is based on
The direction of motion of second control-rod on second preset direction, controls the direction of rotation of the unmanned plane.
Preferably, the processing unit is additionally operable to：
Obtain current kinetic direction of the unmanned plane on first preset direction；
Judge current kinetic direction of the unmanned plane on first preset direction with first control-rod in institute
Whether the direction of motion stated on the first preset direction is consistent；
When current kinetic direction of the unmanned plane on first preset direction with first control-rod described
When the direction of motion on first preset direction is inconsistent, motion side of the unmanned plane on first preset direction is adjusted
To making current kinetic direction of the unmanned plane on first preset direction pre- described first with first control-rod
The direction of motion on set direction is consistent.
Preferably, first detecting element is global positioning system.
A kind of UAS, including unmanned plane and control device, the control device include：First control-rod, first
Detecting element and processing unit；
Wherein, first detecting element is used to detect the direction of motion of first control-rod on the first preset direction；
The processing unit is used to obtaining the first control-rod that first detecting element detects in the first preset direction
On the direction of motion, and the direction of motion based on first control-rod on the first preset direction controls the unmanned plane to exist
The direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction and described
One control-rod direction of motion on first preset direction is identical.
Preferably, the control device also includes the second control-rod；
First detecting element is additionally operable to the direction of motion of detection second control-rod on the second preset direction；
The processing unit is additionally operable to obtain the direction of motion of second control-rod on the second preset direction, and is based on
The direction of motion of second control-rod on second preset direction, controls the direction of rotation of the unmanned plane.
Preferably, the unmanned plane also include the second detecting element, second detecting element be used for detect it is described nobody
Current kinetic direction of the machine on first preset direction.
Preferably, the processing unit is additionally operable to：
Obtain the current kinetic of the unmanned plane that second detecting element detects on first preset direction
Direction；
Judge current kinetic direction of the unmanned plane on first preset direction with first control-rod in institute
Whether the direction of motion stated on the first preset direction is consistent；
When current kinetic direction of the unmanned plane on first preset direction with first control-rod described
When the direction of motion on first preset direction is inconsistent, motion side of the unmanned plane on first preset direction is adjusted
To making current kinetic direction of the unmanned plane on first preset direction pre- described first with first control-rod
The direction of motion on set direction is consistent.
Compared with prior art, above-mentioned technical proposal has advantages below：
The information processing method that the embodiment of the present invention is provided, the method includes：Obtain the first control-rod default first
The direction of motion on direction；Based on the direction of motion of first control-rod on the first preset direction, the unmanned plane is controlled
The direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction with it is described
First control-rod direction of motion on first preset direction is identical.As can be seen here, the information that the embodiment of the present invention is provided
Processing method, control unmanned plane during flying when, the direction of motion of the unmanned plane on first preset direction all the time with institute
State the direction of motion of first control-rod on first preset direction identical, and without by recognizing the indicator lamp on unmanned plane
To realize the calibration in direction, it is to avoid when flying distance farther out when, led due to the indicator lamp that cannot be accurately identified on unmanned plane
The phenomenon of manipulation error is caused, the manipulation fault rate during control unmanned plane during flying is reduced.
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
The accompanying drawing to be used needed for having technology description is briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, can be with
Other accompanying drawings are obtained according to these accompanying drawings.
The flow chart of the information processing method that Fig. 1 is provided by one embodiment of the invention；
The flow chart of the information processing method that Fig. 2 is provided by another embodiment of the present invention；
Fig. 3 is the flow chart of the information processing method that another embodiment of the invention is provided；
The structural representation of the information processor that Fig. 4 is provided by one embodiment of the invention；
The structural representation of the information processor that Fig. 5 is provided by another embodiment of the present invention；
Fig. 6 is the structural representation of the information processor that another embodiment of the invention is provided；
The structural representation of the UAS that Fig. 7 is provided by one embodiment of the invention.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Many details are elaborated in the following description in order to fully understand the present invention, but the present invention can be with
Other manner described here is different from using other to implement, those skilled in the art can be without prejudice to intension of the present invention
In the case of do similar popularization, therefore the present invention is not limited by following public specific embodiment.
