CN106155046A - Rocker assembly, remote control unit and flight system - Google Patents
Rocker assembly, remote control unit and flight system Download PDFInfo
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- CN106155046A CN106155046A CN201610442557.XA CN201610442557A CN106155046A CN 106155046 A CN106155046 A CN 106155046A CN 201610442557 A CN201610442557 A CN 201610442557A CN 106155046 A CN106155046 A CN 106155046A
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- chute
- induction zone
- stick
- aircraft
- rocker assembly
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- 230000006698 induction Effects 0.000 claims description 75
- 230000007423 decrease Effects 0.000 claims description 17
- 230000000630 rising effect Effects 0.000 claims description 16
- 230000000994 depressogenic effect Effects 0.000 claims description 5
- 230000011664 signaling Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 210000003811 finger Anatomy 0.000 description 2
- 210000004247 hand Anatomy 0.000 description 2
- 210000003813 thumb Anatomy 0.000 description 2
- 206010034719 Personality change Diseases 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 210000005224 forefinger Anatomy 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 210000004932 little finger Anatomy 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
- G05D1/0016—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement characterised by the operator's input device
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- 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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
- G05G9/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
- G05G9/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only
- G05G9/04—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously
- G05G9/047—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks
- G05G2009/04774—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks with additional switches or sensors on the handle
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
- G05G9/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
- G05G9/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only
- G05G9/04—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously
- G05G9/047—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks
- G05G2009/04777—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks with additional push or pull action on the handle
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Computing Systems (AREA)
- Mathematical Physics (AREA)
- Theoretical Computer Science (AREA)
- Toys (AREA)
- Mechanical Control Devices (AREA)
Abstract
The open a kind of rocker assembly of the present invention, described rocker assembly includes sensor, controller and a stick；A described stick has at least six kinds of operation states, six kinds of described operation states be respectively used to control the advance of aircraft, retrogressing, to the left, to the right, rise and down maneuver；Described sensor is for obtaining the mode of operation of described stick；Described controller electrically connects with described sensor, and the mode of operation of the described stick that described controller obtains according to described sensor sends and controls signal to described aircraft accordingly.The present invention also provides for a kind of remote control unit applying described rocker assembly and flight system.The technical scheme that the present invention provides aims to provide the simple rocker assembly of a kind of manipulation.
Description
Technical field
The present invention relates to a kind of rocker assembly and there is remote control unit and the flight system of described rocker assembly.
Background technology
At present, unmanned plane has been widely used for taking photo by plane and the every field such as detection, and the control for unmanned plane is generally adopted
Using remote controller control, the conventional remote controller major part of unmanned plane is hand-held, needs both hands to control two on remote controller respectively
Rocking bar realize the advance of unmanned plane, retrogressing, to the left, to the right, rise and decline amount to six direction motion control.Two rocking bars
Cooperating and could realize the flight of the skyborne any degree of freedom of unmanned plane, the manipulation process of remote controller is more complicated.
Summary of the invention
The main object of the present invention is to provide the simple rocker assembly of a kind of manipulation.
For achieving the above object, the rocker assembly that the present invention proposes includes sensor, controller and a stick；Described one
Stick has at least six kinds of operation states, six kinds of described operation states be respectively used to control the advance of aircraft, retrogressing, to
Left, to the right, rise and down maneuver；Described sensor is for obtaining the mode of operation of described stick；Described controller and institute
Stating sensor electrical connection, the mode of operation of the described stick that described controller obtains according to described sensor sends corresponding control
Signal processed is to described aircraft.
Preferably, described rocker assembly also includes six induction zones, is respectively induction zone, backward induction zone, to the left the most forward
Induction zone, to the right induction zone, rising induction zone and decline induction zone；When described stick is in above-mentioned induction zone, it is respectively used to
Control the advance of described aircraft, retrogressing, to the left, to the right, rise and down maneuver.
Preferably, described rocker assembly also includes base；Described base includes the first chute and the second chute；Described first
The middle part of chute is intersected with the middle part of described second chute, described second chute described first chute is divided into described in sense forward
District and described induction zone backward, described first chute described second chute is divided into described in induction zone and described sense to the right to the left
District.
Preferably, described base also includes that the 3rd chute, described stick also include upper and lower lifting parts and house on described
The host cavity of lower lifting parts, described host cavity is described 3rd chute, have in described 3rd chute described rising induction zone and
Described decline induction zone, described upper and lower lifting parts is flexible, to realize rising or falling of described aircraft in described host cavity.
