WO2017215199A1 - Rocker assembly, remote control device and flight system - Google Patents

Rocker assembly, remote control device and flight system Download PDF

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Publication number
WO2017215199A1
WO2017215199A1 PCT/CN2016/107927 CN2016107927W WO2017215199A1 WO 2017215199 A1 WO2017215199 A1 WO 2017215199A1 CN 2016107927 W CN2016107927 W CN 2016107927W WO 2017215199 A1 WO2017215199 A1 WO 2017215199A1
Authority
WO
WIPO (PCT)
Prior art keywords
rocker assembly
aircraft
rising
button
controlling
Prior art date
Application number
PCT/CN2016/107927
Other languages
French (fr)
Chinese (zh)
Inventor
刘均
刘新
宋朝忠
欧阳张鹏
Original Assignee
深圳市元征科技股份有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by 深圳市元征科技股份有限公司 filed Critical 深圳市元征科技股份有限公司
Publication of WO2017215199A1 publication Critical patent/WO2017215199A1/en

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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

Definitions

  • the invention relates to a rocker assembly and a remote control device and flight system having the same.
  • drones have been widely used in various fields such as aerial photography and detection.
  • the control of drones is usually controlled by remote control.
  • Most of the commonly used remote control of drones are hand-held, requiring two hands to separately control two on the remote control.
  • the rocker realizes the control of the six directions of the forward, backward, leftward, rightward, ascending and descending of the drone.
  • the two rockers cooperate to realize the freedom of the drone in the air, and the manipulation process of the remote controller is complicated.
  • the rocker assembly of the present invention comprises a sensor, a controller and a joystick;
  • the joystick has at least six operating states, and the six operating states are respectively used to control the forward and backward of the aircraft, a leftward, rightward, rising and falling motion;
  • the sensor is configured to acquire an operating state of the joystick;
  • the controller is electrically coupled to the sensor, and the controller is based on the joystick acquired by the sensor The operational status issues a corresponding control signal to the aircraft.
  • the rocker assembly further includes six sensing regions, which are a forward sensing region, a backward sensing region, a left sensing region, a right sensing region, a rising sensing region, and a falling sensing region;
  • the sensing zone is used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft, respectively.
  • the rocker assembly further includes a base; the base includes a first sliding slot and a second sliding slot; a middle portion of the first sliding slot intersects a middle portion of the second sliding slot, the second sliding The slot divides the first chute into the forward sensing area and the backward sensing area, and the first chute divides the second chute into the left sensing area and the right sensing area .
  • the base further includes a third sliding slot
  • the operating lever further includes an upper and lower lifting portion and a receiving cavity for receiving the upper and lower lifting portions
  • the receiving cavity is the third sliding slot
  • the third sliding The rising sensing area and the falling sensing area are arranged in the slot, and the upper and lower lifting parts are telescoped in the receiving cavity to achieve the ascent or descent of the aircraft.
  • the first chute, the second chute and the third chute are perpendicular to each other.
  • the joystick includes a pressing portion disposed thereon, the pressing portion includes a rising button and a falling button, the rising button is configured to control the aircraft to perform a rising motion, and the lowering button is configured to control the The aircraft performs a descending action.
  • the pressing portion further comprises an acceleration button for controlling the aircraft to accelerate flight, and a deceleration button for controlling the aircraft to decelerate the flight.
  • the lever further includes a rod-shaped body portion, and a side wall of the body portion forms a recessed portion.
  • the present invention also provides a remote control device including a housing and the rocker assembly, the rocker assembly being disposed in the housing.
  • the present invention also provides a flight system including an aircraft and the remote control device for controlling the flight state of the aircraft.
  • one of the joysticks has at least six operating states, and the six operating states are respectively used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft;
  • the joystick can realize the flight of any degree of freedom of the drone in the air, and the operation is simple.
  • Figure 1 is a schematic structural view of a rocker assembly of the present invention
  • FIG. 2 is a schematic view showing the structure of a joystick in the rocker assembly of the present invention.
  • first, second, and the like in the present invention are used for the purpose of description only, and are not to be construed as indicating or implying their relative importance or implicitly indicating the number of technical features indicated.
  • features defining “first” or “second” may include at least one of the features, either explicitly or implicitly.
  • the meaning of "a plurality” is at least two, such as two, three, etc., unless specifically defined otherwise.
  • the terms "connected”, “fixed” and the like should be understood broadly, unless otherwise clearly defined and limited.
  • “fixed” may be a fixed connection, or may be a detachable connection, or may be integrated; It may be a mechanical connection or an electrical connection; it may be directly connected or indirectly connected through an intermediate medium, and may be an internal connection of two elements or an interaction relationship of two elements unless explicitly defined otherwise.
  • the specific meanings of the above terms in the present invention can be understood on a case-by-case basis.
  • the present invention provides a rocker assembly 100.
  • the rocker assembly 100 of the present invention includes a sensor (not shown), a controller (not shown), and a joystick 110;
  • the joystick 110 has at least six operating states, six The manipulation states are respectively used to control forward, backward, leftward, rightward, ascending and descending actions of the aircraft;
  • the sensor is configured to acquire an operating state of the joystick 110;
  • the controller is electrically connected to the sensor, The controller sends a corresponding control signal to the aircraft according to the operating state of the joystick 110 acquired by the sensor.
  • the joystick 110 has at least six operating states, and the six operating states are respectively used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft;
  • the joystick 110 can realize the flight of any degree of freedom of the drone in the air, and the operation is simple.
  • the joysticks 110 may be disposed on both sides or in the middle of the rocker assembly 100 to accommodate the habits of different operators.
  • one of the joysticks 110 in the present invention achieves at least six manipulations of controlling the forward, backward, leftward, rightward, ascending and descending actions of the aircraft, not the steering direction of the joystick 110 and the aircraft.
  • the direction of flight is uniquely matched.
  • the control direction of the aircraft corresponding to the steering direction of the joystick 110 in the present invention can be customized according to the operator's operating habits to conform to the operator's manipulation habits.
  • advancing the joystick 110 can not only control the aircraft to increase the horsepower forward (ie, the aircraft flies forward), but also can control the aircraft to fly backwards according to the operator's customization. Left-flying, flying to the right, performing an ascending motion, or performing any of the descending motions.
  • Advancing the joystick 110 in the backward direction can control either the forward flight, the backward flight, the left flight, the rightward flight, the ascending motion, or the descending motion.
  • pushing the joystick 110 to the left is not limited to realizing the leftward flying motion of the aircraft, but also controlling the forward flight, backward flight, rightward flight, and ascending motion of the aircraft according to the needs of the operator. , or perform any of the descending actions.
  • propelling the joystick 110 to the right, pressing the joystick 110 downward, and lifting the joystick 110 upwardly are not limited to controlling the flight of the aircraft to the right, performing the descending motion, and performing the ascending motion.
  • the aircraft may fly forward, backward, fly to the left, fly to the right, perform an ascending motion, or perform any one or more of the descending actions, that is, one-way propulsion control of the joystick 110 may be performed according to
  • the manipulating habit of the operator is manipulated and customized to control any one of the forward flight, the backward flight, the left flight, the rightward flight, the ascending motion, or the descending motion.