A kind of information processing method is the embodiment of the invention provides, unmanned plane is applied to, as shown in figure 1, the method includes：
S1：Obtain the direction of motion of first control-rod on the first preset direction；
S2：Based on the direction of motion of first control-rod on the first preset direction, the unmanned plane is controlled described
The direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction and the described first control
Bar processed direction of motion on first preset direction is identical.
Specifically, in one embodiment of the invention, when first control-rod is moved forward, the unmanned plane to
Preceding flight；When first control-rod is moved rearwards by, the unmanned plane flies backward；When first control-rod is to left movement
When, the unmanned plane flies to the left, and when first control-rod is moved right, the unmanned plane flies to the right.Need explanation
, the heading all around of the unmanned plane is unmanned operators direction all around within the vision.
On the basis of above-described embodiment, in one embodiment of the invention, first preset direction includes described
The fore-and-aft direction within the vision of unmanned operators；In another embodiment of the present invention, first preset direction
Including unmanned operators' left and right directions within the vision；In yet another embodiment of the present invention, described first is pre-
Set direction includes that unmanned operators' fore-and-aft direction within the vision and the unmanned operators are within the vision
Left and right directions, in other embodiments of the invention, first preset direction can also be the unmanned operators visual field
In the range of other directions, the present invention this is not limited, specifically depend on the circumstances.
On the basis of any of the above-described embodiment, in one embodiment of the invention, the first control-rod of the acquisition exists
The direction of motion on first preset direction includes：First control-rod that acquisition global positioning system is detected is default first
The direction of motion on direction.I.e. in embodiments of the present invention, detect first control-rod described by global positioning system
The direction of motion on first preset direction, in other embodiments of the invention, can also by other means detect described
The direction of motion of one control-rod on first preset direction, the present invention is not limited this, is specifically depended on the circumstances.
On the basis of any of the above-described embodiment, in one embodiment of the invention, as shown in Fig. 2 the method is also wrapped
Include：
S3：Obtain the direction of motion of second control-rod on the second preset direction；
S4：Based on the direction of motion of second control-rod on second preset direction, the unmanned plane is controlled
Direction of rotation.
Optionally, in embodiments of the present invention, when second control-rod is transported along the positive direction of second preset direction
When dynamic, the unmanned plane turns clockwise；When second control-rod is moved along the negative direction of second preset direction, institute
State unmanned plane rotate counterclockwise；Wherein, the positive direction and negative direction of second preset direction are default parallel to described second
Two rightabouts in direction.
On the basis of above-described embodiment, in one embodiment of the invention, second control-rod is swingle, institute
The positive direction of the second preset direction is stated for clockwise, the negative direction of second preset direction is for counterclockwise；At this
In the other embodiment of invention, second control-rod can also be sliding bar, and the positive direction of second preset direction is cunning
The direction that lever is slided, the negative direction of second preset direction is another direction of sliding bar slip, and the present invention is right
This is not limited, and is specifically depended on the circumstances.
On the basis of above-described embodiment, in one embodiment of the invention, as shown in figure 3, the method also includes：
S5：Obtain current kinetic direction of the unmanned plane on first preset direction；
S6：Judge that current kinetic direction of the unmanned plane on first preset direction exists with first control-rod
Whether the direction of motion on first preset direction is consistent；
S7：When current kinetic direction of the unmanned plane on first preset direction with first control-rod in institute
State the direction of motion on the first preset direction it is inconsistent when, adjust motion side of the unmanned plane on first preset direction
To making current kinetic direction of the unmanned plane on first preset direction pre- described first with first control-rod
The direction of motion on set direction is consistent.
