CN204695614U - A kind of training guiding device of aircraft - Google Patents
A kind of training guiding device of aircraft Download PDFInfo
- Publication number
- CN204695614U CN204695614U CN201520363991.XU CN201520363991U CN204695614U CN 204695614 U CN204695614 U CN 204695614U CN 201520363991 U CN201520363991 U CN 201520363991U CN 204695614 U CN204695614 U CN 204695614U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- training
- user
- subelement
- guiding device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Electrically Operated Instructional Devices (AREA)
Abstract
The utility model discloses a kind of training guiding device and method of aircraft, belong to technical field of aerospace.Training guiding device comprises the bootstrap module guiding user operation aircraft to implement to specify flare maneuver, and bootstrap module comprises operating database, sensing unit and Tip element further, and wherein, operating database is applicable to the program storing operate aircraft; Sensing unit is applicable to the state responding to aircraft, produces feedback information; Tip element is according to the feedback information of sensing unit, and the corresponding operating in read operation database or action, send cue to user, and prompting user completes appointment flare maneuver.Arrange user by the utility model and instruct program, the functions such as the flare maneuver of assisting users study aircraft and application operating, greatly improve the operating experience of user, and can enjoy the enjoyment of beam riding device.
Description
Technical field
The utility model relates to aviation and automatic control technology field, is specifically related to a kind of training guiding device of aircraft.
Background technology
Unmanned plane Aerial photography, demonstration flight, take precautions against natural calamities recover, there is wide application in the field such as scientific investigation.Along with the develop rapidly of electronic technology, small-sized, Micro Aerial Vehicle has had obvious breakthrough in Remote, cruising time, flight quality, becomes the General Aviation field focus of rising in recent years, is generally considered and has good development prospect.
Current unmanned plane has started to enter consumer level market, especially multi-rotor aerocraft, typically, as four axle multi-rotor aerocrafts have become in consumer level market the preferred unit being used for implementing to take photo by plane.
What prior art was mainly paid close attention to is how Navigation of Pilotless Aircraft location is realized by various method, such as: application number is 201310059457.5, the Chinese invention patent application that denomination of invention is " a kind of unmanned plane dynamic target tracking of view-based access control model and localization method " discloses a kind of unmanned plane dynamic target tracking and localization method of view-based access control model, the present invention completes the detection to moving target, image trace, automatic deflection optical axis, dynamic object is made to be presented on imaging plane central authorities all the time, the distance between unmanned plane and dynamic object is measured in real time according to the model set up in the basis obtaining unmanned plane elevation information, thus the location realized dynamic object, in this, as feedback signal, form closed-loop control, guide the tracking flight of unmanned plane.
Because multi-rotor aerocraft is a kind of airflight equipment, handling to get up to acquire a certain degree of difficulty, aloft in flight course, just likely occurring airflight accident once break down.In prior art, the Chinese invention patent application that application number is 201410006690.1, denomination of invention is " system that the task for operational administrative in aircraft cockpit guides " discloses the system and computer-readable medium that the task for operational administrative in aircraft cockpit guides, comprising the system for providing task to guide and computer-readable medium, managing flight operation for during the abnormal conditions that cause at normal operating procedure or anomalous event.The system guided for providing task can comprise processor, storer and be configured to receive from multiple server the flight supplementary module of data.Supplementary module can show the possible aircraft flight stage while instruction mission phase.Supplementary module can also the show needle operation that will perform mission phase, and operates corresponding action with these.This invention, for convenience of crew's operation, that make standard is arranged into a center system with program that is exception and control device.
But above-mentioned patented claim does not all provide the technical scheme how helping user-friendly study multi-rotor aerocraft driving efficiency.And active user is for the use of multi-rotor aerocraft, only realize by instructions or operation interface, learning process is unfriendly, thus reduces the Consumer's Experience of multi-rotor aerocraft.Further, learn in this uncertain mode, all can bring great hidden danger to the safe flight, functional development etc. of multi-rotor aerocraft.User probably causes aircraft accident because being unfamiliar with the performance of multi-rotor aerocraft, also very possible because do not know that multi-rotor aerocraft can accomplish more flare maneuver, and loses the interest etc. to multi-rotor aerocraft.