Preferably, described first chute, described second chute and described 3rd chute are the most vertical.
Preferably, described stick include the press section being provided thereon, described press section include rise button and decline by
Key, described rising button is used for controlling described aircraft and carries out vertical motion, and described decline button is used for controlling described aircraft
Carry out down maneuver.
Preferably, described press section also includes turbo and deceleration button, described turbo be used for controlling described in fly
Row device accelerates flight, and described deceleration button is used for controlling the flight of described aircraft down.
Preferably, described stick also includes shaft-like main part, and the sidewall of described main part forms depressed area.
The present invention also provides for a kind of remote control unit, and including housing and described rocker assembly, described rocker assembly is located at described
Housing.
The present invention also provides for a kind of flight system, and including aircraft and described remote control unit, described remote control unit is used for controlling
Make the state of flight of described aircraft.
In technical scheme, a described stick has at least six kinds of operation states, six kinds of described manipulation shapes
State be respectively used to control the advance of aircraft, retrogressing, to the left, to the right, rise and down maneuver；By handling a described manipulation
Bar, can realize the flight of the skyborne any degree of freedom of unmanned plane, handles simple.
Accompanying drawing explanation
In order to be illustrated more clearly that the present embodiment or technical scheme of the prior art, below will be to embodiment or existing skill
In art description, the required accompanying drawing used is briefly described, it should be apparent that, the accompanying drawing in describing below is only the present invention
Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to according to
Structure shown in these accompanying drawings obtains other accompanying drawing.
Fig. 1 is the structural representation of the rocker assembly of the present invention；
Fig. 2 is the structural representation of the stick in the rocker assembly of the present invention.
Drawing reference numeral illustrates:
| Label | Title | Label | Title |
| 100 | Rocker assembly | 110 | Stick |
| 111 | Main part | 112 | Depressed area |
| 113 | Press section | 114 | Rise button |
| 115 | Decline button | 116 | Turbo |
| 117 | Deceleration button | 118 | Lifting parts up and down |
| 119 | 3rd chute | 130 | Base |
| 131 | First chute | 132 | Second chute |
| 133 | Limiting section | 134 | First pars contractilis |
| 135 | Second pars contractilis | 136 | Induction zone forward |
| 137 | Induction zone backward | 138 | Induction zone to the left |
| 139 | Induction zone backward |
The realization of the object of the invention, functional characteristics and advantage will in conjunction with the embodiments, are described further referring to the drawings.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the present embodiment, the technical scheme in the present embodiment is clearly and completely described,
Obviously, described embodiment is only a part of embodiment of the present invention rather than whole embodiments.Based in the present invention
Embodiment, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise,
Broadly fall into the scope of protection of the invention.
It is to be appreciated that directional instruction in the present embodiment (such as up, down, left, right, before and after ...) is only used for solving
Release under a certain particular pose (as shown in drawings) relative position relation between each parts, motion conditions etc., if this is specific
When attitude changes, then directionality instruction changes the most therewith.
It addition, in the present invention such as relating to the description of " first ", " second " etc. be only used for describe purpose, and it is not intended that
Indicate or imply its relative importance or the implicit quantity indicating indicated technical characteristic.Thus, define " first ",
The feature of " second " can express or implicitly include at least one this feature.In describing the invention, the containing of " multiple "
Justice is at least two, such as two, three etc., unless otherwise expressly limited specifically.
In the present invention, unless otherwise clearly defined and limited, term " connects ", " fixing " etc. should be interpreted broadly,
Such as, " fixing " can be fixing connection, it is also possible to be to removably connect, or integral；Can be to be mechanically connected, it is also possible to be
Electrical connection；Can be to be joined directly together, it is also possible to be indirectly connected to by intermediary, can be the connection or two of two element internals
The interaction relationship of individual element, unless otherwise clear and definite restriction.For the ordinary skill in the art, can basis
Concrete condition understands above-mentioned term concrete meaning in the present invention.
It addition, the technical scheme between each embodiment of the present invention can be combined with each other, but must be general with this area
Based on logical technical staff is capable of, when technical scheme combination occur conflicting maybe cannot realize time will be understood that this
The combination of technical scheme does not exists, the most not within the protection domain of application claims.