It should be noted that on the basis of above-described embodiment, in one embodiment of the invention, can be with direct access
Current kinetic direction of the unmanned plane on first preset direction；In another embodiment of the present invention, can be with
The current kinetic direction of the unmanned plane is obtained by recording the anglec of rotation of the unmanned plane on the second preset direction.As worked as
The anglec of rotation of the unmanned plane be less than 360 ° when, then the current kinetic direction of the unmanned plane with first control-rod in institute
It is then the anglec of rotation of the unmanned plane to state the deviation between the direction of motion on the first preset direction；When the rotation of the unmanned plane
Gyration be more than 360 ° when, then the current kinetic direction of the unmanned plane with first control-rod in first preset direction
On the direction of motion between deviation then for the anglec of rotation of the unmanned plane subtracts 360 ° of * n, wherein, n is whole more than zero
Number, and 360 ° of * n are less than the anglec of rotation of the unmanned plane；When the anglec of rotation of the unmanned plane is equal to 360 °, then the nothing
Deviation between the direction of motion of the man-machine current kinetic direction and first control-rod on first preset direction is
Zero, i.e., current kinetic direction of the described unmanned plane on first preset direction is pre- described first with first control-rod
The direction of motion on set direction is consistent.
Understand from the above mentioned, the information processing method that the embodiment of the present invention is provided, it is described when unmanned plane during flying is controlled
The direction of motion of the unmanned plane on first preset direction is all the time with first control-rod on first preset direction
The direction of motion it is identical, so as to the unmanned plane be in larger distance, as long as in operator within sweep of the eye, you can hold
Easily manipulation, when particularly withdrawing unmanned plane, only need to be consistent toward control-rod of pulling back, and without by recognizing unmanned plane
On indicator lamp realize the calibration in direction, it is to avoid when flying distance farther out when, due to that cannot accurately identify on unmanned plane
Indicator lamp and cause manipulation slip up phenomenon, reduce control unmanned plane during flying during manipulation fault rate.
Accordingly, the embodiment of the present invention additionally provides a kind of information processor, as shown in figure 4, the information processor
Including：
Acquiring unit 10, for obtaining the direction of motion of first control-rod on the first preset direction；
Control unit 20, for the direction of motion based on first control-rod on the first preset direction, control is described
The direction of motion of the unmanned plane on first preset direction, the direction of motion of the unmanned plane on first preset direction
The direction of motion is identical on first preset direction with first control-rod.
Specifically, in one embodiment of the invention, when first control-rod is moved forward, the unmanned plane to
Preceding flight；When first control-rod is moved rearwards by, the unmanned plane flies backward；When first control-rod is to left movement
When, the unmanned plane flies to the left, and when first control-rod is moved right, the unmanned plane flies to the right.Need explanation
, the heading all around of the unmanned plane is unmanned operators direction all around within the vision.
On the basis of above-described embodiment, in one embodiment of the invention, first preset direction includes described
The fore-and-aft direction within the vision of unmanned operators；In another embodiment of the present invention, first preset direction
Including unmanned operators' left and right directions within the vision；In yet another embodiment of the present invention, described first is pre-
Set direction includes that unmanned operators' fore-and-aft direction within the vision and the unmanned operators are within the vision
Left and right directions, in other embodiments of the invention, first preset direction can also be the unmanned operators visual field
In the range of other directions, the present invention this is not limited, specifically depend on the circumstances.
On the basis of any of the above-described embodiment, in one embodiment of the invention, acquiring unit 10 is used to obtain the
During the direction of motion of one control-rod on the first preset direction specifically for：Obtain global positioning system is detected described first
The direction of motion of the control-rod on the first preset direction.I.e. in embodiments of the present invention, detect described by global positioning system
The direction of motion of first control-rod on first preset direction, in other embodiments of the invention, can also be by it
His mode detects the direction of motion of first control-rod on first preset direction, and the present invention is not limited this,
Specifically depend on the circumstances.
On the basis of any of the above-described embodiment, in implementing at one of the invention, the acquiring unit 10 is additionally operable to obtain
Take the direction of motion of second control-rod on the second preset direction；
Described control unit 20 is additionally operable to based on the direction of motion of second control-rod on second preset direction,
Control the direction of rotation of the unmanned plane.
Optionally, in embodiments of the present invention, when second control-rod is transported along the positive direction of second preset direction
When dynamic, the unmanned plane turns clockwise；When second control-rod is moved along the negative direction of second preset direction, institute
State unmanned plane rotate counterclockwise；Wherein, the positive direction and negative direction of second preset direction are default parallel to described second
Two rightabouts in direction.