Therefore, be necessary to arrange an incremental process, user is helped to complete the study handled multi-rotor aerocraft gradually in the mode of intelligently guiding, by well-designed boot, the manipulation skill of the grasp multi-rotor aerocraft that novice users can be allowed correct, also can allow novice users understand repertoire achieved by multi-rotor aerocraft.
Utility model content
Goal of the invention of the present utility model is to provide a kind of training guiding device of aircraft, for the problems referred to above, by designing the intelligently guiding program combined with aircraft, instruction user learns driving efficiency and the integrated application of aircraft, the manipulation of significant increase user is experienced, and can enjoy the enjoyment of beam riding device.
In order to solve the problems of the technologies described above, the technical solution adopted in the utility model is as follows:
A training guiding device for aircraft, described training guiding device comprises the bootstrap module guiding aircraft described in user operation to implement to specify flare maneuver, and described bootstrap module comprises operating database, sensing unit and Tip element further, wherein,
Described operating database is applicable to the program that storage operates described aircraft;
Described sensing unit is applicable to the state responding to described aircraft, produces feedback information;
Described Tip element, according to the feedback information of described sensing unit, reads the corresponding operating in described operating database or action, sends cue to user, and prompting user completes described appointment flare maneuver.
Specify flare maneuver to specify flare maneuver further, the program stored in described operating database comprises Basic Flight Maneuver guidance unit and/or take off self-inspection guidance unit and/or combination flare maneuver guidance unit and/or malfunction elimination guidance unit and/or integrated application guidance unit.
Further, described sensing unit comprises the flight steering order judgment sub-unit of GPS locator and/or altimeter and/or telepilot and/or gyroscope and/or acceleration transducer.
Further, described Tip element comprises subunits of speech and/or image subelement and/or word subelement, is applicable to send voice signal prompting and/or picture signal prompting and/or letter signal prompting respectively.
Further, also comprise User Information Database, it is applicable to therefrom identify the user profile of driving described aircraft and the airmanship information corresponding to this user.
Further, also comprise electronic control module, deviation between the flight path of its described appointment flare maneuver during being applicable to determine described aircraft flight and described aircraft current location, comprise positioning unit and processor unit, described electronic control module is electrically connected with described bootstrap module.
Further, described Basic Flight Maneuver guidance unit comprises Throttle Opening Control training subelement and/or front and back flight training subelement and/or left and right sides fly training subelement and/or mouth word flight training subelement.
Further, what the self-inspection guidance unit that takes off described in comprised flight state training subelement and/or aircraft and telepilot trains subelement to code.
Further, the prompting subelement of training subelement also to comprise to arrange the prompting subelement of horizontal alignment and/or telepilot pattern to arrange to code of described aircraft and telepilot.
Further, described combination flare maneuver guidance unit comprise spiraling training subelement and/or head before formula mouth word train subelement and/or pinpoint landing training and/or given line training subelement.
The utility model discloses a kind of training guiding device of aircraft, by well-designed intelligently guiding program, incremental guiding user completes the study to aircraft control, novice users can either be allowed correctly to grasp the driving skills of aircraft, also novice users can be allowed to understand repertoire achieved by aircraft, the manipulation greatly improving user is experienced, and enables user enjoy the enjoyment of beam riding device.
Above-mentioned explanation is only the general introduction of technical solutions of the utility model, clearly understand in order to technological means of the present utility model can be made, reach the degree that those skilled in the art can be implemented according to the content of instructions, and in order to above-mentioned and other objects, features and advantages of the present utility model can be allowed to become apparent, be illustrated with embodiment of the present utility model below.