  • the rocker assembly 100 further includes six sensing regions, which are a forward sensing region 136, a backward sensing region 137, a left sensing region 138, a right sensing region 139, and a rising sensing region (not shown). And a descent sensing area (not shown); when the joystick 110 is in the sensing area, it is used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft, respectively.
  • six sensing regions which are a forward sensing region 136, a backward sensing region 137, a left sensing region 138, a right sensing region 139, and a rising sensing region (not shown).
  • a descent sensing area (not shown); when the joystick 110 is in the sensing area, it is used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft, respectively.
  • the sensor is configured to acquire an operating state of the joystick 110, wherein the sensor may be a pressure sensor that senses manipulation of the joystick 110 when the joystick 110 is toggled toward each sensing zone The status is obtained and the corresponding control signal is obtained.
  • the sensing area of the rocker assembly 100 is not limited to the above six sensing areas.
  • the rocker assembly 100 can also add four new sensing areas on the basis of the sensing area, including the left front sensing area and the left rear sensing area. Zone, right front sensing zone, right rear sensing zone, etc.
  • the joystick 110 is in the left front sensing area for controlling the aircraft to fly to the left front direction
  • the joystick 110 is in the left rear sensing area for controlling the aircraft to fly to the left rear direction
  • the joystick 110 is in the right front sensing area for controlling the aircraft to fly to the right front direction
  • the joystick 110 is in the right rear sensing area for controlling the aircraft to fly to the right rear direction.
  • the joystick 110 can also be designed to be 360° toggled to control the aircraft to travel 360° in the plane of flight.
  • the sensor can also recognize the manipulation requirement of the operator by sensing the position signal of the joystick 110.
  • the plurality of sensing regions of the joystick 110 are provided. a sensor, each of the sensors for sensing a position signal of the joystick 110 and transmitting a corresponding position signal to the controller, the controller identifying an operator's manipulation requirement based on the received position signal, And send corresponding control signals to the aircraft.
  • the rocker assembly 100 further includes a base 130; the base 130 includes a first sliding slot 131 and a second sliding slot 132; a middle portion of the first sliding slot 131 and a middle portion of the second sliding slot 132 Intersecting, the second chute 132 divides the first chute 131 into the forward sensing area 136 and the backward sensing area 137, and the first chute 131 divides the second chute 132 into The left sensing area 138 and the right sensing area 139.
  • the base 130 further includes a third sliding slot 119.
  • the operating lever 110 further includes an upper and lower lifting portion 118 and a receiving cavity for receiving the upper and lower lifting portions 118.
  • the third sliding slot 119 has the rising sensing area and the falling sensing area, and the upper and lower lifting parts 118 are telescoped in the receiving cavity to realize the ascending or descending of the aircraft. .
  • the first chute 131 intersects the middle of the second chute 132.
  • the second chute 132 divides the first chute 131 into the forward sensing area 136 and In the backward sensing area, the first chute 131 divides the second chute 132 into the left sensing area 138 and the right sensing area 139, and the joystick 110 is toggled to the above four In the sensing area, the controller issues flight instructions to the aircraft forward, backward, leftward, and rightward, respectively.
  • each of the sliding grooves on the rocker assembly 100 is not limited to the above structure, and any one of the sliding grooves is mutually staggered to form a plurality of sensing regions for the joystick 110 to be slid or slid, and the same is included in the present invention.
  • any one of the sliding grooves is mutually staggered to form a plurality of sensing regions for the joystick 110 to be slid or slid, and the same is included in the present invention.
  • the lever 110 is configured in a rod shape, and one end of the lever-shaped lever 110 is a sliding end, and the sliding end is used in the first chute 131 and the first The two chutes 132 slide, and the upper and lower lifting portions 118 are used for sliding in the third chute 119.
  • the initial position of the sliding end is located at an intersection of the first sliding slot 131 and the second sliding slot 132. The operator manipulates one end of the joystick 110 away from the sliding end.
  • the operator In order to send a rising signal or a falling signal to the aircraft, the operator needs to lift the upper and lower lifting portions 118 upward or downward in the third sliding slot 119, and lift up the upper and lower lifting portions 118 to The up and down lifting portion 118 is lifted to the rising sensing region, or the upper and lower lifting portions 118 are pressed to push the upper and lower lifting portions 118 to the descending sensing region to control the ascending and descending actions of the aircraft.
  • the first chute 131, the second chute 132 and the third chute 119 are perpendicular to each other.
  • Each chute is perpendicular to each other in accordance with the operator's manipulation habits, reducing mishandling.
  • the joystick 110 includes a pressing portion 113 disposed thereon, the pressing portion 113 includes a rising button 114 and a falling button 115, and the rising button 114 is configured to control the aircraft to perform a rising motion, the descending The button 115 is used to control the aircraft to perform a lowering action.
  • the pressing portion 113 is provided on the upper and lower lifting portions 118.
  • the raising and lowering of the aircraft can also be controlled by the up button 114 and the down button 115, respectively.
  • the pressing portion 113 further includes an acceleration button 116 and a deceleration button 117. Pressing the different positions of the pressing portion 113 includes pressing the acceleration button 116 and pressing the deceleration button 117.
  • the pressing portion 113 may be in a ring shape, and each button is annularly distributed on the pressing portion 113 to prevent the distribution range of the button from being too large, exceeding the flexible manipulation range of the thumb.
  • each button can also be arbitrarily distributed on the main body portion 111, such as along the length direction of the joystick 110, and the like is equally included in the protection scope of the present invention.
  • the pressing portion 113 further includes an acceleration button 116 for controlling the aircraft to accelerate flight, and a deceleration button 117 for controlling the aircraft to decelerate the flight.
  • the lever 110 further includes a rod-shaped main body portion 111, and a side wall of the main body portion 111 forms a recessed portion 112.
  • the main body portion 111 has a rod shape, and the receiving cavity is formed therein, and the recessed portion 112 forms the handle bar 110 to form a grip sensing area, preventing the operator from manipulating the joystick 110 when the hand is The joystick 110 is slipped between.
  • the pressing portion 113 is disposed on the upper and lower lifting portion 118. Since the pressing portion 113 is provided with a plurality of manipulation buttons, the index finger, the middle finger, the ring finger and the little finger of the operator can be gripped in the recessed area 112, the operator The thumb can be used to manipulate the buttons.
  • Each of the sensing regions may further be provided with a retractable limiting portion 133, and the limiting portion 133 includes a first telescopic portion 134 and a second telescopic portion 135 disposed oppositely, when the sliding end of the operating lever 110 is facing When a certain sensing area of the first chute slides, the operator applies a thrust to the operating lever 110 to squeeze the first telescopic portion 134 and the second telescopic portion 135, and the operating lever 110 The first telescopic portion 134 and the second telescopic portion 135 pass between and slide into the corresponding sensing regions.