The present invention proposes a kind of rocker assembly 100.
Refer to Fig. 1, the rocker assembly 100 that the present invention proposes include sensor (not shown), controller (not shown) and
One stick 110；A described stick 110 has at least six kinds of operation states, and six kinds of described operation states are respectively used to control
The advance of aircraft, retrogressing, to the left, to the right, rise and down maneuver；Described sensor is for obtaining described stick 110
Mode of operation；Described controller electrically connects with described sensor, the described manipulation that described controller obtains according to described sensor
The mode of operation of bar 110 sends and controls signal to described aircraft accordingly.
In technical scheme, described stick 110 has at least six kinds of operation states, six kinds of described operation states
Be respectively used to control the advance of aircraft, retrogressing, to the left, to the right, rise and down maneuver；By handling a described stick
110, the flight of the skyborne any degree of freedom of unmanned plane can be realized, handle simple.
Described stick 110 can be located at both sides or the middle part of described rocker assembly 100, to adapt to making of different operator
By custom.
Heretofore described utilize a described stick 110 realize controlling the advance of aircraft, retrogressing, to the left, to
At least six kinds of manipulations such as the right side, rising and down maneuver, are not the flight of the steering by described stick 110 and aircraft
Direction carries out unique correspondence.The control direction to aircraft corresponding to the steering of the described stick 110 in the present invention
Can be customized according to the operating habit of operator, to meet the manipulation custom of operator.
Such as, it is accustomed to according to the manipulation of operator, pushes ahead described stick 110 and be possible not only to realize controlling aircraft
Souping up (i.e. aircraft forward flight) forward, it is also possible to according to operator customize, it is achieved control aircraft fly backward, to
Left flight, fly to the right, carry out vertical motion, or carry out any one in down maneuver.
Advance described stick 110 backward, it is possible to achieve control aircraft forward flight, backward flight, to the left flight, to
Right flight, carry out vertical motion, or carry out any one in down maneuver.
Accordingly, the described stick 110 of propelling of turning left, it is also not limited to realize the flare maneuver to the left of aircraft, also
Can be according to the needs of operator, it is achieved control aircraft forward flight, fly backward, fly to the right, carry out vertical motion, or
Carry out in down maneuver any one.
In like manner, advance to the right described stick 110, be pressed downward against described stick 110 and upwards carry described stick 110 also
It is not limited in controlling aircraft to fly to the right, carry out down maneuver and carry out vertical motion, all can realize controlling aircraft
Flight forward, fly backward, fly to the left, fly to the right, carry out vertical motion, or carry out in down maneuver any one or
Multiple, i.e. described stick 110 is carried out the Solid rocket engine in a direction, can be accustomed to handling according to the manipulation of operator
Customization, to realize controlling aircraft forward flight, flying backward, fly to the left, fly to the right, carry out vertical motion, or is carried out
Any one in down maneuver.
Preferably, described rocker assembly 100 also includes six induction zones, is respectively induction zone 136, backward induction zone forward
137, to the left induction zone 138, to the right induction zone 139, rise induction zone (not shown) and decline induction zone (not shown)；Described behaviour
When vertical pole 110 is in above-mentioned induction zone, be respectively used to control the advance of described aircraft, retrogressing, to the left, to the right, rise and under
Fall action.
Described sensor is for obtaining the mode of operation of described stick 110, and wherein, described sensor can be that pressure passes
Sensor, when described stick 110 is stirred toward each induction zone, described sensor sense described stick 110 operation state and
Obtain corresponding control signal.
The induction zone of described rocker assembly 100 is not limited in above-mentioned six induction zones, and described rocker assembly 100 is all right
On the basis of above-mentioned induction zone, set up four new induction zones, including left front induction zone, left back induction zone, right front induction zone,
Induction zone etc. behind the right side.Described stick 110 be in described left front induction zone for control described aircraft to left front to flight,
Described stick 110 is in described left back induction zone for controlling described aircraft to left back to flight, described stick 110
Be in front induction zone, the described right side for control described aircraft to right front to flight, after described stick 110 is in the described right side
Induction zone is used for controlling described aircraft to right back to flight.
Described stick 110 is also designed to 360 ° and stirs, to control the 360 ° of rotations in flight plane of described aircraft
Change one's profession into.