On the basis of above-described embodiment, in one embodiment of the invention, second control-rod is swingle, institute
The positive direction of the second preset direction is stated for clockwise, the negative direction of second preset direction is for counterclockwise；At this
In the other embodiment of invention, second control-rod can also be sliding bar, and the positive direction of second preset direction is cunning
The direction that lever is slided, the negative direction of second preset direction is another direction of sliding bar slip, and the present invention is right
This is not limited, and is specifically depended on the circumstances.
On the basis of any of the above-described embodiment, in one embodiment of the invention, the acquiring unit 10 is additionally operable to
Obtain current kinetic direction of the unmanned plane on first preset direction；
Described control unit 20 is additionally operable to judge current kinetic direction of the unmanned plane on first preset direction
It is whether consistent with the direction of motion of first control-rod on first preset direction, when the unmanned plane is described first
The direction of motion of current kinetic direction on preset direction with first control-rod on first preset direction is inconsistent
When, the direction of motion of the unmanned plane on first preset direction is adjusted, make the unmanned plane in the described first default side
The direction of motion of the upward current kinetic direction with first control-rod on first preset direction is consistent.
It should be noted that on the basis of above-described embodiment, in one embodiment of the invention, the acquiring unit
10 can be with unmanned plane described in direct access on first preset direction current kinetic direction；In another reality of the invention
Apply in example, the acquiring unit 10 can also obtain institute by recording the anglec of rotation of the unmanned plane on the second preset direction
State the current kinetic direction of unmanned plane.Such as when the anglec of rotation of the unmanned plane is less than 360 °, then the unmanned plane is current
Deviation between the direction of motion of the direction of motion and first control-rod on first preset direction then for it is described nobody
The anglec of rotation of machine；When the anglec of rotation of the unmanned plane is more than 360 °, then the current kinetic direction of the unmanned plane and institute
It is then the anglec of rotation of the unmanned plane to state the deviation between the direction of motion of first control-rod on first preset direction
360 ° of * n are subtracted, wherein, n is the integer more than zero, and 360 ° of * n are less than the anglec of rotation of the unmanned plane；When the unmanned plane
Anglec of rotation when being equal to 360 °, then the current kinetic direction of the unmanned plane and first control-rod are default described first
The deviation between the direction of motion on direction is zero, i.e., current kinetic direction of the described unmanned plane on first preset direction
It is consistent with the direction of motion of first control-rod on first preset direction.
Understand from the above mentioned, the information processor that the embodiment of the present invention is provided, it is described when unmanned plane during flying is controlled
The direction of motion of the unmanned plane on first preset direction is all the time with first control-rod on first preset direction
The direction of motion it is identical, so as to the unmanned plane be in larger distance, as long as in operator within sweep of the eye, you can hold
Easily manipulation, when particularly withdrawing unmanned plane, only need to be consistent toward control-rod of pulling back, and without by recognizing unmanned plane
On indicator lamp realize the calibration in direction, it is to avoid when flying distance farther out when, due to that cannot accurately identify on unmanned plane
Indicator lamp and cause manipulation slip up phenomenon, reduce control unmanned plane during flying during manipulation fault rate.
Additionally, the embodiment of the present invention additionally provides a kind of control device, as shown in figure 5, the control device includes：First control
Bar processed 30, the first detecting element 40 and processing unit 50, wherein, first detecting element 40 is used to detect the first control-rod 30
The direction of motion on the first preset direction；
The processing unit 50 is pre- first for obtaining the first control-rod 30 that first detecting element 40 is detected
The direction of motion on set direction, and the direction of motion based on first control-rod 30 on the first preset direction, control are described
The direction of motion of the unmanned plane on first preset direction, the direction of motion of the unmanned plane on first preset direction
The direction of motion is identical on first preset direction with first control-rod 30.
Specifically, in one embodiment of the invention, when first control-rod 30 is moved forward, the unmanned plane
Flight forward；When first control-rod 30 is moved rearwards by, the unmanned plane flies backward；When first control-rod 30 to
During left movement, the unmanned plane flies to the left, and when first control-rod 30 is moved right, the unmanned plane flies to the right.
It should be noted that the heading all around of the unmanned plane is the within the vision front and rear left unmanned operators
Right direction.