  • the limiting portion 133 limits the operating lever 110, and the operator can take the hand from the The joystick 110 is released, and since the joystick 110 is limited to the manipulation area by the limiting portion 133, the aircraft will maintain the current flight state until the operator puts the joystick 110 dials away from the current sensing area.
  • the two sides of the first telescopic portion 134 are respectively chamfered, and the second telescopic The two sides of the portion 135 are respectively provided with chamfers. Therefore, the first expansion and contraction portion 134 and the second expansion and contraction portion 135 have a bell mouth shape.
  • the present invention also provides a remote control device (not shown) including a housing (not shown) and the rocker assembly 100, the rocker assembly 100 being disposed in the housing. Since the remote control device adopts all the technical solutions of the embodiment, at least all the beneficial effects brought by the technical solutions of the foregoing embodiments are not repeatedly described herein.
  • the present invention also provides a flight system (not shown) including an aircraft (not shown) and the remote control device for controlling the flight state of the aircraft. Since the flight system adopts all the technical solutions of the embodiment, at least all the beneficial effects brought by the technical solutions of the foregoing embodiments are not repeatedly described herein.

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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)
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  • Mechanical Control Devices (AREA)

Abstract

A rocker assembly (100), comprising a sensor, a controller, and an operating lever (110). The operating lever (110) has at least six operating states respectively used for controlling forward, backward, leftward, rightward, rising and descending actions of an aircraft. The sensor is used for obtaining the operating states of the operating lever (110). The controller is electrically connected to the sensor, and sends corresponding control signals to the aircraft according to the operating states of the operating lever (110) obtained by the sensor. Also provided is a remote control device applying the rocker assembly (100) and a flight system. The technical solution aims to provide a rocker assembly (100) easy to operate.

Description

摇杆组件、遥控装置及飞行系统  Rocker assembly, remote control and flight system
技术领域Technical field
本发明涉及一种摇杆组件及具有所述摇杆组件的遥控装置及飞行系统。The invention relates to a rocker assembly and a remote control device and flight system having the same.
背景技术Background technique
目前，无人机已经广泛应用于航拍及检测等各个领域，对于无人机的控制通常采用遥控器控制，无人机的常用遥控器大部分为手持式，需要双手分别控制遥控器上的两个摇杆实现无人机的前进、后退、向左、向右、上升及下降共计六个方向运动的控制。两个摇杆相互配合才能实现无人机在空中的任意自由度的飞行，遥控器的操纵过程较复杂。At present, drones have been widely used in various fields such as aerial photography and detection. The control of drones is usually controlled by remote control. Most of the commonly used remote control of drones are hand-held, requiring two hands to separately control two on the remote control. The rocker realizes the control of the six directions of the forward, backward, leftward, rightward, ascending and descending of the drone. The two rockers cooperate to realize the freedom of the drone in the air, and the manipulation process of the remote controller is complicated.
发明内容Summary of the invention
本发明的主要目的是提供一种操纵简单的摇杆组件。It is a primary object of the present invention to provide a rocker assembly that is simple to handle.
为实现上述目的，本发明提出的摇杆组件包括传感器、控制器及一操纵杆；所述一操纵杆具有至少六种操纵状态，六种所述操纵状态分别用于控制飞行器的前进、后退、向左、向右、上升及下降动作；所述传感器用于获取所述操纵杆的操作状态；所述控制器与所述传感器电连接，所述控制器根据所述传感器获取的所述操纵杆的操作状态发出相应的控制信号至所述飞行器。To achieve the above object, the rocker assembly of the present invention comprises a sensor, a controller and a joystick; the joystick has at least six operating states, and the six operating states are respectively used to control the forward and backward of the aircraft, a leftward, rightward, rising and falling motion; the sensor is configured to acquire an operating state of the joystick; the controller is electrically coupled to the sensor, and the controller is based on the joystick acquired by the sensor The operational status issues a corresponding control signal to the aircraft.
优选地，所述摇杆组件还包括六个感应区，分别为向前感应区、向后感应区、向左感应区、向右感应区、上升感应区及下降感应区；所述操纵杆处于上述感应区时，分别用于控制所述飞行器的前进、后退、向左、向右、上升及下降动作。Preferably, the rocker assembly further includes six sensing regions, which are a forward sensing region, a backward sensing region, a left sensing region, a right sensing region, a rising sensing region, and a falling sensing region; The sensing zone is used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft, respectively.
优选地，所述摇杆组件还包括底座；所述底座包括第一滑槽及第二滑槽；所述第一滑槽的中部与所述第二滑槽的中部相交，所述第二滑槽将所述第一滑槽分成所述向前感应区和所述向后感应区，所述第一滑槽将所述第二滑槽分成所述向左感应区和所述向右感应区。Preferably, the rocker assembly further includes a base; the base includes a first sliding slot and a second sliding slot; a middle portion of the first sliding slot intersects a middle portion of the second sliding slot, the second sliding The slot divides the first chute into the forward sensing area and the backward sensing area, and the first chute divides the second chute into the left sensing area and the right sensing area .
优选地，所述底座还包括第三滑槽，所述操纵杆还包括上下提升部及收容所述上下提升部的收容腔，所述收容腔为所述第三滑槽，所述第三滑槽内具有所述上升感应区及所述下降感应区，所述上下提升部于所述收容腔内伸缩，以实现所述飞行器的上升或下降。Preferably, the base further includes a third sliding slot, the operating lever further includes an upper and lower lifting portion and a receiving cavity for receiving the upper and lower lifting portions, the receiving cavity is the third sliding slot, the third sliding The rising sensing area and the falling sensing area are arranged in the slot, and the upper and lower lifting parts are telescoped in the receiving cavity to achieve the ascent or descent of the aircraft.
优选地，所述第一滑槽、所述第二滑槽及所述第三滑槽两两垂直。Preferably, the first chute, the second chute and the third chute are perpendicular to each other.
优选地，所述操纵杆包括设于其上的按压部，所述按压部包括上升按键和下降按键，所述上升按键用于控制所述飞行器进行上升动作，所述下降按键用于控制所述飞行器进行下降动作。Preferably, the joystick includes a pressing portion disposed thereon, the pressing portion includes a rising button and a falling button, the rising button is configured to control the aircraft to perform a rising motion, and the lowering button is configured to control the The aircraft performs a descending action.
优选地，所述按压部还包括加速按键和减速按键，所述加速按键用于控制所述飞行器加速飞行，所述减速按键用于控制所述飞行器减速飞行。 Preferably, the pressing portion further comprises an acceleration button for controlling the aircraft to accelerate flight, and a deceleration button for controlling the aircraft to decelerate the flight.
优选地，所述操纵杆还包括杆状的主体部，所述主体部的侧壁形成凹陷区。Preferably, the lever further includes a rod-shaped body portion, and a side wall of the body portion forms a recessed portion.
本发明还提供一种遥控装置，包括壳体和所述摇杆组件，所述摇杆组件设于所述壳体。The present invention also provides a remote control device including a housing and the rocker assembly, the rocker assembly being disposed in the housing.
本发明还提供一种飞行系统，包括飞行器和所述遥控装置，所述遥控装置用于控制所述飞行器的飞行状态。The present invention also provides a flight system including an aircraft and the remote control device for controlling the flight state of the aircraft.