Certainly, in described rocker assembly 100, described sensor can also be believed by sensing the position of described stick 110
Number identify the manipulation demand of operator, such as, in each induction zone of described stick 110, be provided with multiple described sensor,
Each described sensor is for sensing the position signalling of described stick 110, and sends corresponding position signalling to described control
Device processed, described controller is according to the manipulation demand of the position signalling identification operator received, and sends aircraft accordingly
Control signal.
Preferably, described rocker assembly 100 also includes base 130；Described base 130 includes the first chute 131 and second
Chute 132；The middle part of described first chute 131 is intersected with the middle part of described second chute 132, and described second chute 132 is by institute
State the first chute 131 be divided into described in induction zone 136 and described induction zone 137 backward forward, described first chute 131 is by described
Two chutes 132 be divided into described in induction zone 138 and described induction zone 139 to the right to the left.
Incorporated by reference to reference to Fig. 2, it is preferable that described base 130 also includes that the 3rd chute 119, described stick 110 also include
Up and down lifting parts 118 and house the host cavity of described upper and lower lifting parts 118, described host cavity is the described 3rd sliding 119, described the
Having described rising induction zone and described decline induction zone in three chutes 119, described upper and lower lifting parts 118 is in described host cavity
Flexible, to realize rising or falling of described aircraft.
The middle part of described first chute 131 and described second chute 132 is intersected, in the present embodiment, and described second chute
132 described first chute 131 is divided into described in induction zone 136 and described induction zone backward forward, described first chute 131 is by institute
State the second chute 132 be divided into described in induction zone 138 and described induction zone 139 to the right to the left, described stick 110 dials to above-mentioned
During four induction zones, described controller sends flight directive forward, backward, to the left and to the right to described aircraft respectively.
Certainly, each chute on described rocker assembly 100 is not limited in said structure, and any bar chute is mutually handed over
Mistake, forms the multiple induction regions stirred or slide for described stick 110, be the most in like manner included in protection scope of the present invention it
In.
In a specific embodiment, the structure that described stick 110 uses is shaft-like, shaft-like described stick 110
One end is sliding end, described sliding end be used for sliding in described first chute 131 and described second chute 132, described up and down
Lifting parts 118 is for sliding in described 3rd chute 119.The initial position of described sliding end is positioned at described first chute 131
Crossover location with described second chute 132.Described operator handle described stick 110 away from the one of described sliding end
End.Induction zone 136, described induction zone backward 137, described induction zone 138 to the left forward described in described stick 110 is dialed to
And during described induction zone 139 to the right, operator, by applying thrust to described stick, makes described sliding end pushed to accordingly
Induction zone, to realize controlling the advance of described aircraft, retrogressing, the action flown to the left and to the right respectively.In order to described
Aircraft sends rising signals or dropping signal, and operator needs described upper and lower lifting parts 118 in described 3rd chute 119
It is lifted up or presses down on, above put forward described upper and lower lifting parts 118 and feel described upper and lower lifting parts 118 to be promoted to described rising
Answer district, or under press described upper and lower lifting parts 118 can realize so that described upper and lower lifting parts 118 is pushed to described decline induction zone
Control rising and the down maneuver of described aircraft.
Preferably, described first chute 131, described second chute 132 and described 3rd chute 119 are the most vertical.
Each chute is mutually perpendicular to meet the manipulation custom of operator, reduces error operations.
Preferably, described stick 110 includes that the press section 113 being provided thereon, described press section 113 include rising button
114 and decline button 115, described rising button 114 is used for controlling described aircraft and carries out vertical motion, described decline button
115 are used for controlling described aircraft carries out down maneuver.
In the present embodiment, described upper and lower lifting parts 118 is located in described press section 113.
Except use the mode carrying on described stick 110 and pressing down to realize to control described aircraft raising and lowering it
Outward, it is also possible to controlled the lifting of aircraft respectively by described rising button 114 and described decline button 115.
Preferably, described press section 113 also includes turbo 116 and deceleration button 117, presses described press section 113
Diverse location include pressing described turbo 116 and press described deceleration button 117.
Described press section 113 can in the form of a ring, and each button annular distribution is on described press section 113, it is to avoid button
Distribution is excessive, exceedes the active manipulation scope of thumb.
Certainly, each button can also on described main part 111 Arbitrary distribution, along as described in the length of stick 110
Directional spreding etc., within being the most in like manner included in protection scope of the present invention.