Accompanying drawing explanation
By reading the detailed description in hereafter preferred embodiment, the utility model various other advantage and benefit will become cheer and bright for those of ordinary skill in the art.Figure of description only for illustrating the object of preferred implementation, and is not thought restriction of the present utility model.Apparently, accompanying drawing described below is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, can also obtain other accompanying drawing according to these accompanying drawings.And in whole accompanying drawing, represent identical parts by identical reference symbol.In the accompanying drawings:
Fig. 1 shows the training guiding arrangement structure block diagram of the aircraft according to the utility model embodiment one;
Fig. 2 shows the training guiding arrangement structure block diagram of the aircraft according to the utility model embodiment two;
Fig. 3 shows the training guiding arrangement structure block diagram of the aircraft according to the utility model embodiment three;
Fig. 4 shows the training guiding arrangement structure block diagram of the aircraft according to the utility model embodiment four;
Fig. 5 shows the training bootstrap technique process flow diagram of the aircraft according to the utility model embodiment five;
Fig. 6 shows the bootstrap technique process flow diagram that climbs of Throttle Opening Control training in the training guiding device of the aircraft according to the utility model embodiment one to five or method.
Embodiment
In more detail specific embodiment of the utility model is described below with reference to accompanying drawings.Although show specific embodiment of the utility model in accompanying drawing, however should be appreciated that can realize the utility model in a variety of manners and not should limit by the embodiment set forth here.On the contrary, provide these embodiments to be in order to more thoroughly the utility model can be understood, and complete for scope of the present utility model can be conveyed to those skilled in the art.
It should be noted that, in the middle of instructions and claim, employ some vocabulary to censure specific components.Those skilled in the art should be appreciated that hardware manufacturer may call same assembly with different noun.This specification and claims are not used as with the difference of noun the mode distinguishing assembly, but are used as the criterion of differentiation with assembly difference functionally." comprising " or " comprising " as mentioned in the middle of instructions and claim is in the whole text an open language, therefore should be construed to " comprise but be not limited to ".Instructions subsequent descriptions is for implementing better embodiment of the present utility model, and right described description is for the purpose of the rule of instructions, and is not used to limit scope of the present utility model.Protection domain of the present utility model is when being as the criterion depending on the claims person of defining.
For ease of the understanding to the utility model embodiment, be further explained explanation below in conjunction with accompanying drawing for several specific embodiment, and each accompanying drawing does not form the restriction to the utility model embodiment.
Unmanned spacecraft is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft utilizing radio robot to handle with the presetting apparatus provided for oneself.Can be divided into from technical standpoint definition: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc.
In the utility model embodiment, preferred unmanned plane is many rotor wing unmanned aerial vehicles (or being called multi-rotor aerocraft), can be four rotors, six rotors and rotor quantity is greater than six and is the unmanned plane of even number, described many rotor wing unmanned aerial vehicles comprise in rectangular fairshaped fuselage, fuselage is roughly rectangular structure, its corner and corner are flowing transition, to make air show as laminar flow when the surface of fuselage is flow through, thus reduce the resistance of many rotor wing unmanned aerial vehicles in flight course.Preferably, fuselage is made up of carbon fibre material, under the prerequisite meeting higher working strength and rigidity, significantly can alleviate the weight of fuselage, thus reduces the power demand of many rotor wing unmanned aerial vehicles and improve the maneuverability of many rotor wing unmanned aerial vehicles.Certainly, in other embodiments of the present utility model, fuselage can also be made up of plastics or other arbitrarily used materials.Fuselage is provided with multiple slurry arm be symmetric relative to the symmetrical plane in described fuselage, each slurry arm is provided with paddle components away from one end of described fuselage, described paddle components comprises the motor be arranged on described slurry arm and the blade be connected on the output shaft of described motor, and the rotation of every a slice blade is all positioned on the same face of cylinder.
Certainly, the explanation of described many rotor wing unmanned aerial vehicles is a simple declaration, specifically also comprises other composition components many, also also has other many kinds of unmanned plane types, all may be used for realizing the purpose of this utility model, do not repeat them here.
But, from the development trend of the manipulation convenience that demand and the user in consumer level market take for flight, the flight capture apparatus of technical solutions of the utility model mainly refers to little, miniature many rotor wing unmanned aerial vehicles, this unmanned plane volume is little, cost is low, flight stability is better, and flight shooting cost is low.The utility model use aircraft, typically with four axle multi-rotor aerocrafts for representative.Further, this aircraft started to be widely used in take photo by plane, the field such as aerial work, logistics.
The training guiding device of embodiment one, a kind of aircraft.