本发明的技术方案中，一个所述操纵杆具有至少六种操纵状态，六种所述操纵状态分别用于控制飞行器的前进、后退、向左、向右、上升及下降动作；通过操纵一个所述操纵杆，即能实现无人机在空中的任意自由度的飞行，操纵简单。In the technical solution of the present invention, one of the joysticks has at least six operating states, and the six operating states are respectively used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft; The joystick can realize the flight of any degree of freedom of the drone in the air, and the operation is simple.
附图说明DRAWINGS
为了更清楚地说明本实施例或现有技术中的技术方案，下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍，显而易见地，下面描述中的附图仅仅是本发明的一些实施例，对于本领域普通技术人员来讲，在不付出创造性劳动的前提下，还可以根据这些附图示出的结构获得其他的附图。In order to more clearly illustrate the present embodiment or the technical solutions in the prior art, the drawings used in the embodiments or the description of the prior art will be briefly described below. Obviously, the drawings in the following description are merely Some of the embodiments of the present invention can be obtained by those skilled in the art from the structure shown in the drawings without any inventive effort.
图1为本发明的摇杆组件的结构示意图；Figure 1 is a schematic structural view of a rocker assembly of the present invention;
图2为本发明的摇杆组件中的操纵杆的结构示意图。2 is a schematic view showing the structure of a joystick in the rocker assembly of the present invention.
附图标号说明：Description of the reference numerals:
标号Label 名称name 标号Label 名称name
100100 摇杆组件Rocker assembly 110110 操纵杆Joystick
111111 主体部Main body 112112 凹陷区Sag area
113113 按压部Pressing part 114114 上升按键Rise button
115115 下降按键Drop button 116116 加速按键Acceleration button
117117 减速按键Deceleration button 118118 上下提升部Up and down lift
119119 第三滑槽Third chute 130130 底座Base
131131 第一滑槽First chute 132132 第二滑槽Second chute
133133 限位部Limiting department 134134 第一伸缩部First expansion joint
135135 第二伸缩部Second expansion joint 136136 向前感应区Forward sensing area
137137 向后感应区Backward sensing area 138138 向左感应区Left sensing area
139139 向后感应区Backward sensing area
本发明目的的实现、功能特点及优点将结合实施例，参照附图做进一步说明。The implementation, functional features, and advantages of the present invention will be further described in conjunction with the embodiments.
具体实施方式detailed description
下面将结合本实施例中的附图，对本实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明的一部分实施例，而不是全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例，都属于本发明保护的范围。The technical solutions in the present embodiment will be clearly and completely described in the following with reference to the drawings in the embodiments. It is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without creative efforts are within the scope of the present invention.
需要说明，本实施例中所有方向性指示（诸如上、下、左、右、前、后……）仅用于解释在某一特定姿态（如附图所示）下各部件之间的相对位置关系、运动情况等，如果该特定姿态发生改变时，则该方向性指示也相应地随之改变。It should be noted that all directional indications (such as up, down, left, right, front, back, ...) in this embodiment are only used to explain the relative relationship between the components in a certain posture (as shown in the drawing). The positional relationship, the motion situation, and the like, if the specific posture changes, the directional indication also changes accordingly.
另外，在本发明中如涉及“第一”、“第二”等的描述仅用于描述目的，而不能理解为指示或暗示其相对重要性或者隐含指明所指示的技术特征的数量。由此，限定有“第一”、“第二”的特征可以明示或者隐含地包括至少一个该特征。在本发明的描述中，“多个”的含义是至少两个，例如两个，三个等，除非另有明确具体的限定。In addition, the descriptions of "first", "second", and the like in the present invention are used for the purpose of description only, and are not to be construed as indicating or implying their relative importance or implicitly indicating the number of technical features indicated. Thus, features defining "first" or "second" may include at least one of the features, either explicitly or implicitly. In the description of the present invention, the meaning of "a plurality" is at least two, such as two, three, etc., unless specifically defined otherwise.
在本发明中，除非另有明确的规定和限定，术语“连接”、“固定”等应做广义理解，例如，“固定”可以是固定连接，也可以是可拆卸连接，或成一体；可以是机械连接，也可以是电连接；可以是直接相连，也可以通过中间媒介间接相连，可以是两个元件内部的连通或两个元件的相互作用关系，除非另有明确的限定。对于本领域的普通技术人员而言，可以根据具体情况理解上述术语在本发明中的具体含义。In the present invention, the terms "connected", "fixed" and the like should be understood broadly, unless otherwise clearly defined and limited. For example, "fixed" may be a fixed connection, or may be a detachable connection, or may be integrated; It may be a mechanical connection or an electrical connection; it may be directly connected or indirectly connected through an intermediate medium, and may be an internal connection of two elements or an interaction relationship of two elements unless explicitly defined otherwise. For those skilled in the art, the specific meanings of the above terms in the present invention can be understood on a case-by-case basis.
另外，本发明各个实施例之间的技术方案可以相互结合，但是必须是以本领域普通技术人员能够实现为基础，当技术方案的结合出现相互矛盾或无法实现时应当认为这种技术方案的结合不存在，也不在本发明要求的保护范围之内。In addition, the technical solutions between the various embodiments of the present invention may be combined with each other, but must be based on the realization of those skilled in the art, and the combination of technical solutions should be considered when the combination of technical solutions is contradictory or impossible to implement. It does not exist and is not within the scope of protection required by the present invention.
本发明提出一种摇杆组件100。The present invention provides a rocker assembly 100.
请参照图1，本发明提出的摇杆组件100包括传感器（图未示）、控制器（图未示）及一操纵杆110；所述一操纵杆110具有至少六种操纵状态，六种所述操纵状态分别用于控制飞行器的前进、后退、向左、向右、上升及下降动作；所述传感器用于获取所述操纵杆110的操作状态；所述控制器与所述传感器电连接，所述控制器根据所述传感器获取的所述操纵杆110的操作状态发出相应的控制信号至所述飞行器。Referring to Figure 1, the rocker assembly 100 of the present invention includes a sensor (not shown), a controller (not shown), and a joystick 110; the joystick 110 has at least six operating states, six The manipulation states are respectively used to control forward, backward, leftward, rightward, ascending and descending actions of the aircraft; the sensor is configured to acquire an operating state of the joystick 110; the controller is electrically connected to the sensor, The controller sends a corresponding control signal to the aircraft according to the operating state of the joystick 110 acquired by the sensor.
本发明的技术方案中，所述操纵杆110具有至少六种操纵状态，六种所述操纵状态分别用于控制飞行器的前进、后退、向左、向右、上升及下降动作；通过操纵一个所述操纵杆110，即能实现无人机在空中的任意自由度的飞行，操纵简单。In the technical solution of the present invention, the joystick 110 has at least six operating states, and the six operating states are respectively used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft; The joystick 110 can realize the flight of any degree of freedom of the drone in the air, and the operation is simple.