On the basis of above-described embodiment, in one embodiment of the invention, first preset direction includes described
The fore-and-aft direction within the vision of unmanned operators；In another embodiment of the present invention, first preset direction
Including unmanned operators' left and right directions within the vision；In yet another embodiment of the present invention, described first is pre-
Set direction includes that unmanned operators' fore-and-aft direction within the vision and the unmanned operators are within the vision
Left and right directions, in other embodiments of the invention, first preset direction can also be the unmanned operators visual field
In the range of other directions, the present invention this is not limited, specifically depend on the circumstances.
On the basis of any of the above-described embodiment, in one embodiment of the invention, first detecting element is preferred
It is global positioning system.But the present invention is not limited this, specifically depend on the circumstances.
On the basis of above-described embodiment, in one embodiment of the invention, as shown in fig. 6, the control device is also
Including the second control-rod 60；
First detecting element 40 is additionally operable to motion side of detection second control-rod 60 on the second preset direction
To；
The processing unit 50 is additionally operable to obtain the direction of motion of second control-rod 60 on the second preset direction, and
Based on the direction of motion of second control-rod 60 on second preset direction, the direction of rotation of the unmanned plane is controlled.
Optionally, in embodiments of the present invention, when second control-rod 60 is along the positive direction of second preset direction
During motion, the unmanned plane turns clockwise；When second control-rod 60 is moved along the negative direction of second preset direction
When, the unmanned plane rotate counterclockwise；Wherein, the positive direction and negative direction of second preset direction are parallel to described second
Two rightabouts of preset direction.
On the basis of above-described embodiment, in one embodiment of the invention, second control-rod 60 is swingle,
The positive direction of second preset direction is for clockwise, the negative direction of second preset direction is for counterclockwise；
In other embodiment of the invention, second control-rod 60 can also be sliding bar, the positive direction of second preset direction
It is a direction of sliding bar slip, the negative direction of second preset direction is another direction, this hair of sliding bar slip
It is bright that this is not limited, specifically depend on the circumstances.
On the basis of above-described embodiment, in one embodiment of the invention, the processing unit 50 is additionally operable to：
Obtain current kinetic direction of the unmanned plane on first preset direction；
Judge that current kinetic direction of the unmanned plane on first preset direction exists with first control-rod 30
Whether the direction of motion on first preset direction is consistent；
When current kinetic direction of the unmanned plane on first preset direction with first control-rod 30 in institute
State the direction of motion on the first preset direction it is inconsistent when, adjust motion side of the unmanned plane on first preset direction
To making current kinetic direction of the unmanned plane on first preset direction with first control-rod 30 described first
The direction of motion on preset direction is consistent.
It should be noted that on the basis of above-described embodiment, in one embodiment of the invention, the processing unit
50 can be with unmanned plane described in direct access on first preset direction current kinetic direction；In another reality of the invention
Apply in example, the processing unit 50 can also obtain institute by recording the anglec of rotation of the unmanned plane on the second preset direction
State the current kinetic direction of unmanned plane.Such as when the anglec of rotation of the unmanned plane is less than 360 °, then the unmanned plane is current
Deviation between the direction of motion of the direction of motion and first control-rod 30 on first preset direction is then the nothing
The man-machine anglec of rotation；When the unmanned plane the anglec of rotation be more than 360 ° when, then the current kinetic direction of the unmanned plane with
Deviation between the direction of motion of first control-rod 30 on first preset direction is then the rotation of the unmanned plane
Angle subtracts 360 ° of * n, wherein, n is the integer more than zero, and 360 ° of * n are less than the anglec of rotation of the unmanned plane；When the nothing
When the man-machine anglec of rotation is equal to 360 °, then the current kinetic direction of the unmanned plane and first control-rod 30 are described the
The deviation between the direction of motion on one preset direction is zero, i.e., current fortune of the described unmanned plane on first preset direction
The dynamic direction of motion of the direction with first control-rod 30 on first preset direction is consistent.