Fig. 1 is the training guiding arrangement structure block diagram of a kind of aircraft of the utility model embodiment one, and composition graphs 1 is specifically described by the utility model embodiment.
As shown in Figure 1, the utility model embodiment provides a kind of training guiding device 101 of aircraft 100, described training guiding device 101 comprises the bootstrap module 102 guiding aircraft described in user operation to implement to specify flare maneuver, described bootstrap module 102 comprises operating database 103, sensing unit 104 and Tip element 105 further, wherein
Described operating database 103 is applicable to the program that storage operates described aircraft 100;
Described sensing unit 104 is applicable to the state responding to described aircraft 100, produces feedback information; State described here comprises flight attitude and/or the flare maneuver of described aircraft 100, even can respond to that described aircraft 100 remains static at present, open state, takeoff condition etc.
Described Tip element 105, according to the feedback information of described sensing unit 104, reads the corresponding operating in described operating database 103 or action, sends cue to user, and prompting user completes described appointment flare maneuver.
In the technical program, core content is to guide user to learn the functional module of beam riding device by gradual and orderly approach.
Preferred in the utility model embodiment, described training guiding device 101 can integrated design in described aircraft 100, also can be an independent physical unit, can also be integrated in the central control system of ground, the particular location that described training guiding device 101 is arranged is unimportant, as long as have this functional module.
Preferred in the utility model embodiment, described sensing unit 104 comprises the flight steering order judgment sub-unit of GPS locator and/or altimeter and/or telepilot and/or gyroscope and/or acceleration transducer.Certainly, described sensing unit 104 can also comprise the sensor of other type for confirming flight attitude or the state of flight of described aircraft 100.How to determine the flight attitude of aircraft 100, flare maneuver, current status, user operation sensing unit have a lot of mode in the prior art, do not repeat them here.
In another embodiment of the utility model, described sensing unit 104 also can adopt user manually to select the induction mode triggered, and such as, the selection of active user's point touching screen is taken off self-inspection guidance unit.
In an alternative embodiment of the invention, the working method of described Tip element 105 is initiatively promptings, send pilot signal, now sensing unit 104 described here or automatically can run to a certain state and detects the operation on a certain device on described aircraft 100, such as, after likely described aircraft 100 1 is started shooting, described sensing unit 104 detects described boot action, then first provide an information, then described sensing unit 104 carries out further information acquisition, carries out next step indication according to the information of described sensing unit 104 collection.
Preferred in the utility model embodiment, the implementation of described bootstrap module 102 is: described aircraft 100 is according to pre-set programs, sound/light/image/letter signal is sent to user, prompting user completes guiding action, by described sensing unit 104, described aircraft 100 senses that user completes guiding action (this induction mode substantially, both can according to GPS positioning signal, altimeter signal etc., also can according to the judgement of the flight steering order from telepilot, these two kinds of modes can also be fully utilized and obtain judged result more accurately), then provide prompting, and according to the preset strategy of described bootstrap module 102, carry out the next prompting guiding action.
Preferred in the utility model embodiment, described Tip element comprises subunits of speech and/or image subelement and/or word subelement, is applicable to send voice signal prompting and/or picture signal prompting and/or letter signal prompting respectively.The concrete mode guided, comprise and carry out the mode of reminding with the voice signal pre-stored, also can be the image pre-stored, letter signal are presented at the mode on user's controller at one's side or other-end, can also be any mode effectively can passing on guidance information or signal.
The training guiding device of embodiment two, a kind of aircraft.
Fig. 2 is the training guiding arrangement structure block diagram of a kind of aircraft of the utility model embodiment two, and composition graphs 2 is specifically described by the utility model embodiment.
As shown in Figure 2, the utility model embodiment provides a kind of training guiding device 101 of aircraft 100, described training guiding device 101 comprises the bootstrap module 102 guiding aircraft appointment flare maneuver described in user operation, described bootstrap module 102 comprises operating database 103 further, sensing unit 104 and Tip element 105, wherein, described operating database 103 comprises Basic Flight Maneuver guidance unit 201 and/or take off self-inspection guidance unit 202 and/or combination flare maneuver guidance unit 203 and/or malfunction elimination guidance unit 204 and/or integrated application guidance unit 205.