所述操纵杆110可以设于所述摇杆组件100的两侧或中部，以适应不同操纵者的使用习惯。The joysticks 110 may be disposed on both sides or in the middle of the rocker assembly 100 to accommodate the habits of different operators.
本发明中所述的利用一个所述操纵杆110实现控制飞行器的前进、后退、向左、向右、上升及下降动作等至少六种操纵，并不是将所述操纵杆110的操纵方向与飞行器的飞行方向进行唯一对应。本发明中的所述操纵杆110的操纵方向所对应的对飞行器的控制方向可以根据操纵者的操作习惯进行定制，以符合操纵者的操纵习惯。The use of one of the joysticks 110 in the present invention achieves at least six manipulations of controlling the forward, backward, leftward, rightward, ascending and descending actions of the aircraft, not the steering direction of the joystick 110 and the aircraft. The direction of flight is uniquely matched. The control direction of the aircraft corresponding to the steering direction of the joystick 110 in the present invention can be customized according to the operator's operating habits to conform to the operator's manipulation habits.
例如，根据操纵者的操纵习惯，向前推进所述操纵杆110不仅可以实现控制飞行器向前加大马力（即飞行器向前飞行），也可以根据操纵者定制，实现控制飞行器向后飞行、向左飞行、向右飞行、进行上升动作，或进行下降动作中的任意一种。For example, according to the manipulation habit of the operator, advancing the joystick 110 can not only control the aircraft to increase the horsepower forward (ie, the aircraft flies forward), but also can control the aircraft to fly backwards according to the operator's customization. Left-flying, flying to the right, performing an ascending motion, or performing any of the descending motions.
往后推进所述操纵杆110，可以实现控制飞行器向前飞行、向后飞行、向左飞行、向右飞行、进行上升动作，或进行下降动作中的任意一种。Advancing the joystick 110 in the backward direction can control either the forward flight, the backward flight, the left flight, the rightward flight, the ascending motion, or the descending motion.
相应的，往左推进所述操纵杆110，也并不仅限于实现飞行器的向左飞行动作，还可以根据操纵者的需要，实现控制飞行器向前飞行、向后飞行、向右飞行、进行上升动作，或进行下降动作中的任意一种。Correspondingly, pushing the joystick 110 to the left is not limited to realizing the leftward flying motion of the aircraft, but also controlling the forward flight, backward flight, rightward flight, and ascending motion of the aircraft according to the needs of the operator. , or perform any of the descending actions.
同理，向右推进所述操纵杆110、向下压所述操纵杆110及向上提所述操纵杆110也并不仅限于控制飞行器向右飞行、进行下降动作及进行上升动作，均可以实现控制飞行器向前飞行、向后飞行、向左飞行、向右飞行、进行上升动作，或进行下降动作中的任意一种或多种，即对所述操纵杆110进行一个方向的推进控制，可以根据操纵者的操纵习惯进行操纵定制，以实现控制飞行器向前飞行、向后飞行、向左飞行、向右飞行、进行上升动作，或进行下降动作中的任意一种。Similarly, propelling the joystick 110 to the right, pressing the joystick 110 downward, and lifting the joystick 110 upwardly are not limited to controlling the flight of the aircraft to the right, performing the descending motion, and performing the ascending motion. The aircraft may fly forward, backward, fly to the left, fly to the right, perform an ascending motion, or perform any one or more of the descending actions, that is, one-way propulsion control of the joystick 110 may be performed according to The manipulating habit of the operator is manipulated and customized to control any one of the forward flight, the backward flight, the left flight, the rightward flight, the ascending motion, or the descending motion.
优选地，所述摇杆组件100还包括六个感应区，分别为向前感应区136、向后感应区137、向左感应区138、向右感应区139、上升感应区（图未示）及下降感应区（图未示）；所述操纵杆110处于上述感应区时，分别用于控制所述飞行器的前进、后退、向左、向右、上升及下降动作。Preferably, the rocker assembly 100 further includes six sensing regions, which are a forward sensing region 136, a backward sensing region 137, a left sensing region 138, a right sensing region 139, and a rising sensing region (not shown). And a descent sensing area (not shown); when the joystick 110 is in the sensing area, it is used to control the forward, backward, leftward, rightward, ascending and descending actions of the aircraft, respectively.
所述传感器用于获取所述操纵杆110的操作状态，其中，所述传感器可以为压力传感器，所述操纵杆110往各个感应区拨动时，所述传感器感测所述操纵杆110的操纵状态而获取相应的控制信号。The sensor is configured to acquire an operating state of the joystick 110, wherein the sensor may be a pressure sensor that senses manipulation of the joystick 110 when the joystick 110 is toggled toward each sensing zone The status is obtained and the corresponding control signal is obtained.
所述摇杆组件100的感应区并不仅限于上述六个感应区，所述摇杆组件100还可以在上述感应区的基础上，增设四个新的感应区，包括左前感应区、左后感应区、右前感应区、右后感应区等。所述操纵杆110处于所述左前感应区用于控制所述飞行器向左前方向飞行、所述操纵杆110处于所述左后感应区用于控制所述飞行器向左后方向飞行、所述操纵杆110处于所述右前感应区用于控制所述飞行器向右前方向飞行、所述操纵杆110处于所述右后感应区用于控制所述飞行器向右后方向飞行。The sensing area of the rocker assembly 100 is not limited to the above six sensing areas. The rocker assembly 100 can also add four new sensing areas on the basis of the sensing area, including the left front sensing area and the left rear sensing area. Zone, right front sensing zone, right rear sensing zone, etc. The joystick 110 is in the left front sensing area for controlling the aircraft to fly to the left front direction, the joystick 110 is in the left rear sensing area for controlling the aircraft to fly to the left rear direction, the joystick 110 is in the right front sensing area for controlling the aircraft to fly to the right front direction, and the joystick 110 is in the right rear sensing area for controlling the aircraft to fly to the right rear direction.
所述操纵杆110还可以设计为360°拨动，以控制所述飞行器在飞行平面内360°旋转行进。The joystick 110 can also be designed to be 360° toggled to control the aircraft to travel 360° in the plane of flight.
当然，所述摇杆组件100中，所述传感器还可以通过感应所述操纵杆110的位置信号来识别操纵者的操纵需求，例如，所述操纵杆110的各个感应区内设有多个所述传感器，每个所述传感器用于感应所述操纵杆110的位置信号，并将相应的位置信号发送至所述控制器，所述控制器根据接收到的位置信号识别操纵者的操纵需求，并对飞行器发出相应的控制信号。 Of course, in the rocker assembly 100, the sensor can also recognize the manipulation requirement of the operator by sensing the position signal of the joystick 110. For example, the plurality of sensing regions of the joystick 110 are provided. a sensor, each of the sensors for sensing a position signal of the joystick 110 and transmitting a corresponding position signal to the controller, the controller identifying an operator's manipulation requirement based on the received position signal, And send corresponding control signals to the aircraft.