Preferably, described press section 113 also includes that turbo 116 and deceleration button 117, described turbo 116 are used
Accelerating flight in controlling described aircraft, described deceleration button 117 is used for controlling the flight of described aircraft down.
Preferably, described stick 110 also includes shaft-like main part 111, and the sidewall of described main part 111 forms depression
District 112.
Described main part 111, in shaft-like, forms described host cavity in it, described depressed area 112 makes described stick 110 shape
Become to hold induction zone, prevent operator when handling described stick 110, skid between hand and described stick 110.
Described upper and lower lifting parts 118 is located in described press section 113, due to arrange on described press section 113 multiple manipulation by
Key, therefore, the forefinger of operator, middle finger, the third finger and little finger of toe can be held in described depressed area 112, and the thumb of operator can
For operating buttons.
Each induction zone can also be respectively provided with telescopic limiting section 133, and described limiting section 133 includes being oppositely arranged
First pars contractilis 134 and the second pars contractilis 135, when a certain to described first chute of the described sliding end of described stick 110
Time slip in induction zone, operator applies thrust to described stick 110, described first pars contractilis 134 and described second is stretched
Portion 135 squeezes, and described stick 110 is from passing through between described first pars contractilis 134 and described second pars contractilis 135 and slipping into phase
The induction zone answered, now, described limiting section 133 is spacing to described stick 110, and operator can be by hands from described stick
Unclamp on 110, owing to described stick 110 is limited in described maneuvering area by described limiting section 133, therefore, described flight
Device will be always maintained at current state of flight, until operator by described stick 110 groups from current induction zone.
In order to make described stick 110 more easily control described first pars contractilis 134 and described second pars contractilis 135 to be pushed away
Opening, the both sides of described first pars contractilis 134 are respectively provided with chamfering, and the both sides of described second pars contractilis 135 are respectively provided with chamfering, because of
This, in bell mouth shape between described first pars contractilis 134 and described second pars contractilis 135.
The present invention also provides for a kind of remote control unit (not shown), including housing (not shown) and described rocker assembly 100, institute
State rocker assembly 100 and be located at described housing.Owing to described remote control unit have employed whole technical schemes of the present embodiment, the most extremely
Having all beneficial effects that the technical scheme of above-described embodiment is brought less, this is no longer going to repeat them.
The present invention also provides for a kind of flight system (not shown), including aircraft (not shown) and described remote control unit, institute
State remote control unit for controlling the state of flight of described aircraft.Owing to described flight system have employed whole skills of the present embodiment
Art scheme, the most at least has all beneficial effects that the technical scheme of above-described embodiment is brought, and this is no longer going to repeat them.
The foregoing is only the preferred embodiments of the present invention, not thereby limit the scope of the claims of the present invention, every at this
Under the inventive concept of invention, utilize the equivalent structure transformation that description of the invention and accompanying drawing content are made, or directly/indirectly use
The technical field relevant at other is included in the scope of patent protection of the present invention.
Claims (10)
1. a rocker assembly, it is characterised in that include sensor, controller and a stick；A described stick have to
Few six kinds of operation states, six kinds of described operation states be respectively used to control the advance of aircraft, retrogressing, to the left, to the right, rise and
Down maneuver；Described sensor is for obtaining the mode of operation of described stick；Described controller electrically connects with described sensor,
The mode of operation of the described stick that described controller obtains according to described sensor send control signal to accordingly described in fly
Row device.
2. rocker assembly as claimed in claim 1, it is characterised in that described rocker assembly also includes six induction zones, respectively
For induction zone forward, backward induction zone, to the left induction zone, to the right induction zone, rise induction zone and decline induction zone；Described manipulation
When bar is in above-mentioned induction zone, be respectively used to control the advance of described aircraft, retrogressing, to the left, to the right, rise and decline dynamic
Make.
3. rocker assembly as claimed in claim 2, it is characterised in that described rocker assembly also includes base；Described base bag
Include the first chute and the second chute；The middle part of described first chute is intersected with the middle part of described second chute, described second chute
Induction zone and described induction zone backward forward described in being divided into by described first chute, described second chute is divided by described first chute
Induction zone and described induction zone to the right to the left described in one-tenth.
4. rocker assembly as claimed in claim 3, it is characterised in that described base also includes the 3rd chute, described stick
Also including upper and lower lifting parts and house the host cavity of described upper and lower lifting parts, described host cavity is described 3rd chute, described
Having described rising induction zone and described decline induction zone in three chutes, described upper and lower lifting parts is flexible in described host cavity,
To realize rising or falling of described aircraft.