In addition, the embodiment of the present invention additionally provides a kind of UAS, as shown in fig. 7, comprises unmanned plane 100 and control
Device 200, the control device 200 includes：First control-rod, the first detecting element and processing unit；
Wherein, first detecting element is used to detect the direction of motion of first control-rod on the first preset direction；
The processing unit is used to obtaining the first control-rod that first detecting element detects in the first preset direction
On the direction of motion, and the direction of motion based on first control-rod on the first preset direction controls the unmanned plane to exist
The direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction and described
One control-rod direction of motion on first preset direction is identical.
Specifically, in one embodiment of the invention, when first control-rod is moved forward, the unmanned plane to
Preceding flight；When first control-rod is moved rearwards by, the unmanned plane flies backward；When first control-rod is to left movement
When, the unmanned plane flies to the left, and when first control-rod is moved right, the unmanned plane flies to the right.Need explanation
, the heading all around of the unmanned plane is unmanned operators direction all around within the vision.
On the basis of above-described embodiment, in one embodiment of the invention, first preset direction includes described
The fore-and-aft direction within the vision of unmanned operators；In another embodiment of the present invention, first preset direction
Including unmanned operators' left and right directions within the vision；In yet another embodiment of the present invention, described first is pre-
Set direction includes that unmanned operators' fore-and-aft direction within the vision and the unmanned operators are within the vision
Left and right directions, in other embodiments of the invention, first preset direction can also be the unmanned operators visual field
In the range of other directions, the present invention this is not limited, specifically depend on the circumstances.
On the basis of any of the above-described embodiment, in one embodiment of the invention, first detecting element is preferred
It is global positioning system.But the present invention is not limited this, specifically depend on the circumstances.
On the basis of above-described embodiment, in one embodiment of the invention, the control device 200 also includes second
Control-rod；
First detecting element is additionally operable to the direction of motion of detection second control-rod on the second preset direction；
The processing unit is additionally operable to obtain the direction of motion of second control-rod on the second preset direction, and is based on
The direction of motion of second control-rod on second preset direction, controls the direction of rotation of the unmanned plane.
Optionally, in embodiments of the present invention, when second control-rod is transported along the positive direction of second preset direction
When dynamic, the unmanned plane turns clockwise；When second control-rod is moved along the negative direction of second preset direction, institute
State unmanned plane rotate counterclockwise；Wherein, the positive direction and negative direction of second preset direction are default parallel to described second
Two rightabouts in direction.
On the basis of above-described embodiment, in one embodiment of the invention, second control-rod is swingle, institute
The positive direction of the second preset direction is stated for clockwise, the negative direction of second preset direction is for counterclockwise；At this
In the other embodiment of invention, second control-rod can also be sliding bar, and the positive direction of second preset direction is cunning
The direction that lever is slided, the negative direction of second preset direction is another direction of sliding bar slip, and the present invention is right
This is not limited, and is specifically depended on the circumstances.
On the basis of above-described embodiment, in one embodiment of the invention, the unmanned plane also includes the second detection
Element, second detecting element is used to detect current kinetic direction of the unmanned plane on first preset direction.
On the basis of above-described embodiment, in one embodiment of the invention, the processing unit is additionally operable to：
Obtain the current kinetic of the unmanned plane that second detecting element detects on first preset direction
Direction；
Judge current kinetic direction of the unmanned plane on first preset direction with first control-rod in institute
Whether the direction of motion stated on the first preset direction is consistent；
When current kinetic direction of the unmanned plane on first preset direction with first control-rod described
When the direction of motion on first preset direction is inconsistent, motion side of the unmanned plane on first preset direction is adjusted
To making current kinetic direction of the unmanned plane on first preset direction pre- described first with first control-rod
The direction of motion on set direction is consistent.