优选地，所述摇杆组件100还包括底座130；所述底座130包括第一滑槽131及第二滑槽132；所述第一滑槽131的中部与所述第二滑槽132的中部相交，所述第二滑槽132将所述第一滑槽131分成所述向前感应区136和所述向后感应区137，所述第一滑槽131将所述第二滑槽132分成所述向左感应区138和所述向右感应区139。Preferably, the rocker assembly 100 further includes a base 130; the base 130 includes a first sliding slot 131 and a second sliding slot 132; a middle portion of the first sliding slot 131 and a middle portion of the second sliding slot 132 Intersecting, the second chute 132 divides the first chute 131 into the forward sensing area 136 and the backward sensing area 137, and the first chute 131 divides the second chute 132 into The left sensing area 138 and the right sensing area 139.
请结合参照图2，优选地，所述底座130还包括第三滑槽119，所述操纵杆110还包括上下提升部118及收容所述上下提升部118的收容腔，所述收容腔为所述第三滑119，所述第三滑槽119内具有所述上升感应区及所述下降感应区，所述上下提升部118于所述收容腔内伸缩，以实现所述飞行器的上升或下降。Referring to FIG. 2, the base 130 further includes a third sliding slot 119. The operating lever 110 further includes an upper and lower lifting portion 118 and a receiving cavity for receiving the upper and lower lifting portions 118. In the third sliding slot 119, the third sliding slot 119 has the rising sensing area and the falling sensing area, and the upper and lower lifting parts 118 are telescoped in the receiving cavity to realize the ascending or descending of the aircraft. .
所述第一滑槽131和所述第二滑槽132的中部相交，在本实施例中，所述第二滑槽132将所述第一滑槽131分为所述向前感应区136和所述向后感应区，所述第一滑槽131将所述第二滑槽132分为所述向左感应区138和所述向右感应区139，所述操纵杆110拨动至上述四个感应区时，所述控制器分别对所述飞行器发出向前、向后、向左及向右的飞行指令。The first chute 131 intersects the middle of the second chute 132. In this embodiment, the second chute 132 divides the first chute 131 into the forward sensing area 136 and In the backward sensing area, the first chute 131 divides the second chute 132 into the left sensing area 138 and the right sensing area 139, and the joystick 110 is toggled to the above four In the sensing area, the controller issues flight instructions to the aircraft forward, backward, leftward, and rightward, respectively.
当然，所述摇杆组件100上的各个滑槽并不仅限于上述结构，任意条滑槽相互交错，形成供所述操纵杆110拨动或滑动的多个感应区域，均同理包含在本发明的保护范围之内。Certainly, each of the sliding grooves on the rocker assembly 100 is not limited to the above structure, and any one of the sliding grooves is mutually staggered to form a plurality of sensing regions for the joystick 110 to be slid or slid, and the same is included in the present invention. Within the scope of protection.
在具体实施方式中，所述操纵杆110采用的结构为杆状，杆状的所述操纵杆110的一端为滑动端，所述滑动端用于在所述第一滑槽131及所述第二滑槽132内滑移，所述上下提升部118用于在所述第三滑槽119内滑移。所述滑动端的初始位置位于所述第一滑槽131和所述第二滑槽132的交叉位置。所述操纵者操纵所述操纵杆110的远离所述滑动端的一端。将所述操纵杆110拨动至所述向前感应区136、所述向后感应区137、所述向左感应区138及所述向右感应区139时，操纵者通过向所述操纵杆施加推力，使所述滑动端被推送至相应的感应区，以分别实现控制所述飞行器的前进、后退、向左及向右飞行的动作。为了向所述飞行器发出上升信号或下降信号，操纵者需要将所述上下提升部118在所述第三滑槽119内向上提升或向下按压，上提所述上下提升部118以将所述上下提升部118提升至所述上升感应区，或下压所述上下提升部118以将所述上下提升部118推送至所述下降感应区即可实现控制所述飞行器的上升及下降动作。In a specific embodiment, the lever 110 is configured in a rod shape, and one end of the lever-shaped lever 110 is a sliding end, and the sliding end is used in the first chute 131 and the first The two chutes 132 slide, and the upper and lower lifting portions 118 are used for sliding in the third chute 119. The initial position of the sliding end is located at an intersection of the first sliding slot 131 and the second sliding slot 132. The operator manipulates one end of the joystick 110 away from the sliding end. When the joystick 110 is toggled to the forward sensing zone 136, the backward sensing zone 137, the left sensing zone 138, and the right sensing zone 139, the operator passes the joystick A thrust is applied to cause the sliding end to be pushed to the corresponding sensing zone to effect an action of controlling the forward, backward, leftward, and rightward flight of the aircraft, respectively. In order to send a rising signal or a falling signal to the aircraft, the operator needs to lift the upper and lower lifting portions 118 upward or downward in the third sliding slot 119, and lift up the upper and lower lifting portions 118 to The up and down lifting portion 118 is lifted to the rising sensing region, or the upper and lower lifting portions 118 are pressed to push the upper and lower lifting portions 118 to the descending sensing region to control the ascending and descending actions of the aircraft.
优选地，所述第一滑槽131、所述第二滑槽132及所述第三滑槽119两两垂直。Preferably, the first chute 131, the second chute 132 and the third chute 119 are perpendicular to each other.
各个滑槽相互垂直符合操纵者的操纵习惯，降低误操纵。Each chute is perpendicular to each other in accordance with the operator's manipulation habits, reducing mishandling.
优选地，所述操纵杆110包括设于其上的按压部113，所述按压部113包括上升按键114和下降按键115，所述上升按键114用于控制所述飞行器进行上升动作，所述下降按键115用于控制所述飞行器进行下降动作。Preferably, the joystick 110 includes a pressing portion 113 disposed thereon, the pressing portion 113 includes a rising button 114 and a falling button 115, and the rising button 114 is configured to control the aircraft to perform a rising motion, the descending The button 115 is used to control the aircraft to perform a lowering action.
在本实施例中，所述按压部113设于所述上下提升部118。In the embodiment, the pressing portion 113 is provided on the upper and lower lifting portions 118.
除了使用所述操纵杆110上提和下压的方式来实现控制所述飞行器上升和下降之外，也可以通过所述上升按键114及所述下降按键115分别控制飞行器的升降。In addition to controlling the raising and lowering of the aircraft by using the lifting and lowering of the joystick 110, the raising and lowering of the aircraft can also be controlled by the up button 114 and the down button 115, respectively.
优选地，所述按压部113还包括加速按键116和减速按键117，按压所述按压部113的不同位置包括按压所述加速按键116和按压所述减速按键117。 Preferably, the pressing portion 113 further includes an acceleration button 116 and a deceleration button 117. Pressing the different positions of the pressing portion 113 includes pressing the acceleration button 116 and pressing the deceleration button 117.
所述按压部113可以呈环状，各个按键环状分布于所述按压部113上，避免按键的分布范围过大，超过大拇指的灵活操纵范围。The pressing portion 113 may be in a ring shape, and each button is annularly distributed on the pressing portion 113 to prevent the distribution range of the button from being too large, exceeding the flexible manipulation range of the thumb.
当然，各个按键也可以在所述主体部111上任意分布，如沿所述操纵杆110的长度方向分布等，均同理包含在本发明的保护范围之内。Of course, each button can also be arbitrarily distributed on the main body portion 111, such as along the length direction of the joystick 110, and the like is equally included in the protection scope of the present invention.