Preferred in the utility model embodiment, described Basic Flight Maneuver guidance unit 201 comprises Throttle Opening Control training subelement and/or front and back flight training subelement and/or left and right sides and flies training subelement and/or mouth word flight training subelement.
Concrete, be described for described Throttle Opening Control training subelement:
Throttle is controlled by aircraft 100 about heading, climbing and the decline of aircraft 100 of guiding user learning aircraft 100 with left hand.
The guiding of climbing of aircraft 100, its main points are: provide power by throttle with fast speed, when ensureing that aircraft 100 reaches high height in visual range, slightly fall some throttles, suitably complete hovering;
The landing of aircraft 100 guides, and its main points are: do not allow rapidly aircraft 100 stall, allows aircraft 100 slowly fall earthward;
Repeat the process three times of the climbing-hover of aircraft 100-land;
The lifting of aircraft 100 combines and guides, and its main points are: allow aircraft 100 can rise to rapidly high height in visual range by training above, slowly stably can be down to ground again.
The hovering of aircraft 100 guides, and its main points are: allow aircraft 100 in visual range a period of time its highly remain unchanged, when height change occurs aircraft 100, in time according to situation of change, suitably increase and decrease throttle.
Again such as, be described for described front and back flight training subelement:
Flight before and after aircraft 100 is controlled with the right hand, after aircraft 100 is remained on certain altitude by left hand, flight before and after training.
Fly before aircraft 100 to guide, its main points are: with ground mark for object of reference, control aircraft 100 flight forward unit length;
Fly after aircraft 100 to guide, its main points are: with ground mark for object of reference, control aircraft 100 and to fly backward a unit length;
The front and back flight of repeating aircraft 100 guides, and its main points are: control aircraft 100 and to advance a long measure, hovering, then control an aircraft 100 slow astern long measure again, repeat three times.
Fly training subelement for left and right sides to be described:
Control aircraft 100 left and right sides with the right hand to fly, aircraft 100 is remained on certain altitude by left hand, and training left and right sides flies.Mode and the flight training of above-mentioned front and back similar.
Be described for mouth word flight training subelement:
By mouth word formula flight training subelement, the flare maneuver that combined training is above-mentioned:
Left hand controls aircraft 100 and aloft hovers, and remains on the safe altitude of liftoff 30 cm;
The right hand controls aircraft 100 and has decomposed the action several times that clockwise mouth word flies aloft, specific as follows: frontly to fly a long measure, flies a long measure in right side, after fly a long measure, fly a long measure in left side;
The right hand controls aircraft 100 and has decomposed the action several times that counterclockwise mouth word flies aloft, specific as follows: frontly to fly a long measure, flies a long measure in left side, after fly a long measure, fly a long measure in right side.
Preferred in the utility model embodiment, described in take off that self-inspection guidance unit 202 comprises flight state training subelement and/or aircraft and telepilot subelement is trained to code.
Be described for described flight state training subelement:
Aircraft 100 sends information, user please confirm that whether the state warning lamp of aircraft 100 is all working properly, such as: whether power light is evergreen, and (evergreen expression electric power is sufficient, flicker represents that voltage is lower than 50%, red expression voltage can not take off lower than 10%), whether malfunction indicator lamp is extinguished, and whether fore-and-aft direction pilot lamp is lighted.
Subelement is trained to be described for described aircraft and telepilot to code:
Aircraft 100 is pointed out current to code state, judges whether to complete code;
When aircraft 100 prompting has the telepilot do not completed code, provide code information, user is such as pointed out aircraft 100 to be placed on the departure location of level, on prompting user operation telepilot to code function key, and provide to coded signal (such as, can be throttle is shifted onto rapidly maximum, then push back rapidly minimum command signal and be used as code cue).
Preferred in the utility model embodiment, for maiden flight aircraft 100 described in the prompting subelement of training subelement also to comprise to arrange the prompting subelement of horizontal alignment and/or telepilot pattern to arrange to code of aircraft and telepilot.