5. rocker assembly as claimed in claim 4, it is characterised in that described first chute, described second chute and described the
Three chutes are the most vertical.
6. the rocker assembly as described in any one in claim 1 to 5, it is characterised in that described stick includes being located at it
On press section, described press section include rise button and decline button, described rising button is used for controlling described aircraft and enters
Row vertical motion, described decline button is used for controlling described aircraft and carries out down maneuver.
7. rocker assembly as claimed in claim 6, it is characterised in that described press section also include turbo and slow down by
Key, described turbo is used for controlling described aircraft and accelerates flight, and described deceleration button is used for controlling described aircraft down
Flight.
8. rocker assembly as claimed in claim 6, it is characterised in that described stick also includes shaft-like main part, described
The sidewall of main part forms depressed area.
9. a remote control unit, it is characterised in that include housing and rocking bar group as claimed in any of claims 1 to 8 in one of claims
Part, described rocker assembly is located at described housing.
10. a flight system, it is characterised in that include aircraft and remote control unit as claimed in claim 9, described remote control
Device is for controlling the state of flight of described aircraft.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610442557.XA CN106155046A (en) | 2016-06-17 | 2016-06-17 | Rocker assembly, remote control unit and flight system |
| PCT/CN2016/107927 WO2017215199A1 (en) | 2016-06-17 | 2016-11-30 | Rocker assembly, remote control device and flight system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610442557.XA CN106155046A (en) | 2016-06-17 | 2016-06-17 | Rocker assembly, remote control unit and flight system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106155046A true CN106155046A (en) | 2016-11-23 |
Family
ID=57353328
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610442557.XA Pending CN106155046A (en) | 2016-06-17 | 2016-06-17 | Rocker assembly, remote control unit and flight system |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN106155046A (en) |
| WO (1) | WO2017215199A1 (en) |
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| CN106774416A (en) * | 2017-01-11 | 2017-05-31 | 联想(北京)有限公司 | Information processing method and device, control device, UAS |
| CN107481498A (en) * | 2017-09-05 | 2017-12-15 | 深圳市道通智能航空技术有限公司 | A kind of remote control |
| WO2017215199A1 (en) * | 2016-06-17 | 2017-12-21 | 深圳市元征科技股份有限公司 | Rocker assembly, remote control device and flight system |
| CN107510945A (en) * | 2017-09-05 | 2017-12-26 | 深圳市道通智能航空技术有限公司 | A kind of rocker actuator and the remote control with this rocker actuator |
| CN109992037A (en) * | 2019-05-08 | 2019-07-09 | 成都航空职业技术学院 | A kind of unmanned plane control stick |
| CN110865457A (en) * | 2019-11-15 | 2020-03-06 | 台州学院 | Unmanned aerial vehicle VR tourism system based on 5G transmission technology |
| CN112896491A (en) * | 2021-03-10 | 2021-06-04 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Vertical take-off and landing aircraft side lever control device and control method |
| CN113955085A (en) * | 2021-10-26 | 2022-01-21 | 上海磐拓航空科技服务有限公司 | Method for controlling aircraft track by multifunctional control rod |
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| WO2017215199A1 (en) * | 2016-06-17 | 2017-12-21 | 深圳市元征科技股份有限公司 | Rocker assembly, remote control device and flight system |
| CN106774416A (en) * | 2017-01-11 | 2017-05-31 | 联想(北京)有限公司 | Information processing method and device, control device, UAS |
| US11623157B2 (en) | 2017-09-05 | 2023-04-11 | Autel Robotics Co., Ltd. | Remote control |
| CN107481498A (en) * | 2017-09-05 | 2017-12-15 | 深圳市道通智能航空技术有限公司 | A kind of remote control |
| CN107510945A (en) * | 2017-09-05 | 2017-12-26 | 深圳市道通智能航空技术有限公司 | A kind of rocker actuator and the remote control with this rocker actuator |
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| CN110865457B (en) * | 2019-11-15 | 2021-08-06 | 台州学院 | Unmanned aerial vehicle VR tourism system based on 5G transmission technology |
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| CN113955085A (en) * | 2021-10-26 | 2022-01-21 | 上海磐拓航空科技服务有限公司 | Method for controlling aircraft track by multifunctional control rod |
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