优选地，所述按压部113还包括加速按键116和减速按键117，所述加速按键116用于控制所述飞行器加速飞行，所述减速按键117用于控制所述飞行器减速飞行。 Preferably, the pressing portion 113 further includes an acceleration button 116 for controlling the aircraft to accelerate flight, and a deceleration button 117 for controlling the aircraft to decelerate the flight.
优选地，所述操纵杆110还包括杆状的主体部111，所述主体部111的侧壁形成凹陷区112。Preferably, the lever 110 further includes a rod-shaped main body portion 111, and a side wall of the main body portion 111 forms a recessed portion 112.
所述主体部111呈杆状，其内形成所述收容腔，所述凹陷区112使所述操纵杆110形成手握感应区，防止操纵者在操纵所述操纵杆110时，手部与所述操纵杆110之间打滑。The main body portion 111 has a rod shape, and the receiving cavity is formed therein, and the recessed portion 112 forms the handle bar 110 to form a grip sensing area, preventing the operator from manipulating the joystick 110 when the hand is The joystick 110 is slipped between.
所述按压部113设于所述上下提升部118，由于所述按压部113上设置多个操纵按键，因此，操纵者的食指、中指、无名指和小指可以握于所述凹陷区112，操纵者的大拇指可以用于操纵按键。 The pressing portion 113 is disposed on the upper and lower lifting portion 118. Since the pressing portion 113 is provided with a plurality of manipulation buttons, the index finger, the middle finger, the ring finger and the little finger of the operator can be gripped in the recessed area 112, the operator The thumb can be used to manipulate the buttons.
各个感应区还可以分别设置可伸缩的限位部133，所述限位部133包括相对设置的第一伸缩部134和第二伸缩部135，当所述操纵杆110的所述滑动端向所述第一滑槽的某一感应区滑动时，操纵者对所述操纵杆110施加推力，将所述第一伸缩部134和所述第二伸缩部135挤开，所述操纵杆110从所述第一伸缩部134和所述第二伸缩部135之间经过并滑入相应的感应区，此时，所述限位部133对所述操纵杆110限位，操纵者可以将手从所述操纵杆110上松开，由于所述操纵杆110被所述限位部133限位于所述操纵区域内，因此，所述飞行器将一直保持当前的飞行状态，直到操纵者将所述操纵杆110拨离当前的感应区。Each of the sensing regions may further be provided with a retractable limiting portion 133, and the limiting portion 133 includes a first telescopic portion 134 and a second telescopic portion 135 disposed oppositely, when the sliding end of the operating lever 110 is facing When a certain sensing area of the first chute slides, the operator applies a thrust to the operating lever 110 to squeeze the first telescopic portion 134 and the second telescopic portion 135, and the operating lever 110 The first telescopic portion 134 and the second telescopic portion 135 pass between and slide into the corresponding sensing regions. At this time, the limiting portion 133 limits the operating lever 110, and the operator can take the hand from the The joystick 110 is released, and since the joystick 110 is limited to the manipulation area by the limiting portion 133, the aircraft will maintain the current flight state until the operator puts the joystick 110 dials away from the current sensing area.
为了使所述操纵杆110能更轻松地将所述第一伸缩部134和所述第二伸缩部135推开，所述第一伸缩部134的两侧分别设置倒角，所述第二伸缩部135的两侧分别设置倒角，因此，所述第一伸缩部134和所述第二伸缩部135之间呈喇叭口状。In order to facilitate the pushing of the first telescopic portion 134 and the second telescopic portion 135 by the lever 110, the two sides of the first telescopic portion 134 are respectively chamfered, and the second telescopic The two sides of the portion 135 are respectively provided with chamfers. Therefore, the first expansion and contraction portion 134 and the second expansion and contraction portion 135 have a bell mouth shape.
本发明还提供一种遥控装置（未图示），包括壳体（未图示）和所述摇杆组件100，所述摇杆组件100设于所述壳体。由于所述遥控装置采用了本实施例的全部技术方案，因此至少具有上述实施例的技术方案所带来的所有有益效果，在此不再一一赘述。The present invention also provides a remote control device (not shown) including a housing (not shown) and the rocker assembly 100, the rocker assembly 100 being disposed in the housing. Since the remote control device adopts all the technical solutions of the embodiment, at least all the beneficial effects brought by the technical solutions of the foregoing embodiments are not repeatedly described herein.
本发明还提供一种飞行系统（未图示），包括飞行器（未图示）和所述遥控装置，所述遥控装置用于控制所述飞行器的飞行状态。由于所述飞行系统采用了本实施例的全部技术方案，因此至少具有上述实施例的技术方案所带来的所有有益效果，在此不再一一赘述。The present invention also provides a flight system (not shown) including an aircraft (not shown) and the remote control device for controlling the flight state of the aircraft. Since the flight system adopts all the technical solutions of the embodiment, at least all the beneficial effects brought by the technical solutions of the foregoing embodiments are not repeatedly described herein.
以上所述仅为本发明的优选实施例，并非因此限制本发明的专利范围，凡是在本发明的发明构思下，利用本发明说明书及附图内容所作的等效结构变换，或直接/间接运用在其他相关的技术领域均包括在本发明的专利保护范围内。The above description is only a preferred embodiment of the present invention, and is not intended to limit the scope of the invention, and the equivalent structural transformation, or direct/indirect use, of the present invention and the contents of the drawings are used in the inventive concept of the present invention. It is included in the scope of the patent protection of the present invention in other related technical fields.

Claims (20)

  1. 一种摇杆组件，其特征在于，包括传感器、控制器及一操纵杆；所述一操纵杆具有至少六种操纵状态，六种所述操纵状态分别用于控制飞行器的前进、后退、向左、向右、上升及下降动作；所述传感器用于获取所述操纵杆的操作状态；所述控制器与所述传感器电连接，所述控制器根据所述传感器获取的所述操纵杆的操作状态发出相应的控制信号至所述飞行器。 A rocker assembly, comprising: a sensor, a controller and a joystick; the joystick has at least six operating states, and the six operating states are respectively used to control the forward, backward, and leftward directions of the aircraft a rightward, rising and falling action; the sensor is configured to acquire an operating state of the joystick; the controller is electrically coupled to the sensor, and the controller operates according to the joystick acquired by the sensor The status issues a corresponding control signal to the aircraft.
  2. 如权利要求1所述的摇杆组件，其特征在于，所述摇杆组件还包括六个感应区，分别为向前感应区、向后感应区、向左感应区、向右感应区、上升感应区及下降感应区；所述操纵杆处于上述感应区时，分别用于控制所述飞行器的前进、后退、向左、向右、上升及下降动作。The rocker assembly according to claim 1, wherein the rocker assembly further comprises six sensing regions, which are a forward sensing region, a backward sensing region, a left sensing region, a right sensing region, and a rising The sensing area and the falling sensing area; when the joystick is in the sensing area, respectively, for controlling the forward, backward, leftward, rightward, rising and falling motions of the aircraft.