Concrete, the described prompting subelement arranging level more accurate can be:
Reminding user is by static for aircraft 100 position being placed on level;
Reminding user remote control two operating rods get to special angle, the such as lower left corner simultaneously;
Reminding user unclamps operating rod when the fore-and-aft direction lamp of aircraft 100 glimmers simultaneously;
Reminding user confirms whether aircraft 100 gives the signal of fore-and-aft direction lamp Chang Liang to represent that calibration completes.
Adopt and remind in this way, complicated horizontal alignment can be allowed for user, resolved into instruction clear and easy to understand step by step, reduced the study understanding cost of user.
Concrete, the prompting subelement that described telepilot pattern is arranged refers to:
Telepilot first time is to after code, default setting is 4 channel patterns, now sends information to user, informs user: the left side operating rod above-below direction of telepilot is throttle, control rising and the decline of aircraft 100, left side operating rod left and right directions controls to rotate; Right-hand joystick above-below direction is the forward-reverse controlling aircraft 100, and left and right directions is the left and right sides direction flight controlling aircraft 100.
According to the difference of telepilot, may also have other auxiliary key mappings, now aircraft 100 also sends information to user successively, such as: the fine setting of four direction is good for, the function of LR key mapping, the function (pointing out long by one second switch mode) of 3 channel patterns and 4 channel pattern switch keys.
For another example, speed key and rolling key may be also had: described speed key with gear to divide speed step (the different speed step of prompting user what situation corresponding); Described rolling key need coordinate with right operating rod, after described rolling key function setting is good, realizes rolling to respective direction with right operating rod.
Preferred in the utility model embodiment, before described combination flare maneuver guidance unit 203 comprises spiraling training subelement and/or head, formula mouth word train subelement and/or pinpoint landing train subelement and/or given line training subelement.
Specifically, described spiraling training subelement comprises:
Spiraling is controlled for left and right, while aircraft 100 is remained on certain altitude by left hand, training spiraling.
Mode and the flight training of above-mentioned front and back similar, comprise a left side and turn 90 degrees, reduction, repeat consolidation; The right side turn 90 degrees, and reduction, repeats consolidation.
Concrete, before described head, formula mouth word train subelement comprises:
Keep the head orientation movements direction all the time of aircraft 100, fly before utilization work and spinning movement, complete flight mouth word clockwise successively, counterclockwise the training of flight mouth word.Concrete training patterns and aforementioned schemes similar, repeat no more.
Concrete, described pinpoint landing training subelement comprises:
On map, provide a landing place at random by aircraft, in requiring that user at the appointed time, complete the task of standing start and pinpoint landing, training several times.
Concrete, described given line training subelement comprises:
On map, provide a given line at random by aircraft, be wherein set with some anchor points, user needs at the appointed time, completes the aerial mission of given line, and completes hovering verification at each anchor point, training several times.
Other content of the utility model embodiment, with reference to above-mentioned utility model embodiment one, does not repeat them here.
The training guiding device of embodiment three, a kind of aircraft.
Fig. 3 is the training guiding arrangement structure block diagram of a kind of aircraft of the utility model embodiment three, and composition graphs 3 is specifically described by the utility model embodiment.
As shown in Figure 3, the utility model embodiment provides a kind of training guiding device 101 of aircraft 100, described training guiding device 101 comprises the bootstrap module 102 guiding aircraft appointment flare maneuver described in user operation, and described bootstrap module 102 comprises operating database 103, sensing unit 104 and Tip element 105 further.Described training guiding device 101 also comprises User Information Database 301, and it is applicable to therefrom identify the user profile of driving described aircraft and the airmanship information corresponding to this user.
Preferred in the utility model embodiment, first described training guiding device 101 identifies the user of the described aircraft 100 of current driving, can be identify from the specific ID information sent, also can be identify from the biological information comprising fingerprint, recognition of face etc., the airmanship information of respective user is read afterwards from described User Information Database 301, and according to described airmanship information, provide corresponding operation indicating.Airmanship information described here, can be the personal considerations of this user of manual entry, such as height and weight age health status, also can be the operation note before this user gathered from described bootstrap module 102, according to operation note before, judge the driving ability that this user is residing at present, select the boot being applicable to this user.Such as, if this user's airmanship is poor, can from most basic boot, if this user's airmanship is very outstanding, then can directly from the boot that grade of difficulty is high, like this can the driving experience of adding users.