It should be noted that on the basis of above-described embodiment, in one embodiment of the invention, the processing unit
Current kinetic direction of the unmanned plane on first preset direction directly can be obtained by second detecting element；
In another embodiment of the present invention, the processing unit can also be by recording the unmanned plane on the second preset direction
The anglec of rotation obtain the current kinetic direction of the unmanned plane.Such as when the anglec of rotation of the unmanned plane is less than 360 °, then
Between the direction of motion of the current kinetic direction of the unmanned plane and first control-rod 30 on first preset direction
Deviation then for the unmanned plane the anglec of rotation；When the anglec of rotation of the unmanned plane is more than 360 °, then the unmanned plane
The direction of motion on first preset direction of current kinetic direction and first control-rod 30 between deviation be then
The anglec of rotation of the unmanned plane subtracts 360 ° of * n, wherein, n is the integer more than zero, and 360 ° of * n are less than the unmanned plane
The anglec of rotation；When the anglec of rotation of the unmanned plane is equal to 360 °, then the current kinetic direction of the unmanned plane and described the
Deviation between the direction of motion of one control-rod 30 on first preset direction is zero, i.e., described unmanned plane is described first
The direction of motion phase one of current kinetic direction on preset direction with first control-rod 30 on first preset direction
Cause.
To sum up, the embodiment of the present invention is provided control device and the UAS including the control device, in control
During unmanned plane during flying, the direction of motion of the unmanned plane on first preset direction is all the time with first control-rod in institute
The direction of motion stated on the first preset direction is identical, and without realizing the school in direction by recognizing the indicator lamp on unmanned plane
It is accurate, it is to avoid when flying distance farther out when, cause what manipulation slipped up to show due to the indicator lamp that cannot be accurately identified on unmanned plane
As reducing the manipulation fault rate during control unmanned plane during flying.
Various pieces are described by the way of progressive in this specification, and what each some importance was illustrated is and other parts
Difference, between various pieces identical similar portion mutually referring to.
The foregoing description of the disclosed embodiments, enables professional and technical personnel in the field to realize or uses the present invention.
Various modifications to these embodiments will be apparent for those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, the present invention
Embodiment illustrated herein is not intended to be limited to, and is to fit to consistent with principles disclosed herein and features of novelty
Scope most wide.
Claims (17)
1. a kind of information processing method, is applied to unmanned plane, it is characterised in that the method includes：
Obtain the direction of motion of first control-rod on the first preset direction；
Based on the direction of motion of first control-rod on the first preset direction, control the unmanned plane default described first
The direction of motion on direction, the direction of motion of the unmanned plane on first preset direction is with first control-rod in institute
State the direction of motion on the first preset direction identical.
2. information processing method according to claim 1, it is characterised in that first preset direction includes：The nothing
Human-machine operation person fore-and-aft direction within the vision and/or the unmanned operators left and right directions within the vision.
3. information processing method according to claim 1, it is characterised in that the control-rod of the acquisition first is default first
The direction of motion on direction includes：
The direction of motion of first control-rod that acquisition global positioning system is detected on the first preset direction.
4. the information processing method according to claim any one of 1-3, it is characterised in that the method also includes：
Obtain the direction of motion of second control-rod on the second preset direction；
Based on the direction of motion of second control-rod on second preset direction, the rotation side of the unmanned plane is controlled
To.
5. information processing method according to claim 4, it is characterised in that when second control-rod is pre- along described second
When the positive direction of set direction is moved, the unmanned plane turns clockwise；When second control-rod is along second preset direction
Negative direction move when, the unmanned plane rotate counterclockwise；
Wherein, the positive direction and negative direction of second preset direction are two phase negative sides parallel to second preset direction
To.
6. information processing method according to claim 5, it is characterised in that the method also includes：
Obtain current kinetic direction of the unmanned plane on first preset direction；
Judge current kinetic direction of the unmanned plane on first preset direction with first control-rod described
Whether the direction of motion on one preset direction is consistent；
When current kinetic direction of the unmanned plane on first preset direction with first control-rod described first
When the direction of motion on preset direction is inconsistent, the direction of motion of the unmanned plane on first preset direction is adjusted, made
Current kinetic direction of the unmanned plane on first preset direction is with first control-rod in the described first default side
The upward direction of motion is consistent.
7. a kind of information processor, it is characterised in that including：
Acquiring unit, for obtaining the direction of motion of first control-rod on the first preset direction；
Control unit, for the direction of motion based on first control-rod on the first preset direction, controls the unmanned plane
The direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction with it is described
First control-rod direction of motion on first preset direction is identical.