  3. 如权利要求2所述的摇杆组件，其特征在于，所述摇杆组件还包括底座；所述底座包括第一滑槽及第二滑槽；所述第一滑槽的中部与所述第二滑槽的中部相交，所述第二滑槽将所述第一滑槽分成所述向前感应区和所述向后感应区，所述第一滑槽将所述第二滑槽分成所述向左感应区和所述向右感应区。The rocker assembly according to claim 2, wherein the rocker assembly further comprises a base; the base comprises a first chute and a second chute; a middle portion of the first chute and the first The middle of the two chutes intersect, the second chute divides the first chute into the forward sensing zone and the backward sensing zone, and the first chute divides the second chute into The left sensing area and the right sensing area are described.
  4. 如权利要求3所述的摇杆组件，其特征在于，所述底座还包括第三滑槽，所述操纵杆还包括上下提升部及收容所述上下提升部的收容腔，所述收容腔为所述第三滑槽，所述第三滑槽内具有所述上升感应区及所述下降感应区，所述上下提升部于所述收容腔内伸缩，以实现所述飞行器的上升或下降。The rocker assembly according to claim 3, wherein the base further comprises a third sliding slot, the operating lever further comprising an upper and lower lifting portion and a receiving cavity for receiving the upper and lower lifting portions, wherein the receiving cavity is In the third sliding slot, the third sliding slot has the rising sensing area and the falling sensing area, and the upper and lower lifting parts are telescoped in the receiving cavity to achieve the ascending or descending of the aircraft.
  5. 如权利要求4所述的摇杆组件，其特征在于，所述第一滑槽、所述第二滑槽及所述第三滑槽两两垂直。The rocker assembly according to claim 4, wherein the first sliding slot, the second sliding slot and the third sliding slot are perpendicular to each other.
  6. 如权利要求1所述的摇杆组件，其特征在于，所述操纵杆包括设于其上的按压部，所述按压部包括上升按键和下降按键，所述上升按键用于控制所述飞行器进行上升动作，所述下降按键用于控制所述飞行器进行下降动作。A rocker assembly according to claim 1, wherein said lever includes a pressing portion provided thereon, said pressing portion includes a rising button and a falling button, said rising button for controlling said aircraft A rising action for controlling the aircraft to perform a lowering action.
  7. 如权利要求2所述的摇杆组件，其特征在于，所述操纵杆包括设于其上的按压部，所述按压部包括上升按键和下降按键，所述上升按键用于控制所述飞行器进行上升动作，所述下降按键用于控制所述飞行器进行下降动作。A rocker assembly according to claim 2, wherein said lever includes a pressing portion provided thereon, said pressing portion includes a rising button and a falling button, said rising button for controlling said aircraft A rising action for controlling the aircraft to perform a lowering action.
  8. 如权利要求3所述的摇杆组件，其特征在于，所述操纵杆包括设于其上的按压部，所述按压部包括上升按键和下降按键，所述上升按键用于控制所述飞行器进行上升动作，所述下降按键用于控制所述飞行器进行下降动作。A rocker assembly according to claim 3, wherein said lever includes a pressing portion provided thereon, said pressing portion includes a rising button and a falling button, said rising button for controlling said aircraft A rising action for controlling the aircraft to perform a lowering action.
  9. 如权利要求4所述的摇杆组件，其特征在于，所述操纵杆包括设于其上的按压部，所述按压部包括上升按键和下降按键，所述上升按键用于控制所述飞行器进行上升动作，所述下降按键用于控制所述飞行器进行下降动作。A rocker assembly according to claim 4, wherein said lever includes a pressing portion provided thereon, said pressing portion includes a rising button and a falling button, said rising button for controlling said aircraft A rising action for controlling the aircraft to perform a lowering action.
  10. 如权利要求5所述的摇杆组件，其特征在于，所述操纵杆包括设于其上的按压部，所述按压部包括上升按键和下降按键，所述上升按键用于控制所述飞行器进行上升动作，所述下降按键用于控制所述飞行器进行下降动作。A rocker assembly according to claim 5, wherein said lever includes a pressing portion provided thereon, said pressing portion includes a rising button and a falling button, said rising button for controlling said aircraft A rising action for controlling the aircraft to perform a lowering action.
  11. 如权利要求6所述的摇杆组件，其特征在于，所述按压部还包括加速按键和减速按键，所述加速按键用于控制所述飞行器加速飞行，所述减速按键用于控制所述飞行器减速飞行。 The rocker assembly according to claim 6, wherein the pressing portion further comprises an acceleration button for controlling the aircraft to accelerate flight, and a deceleration button for controlling the aircraft Slow down the flight.
  12. 如权利要求6所述的摇杆组件，其特征在于，所述操纵杆还包括杆状的主体部，所述主体部的侧壁形成凹陷区。A rocker assembly according to claim 6, wherein said lever further includes a rod-shaped body portion, and a side wall of said body portion forms a recessed portion.
  13. 一种遥控装置，其特征在于，包括壳体和如权利要求1所述的摇杆组件，所述摇杆组件设于所述壳体。A remote control device comprising a housing and the rocker assembly of claim 1, the rocker assembly being disposed on the housing.
  14. 一种遥控装置，其特征在于，包括壳体和如权利要求2所述的摇杆组件，所述摇杆组件设于所述壳体。A remote control device comprising a housing and the rocker assembly of claim 2, the rocker assembly being disposed in the housing.
  15. 一种遥控装置，其特征在于，包括壳体和如权利要求3所述的摇杆组件，所述摇杆组件设于所述壳体。A remote control device comprising a housing and the rocker assembly of claim 3, the rocker assembly being disposed in the housing.
  16. 一种遥控装置，其特征在于，包括壳体和如权利要求4所述的摇杆组件，所述摇杆组件设于所述壳体。A remote control device comprising a housing and the rocker assembly of claim 4, the rocker assembly being disposed in the housing.
  17. 一种遥控装置，其特征在于，包括壳体和如权利要求5所述的摇杆组件，所述摇杆组件设于所述壳体。A remote control device comprising a housing and the rocker assembly of claim 5, the rocker assembly being disposed in the housing.
  18. 一种遥控装置，其特征在于，包括壳体和如权利要求11所述的摇杆组件，所述摇杆组件设于所述壳体。A remote control device comprising a housing and a rocker assembly according to claim 11, the rocker assembly being disposed in the housing.
  19. 一种遥控装置，其特征在于，包括壳体和如权利要求12所述的摇杆组件，所述摇杆组件设于所述壳体。A remote control device comprising a housing and a rocker assembly according to claim 12, the rocker assembly being disposed in the housing.
  20. 一种飞行系统，其特征在于，包括飞行器和如权利要求13所述的遥控装置，所述遥控装置用于控制所述飞行器的飞行状态。An aircraft system is characterized by comprising an aircraft and a remote control device according to claim 13, said remote control device for controlling the flight state of said aircraft.
PCT/CN2016/107927 2016-06-17 2016-11-30 Rocker assembly, remote control device and flight system WO2017215199A1 (en)

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