8. information processor according to claim 7, it is characterised in that the acquiring unit is additionally operable to obtain second to be controlled
The direction of motion of the bar processed on the second preset direction；
Described control unit is additionally operable to, based on the direction of motion of second control-rod on second preset direction, control institute
State the direction of rotation of unmanned plane.
9. information processor according to claim 8, it is characterised in that the acquiring unit is additionally operable to obtain the nothing
The man-machine current kinetic direction on first preset direction；
Described control unit be additionally operable to judge current kinetic direction of the unmanned plane on first preset direction with it is described
Whether the direction of motion of first control-rod on first preset direction is consistent, when the unmanned plane is in the described first default side
When the direction of motion of the upward current kinetic direction with first control-rod on first preset direction is inconsistent, regulation
The direction of motion of the unmanned plane on first preset direction, makes the unmanned plane working as on first preset direction
The direction of motion of the preceding direction of motion with first control-rod on first preset direction is consistent.
10. a kind of control device, it is characterised in that including：First control-rod, the first detecting element and processing unit, wherein, institute
State the first detecting element for detect the direction of motion of first control-rod on the first preset direction；
The processing unit is used to obtaining the first control-rod that first detecting element detects on the first preset direction
The direction of motion, and the direction of motion based on first control-rod on the first preset direction, control the unmanned plane described
The direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction and the described first control
Bar processed direction of motion on first preset direction is identical.
11. control devices according to claim 10, it is characterised in that the control device also includes the second control-rod；
First detecting element is additionally operable to the direction of motion of detection second control-rod on the second preset direction；
The processing unit is additionally operable to obtain the direction of motion of second control-rod on the second preset direction, and based on described
The direction of motion of second control-rod on second preset direction, controls the direction of rotation of the unmanned plane.
12. control devices according to claim 11, it is characterised in that the processing unit is additionally operable to：
Obtain current kinetic direction of the unmanned plane on first preset direction；
Judge current kinetic direction of the unmanned plane on first preset direction with first control-rod described
Whether the direction of motion on one preset direction is consistent；
When current kinetic direction of the unmanned plane on first preset direction with first control-rod described first
When the direction of motion on preset direction is inconsistent, the direction of motion of the unmanned plane on first preset direction is adjusted, made
Current kinetic direction of the unmanned plane on first preset direction is with first control-rod in the described first default side
The upward direction of motion is consistent.
13. control device according to claim any one of 10-12, it is characterised in that first detecting element is complete
Ball alignment system.
14. a kind of UASs, it is characterised in that including unmanned plane and control device, the control device includes：First control
Bar processed, the first detecting element and processing unit；
Wherein, first detecting element is used to detect the direction of motion of first control-rod on the first preset direction；
The processing unit is used to obtaining the first control-rod that first detecting element detects on the first preset direction
The direction of motion, and the direction of motion based on first control-rod on the first preset direction, control the unmanned plane described
The direction of motion on first preset direction, the direction of motion of the unmanned plane on first preset direction and the described first control
Bar processed direction of motion on first preset direction is identical.
15. UASs according to claim 14, it is characterised in that the control device also includes the second control
Bar；
First detecting element is additionally operable to the direction of motion of detection second control-rod on the second preset direction；
The processing unit is additionally operable to obtain the direction of motion of second control-rod on the second preset direction, and based on described
The direction of motion of second control-rod on second preset direction, controls the direction of rotation of the unmanned plane.
16. UASs according to claim 15, it is characterised in that the unmanned plane also includes the second detection unit
Part, second detecting element is used to detect current kinetic direction of the unmanned plane on first preset direction.
17. UASs according to claim 16, it is characterised in that the processing unit is additionally operable to：
Obtain the current kinetic direction of the unmanned plane that second detecting element detects on first preset direction；
Judge current kinetic direction of the unmanned plane on first preset direction with first control-rod described
Whether the direction of motion on one preset direction is consistent；
When current kinetic direction of the unmanned plane on first preset direction with first control-rod described first
When the direction of motion on preset direction is inconsistent, the direction of motion of the unmanned plane on first preset direction is adjusted, made
Current kinetic direction of the unmanned plane on first preset direction is with first control-rod in the described first default side
The upward direction of motion is consistent.
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