In the utility model embodiment, other content is with reference to above-described embodiment one and embodiment two, does not repeat them here.
The training guiding device of embodiment four, a kind of aircraft.
Fig. 4 is the training guiding arrangement structure block diagram of a kind of aircraft of the utility model embodiment four, and composition graphs 4 is specifically described by the utility model embodiment.
As shown in Figure 4, the utility model embodiment provides a kind of training guiding device 101 of aircraft 100, described training guiding device 101 comprises the bootstrap module 102 guiding aircraft described in user operation to implement to specify flare maneuver, and described bootstrap module 102 comprises operating database 103, sensing unit 104 and Tip element 105 further.Described training guiding device 101 also comprises electronic control module 401, deviation during it is applicable to determine the flight of described aircraft 100 between the flight path of described appointment flare maneuver and described aircraft 100 current location, comprise positioning unit and processor unit, described electronic control module is electrically connected with described bootstrap module.Here positioning unit can adopt GPS location technology, also can adopt Beidou navigation technology, or the technology being applicable to aerial vehicle trajectory location ripe arbitrarily.Described electronic control module is by being electrically connected with described bootstrap module, the flight path of described appointment flare maneuver during obtaining described aircraft flight, the locating information of this flight path information and described positioning unit is inputted then described processor unit, through the process of described processor unit, deviation during obtaining described aircraft flight between the flight path of described appointment flare maneuver and described aircraft current location, the deviation information of acquisition is inputted described bootstrap module 102, to the indication that active user is correct.
Preferred in the utility model embodiment, the current location information of described aircraft 100 can be obtained by described sensing unit 104, also can be obtained by above-mentioned positioning unit.During described aircraft 100 flies, the flight path of described appointment flare maneuver can obtain from described operating database 103.When described electronic control module 401 obtains deviation information by algorithm, then provide feedback information according to described deviation information to described bootstrap module 102, corresponding information is provided to user, such as, in described front and back flight training process, described Tip element 105 points out user with ground mark for object of reference, control described aircraft 100 flight forward unit length, because user operation is unskilled, flight forward half unit length or exceeded a unit length, at this moment described electronic control module 401 will feed back the deviation information of " flight forward also poor half unit length or exceeded a unit length " to described bootstrap module 102, described Tip element 105 now can point out user " you need continue flight forward half unit length or you exceeded a unit length! ".
In the utility model embodiment, other content is with reference to above-described embodiment one to embodiment three, does not repeat them here.
The training bootstrap technique of embodiment five, a kind of aircraft.
Fig. 5 is the training bootstrap technique process flow diagram of the aircraft according to the utility model embodiment five, and composition graphs 5 is specifically described by the utility model embodiment.
As shown in Figure 5, a kind of training bootstrap technique of aircraft, comprises the following steps:
Step S501: the relevant procedures storing the described aircraft of operation;
Step S502: respond to the current residing status information of described aircraft;
Step S503: according to described induction information, reads corresponding operating or the action of described storage, sends cue to user, and prompting user completes appointment flare maneuver.
Preferred in the utility model embodiment, the described relevant procedures storing the described aircraft of operation comprise and store Basic Flight Maneuver boot and/or take off self-inspection boot and/or combination flare maneuver boot and/or malfunction elimination boot and/or integrated application boot.
Preferred in the utility model embodiment, the flight steering order that described induction mode comprises GPS positioning signal and/or altimeter signal and/or telepilot judges signal and/or sensor sensing signal.
Preferred in the utility model embodiment, described prompting mode comprises voice signal prompting and/or picture signal prompting and/or letter signal and points out.
Preferred in the utility model embodiment, also comprise the user profile identifying and drive described aircraft and the airmanship information corresponding to this user, according to the airmanship information of this user, provide corresponding operation guide.
Preferred in the utility model embodiment, also comprise the deviation between the flight path of described appointment flare maneuver during determining described aircraft flight and described aircraft current location, provide corresponding information according to described deviation information.
Preferred in the utility model embodiment, described Basic Flight Maneuver boot comprises Throttle Opening Control training and/or front and back flight training and/or left and right sides and flies training and/or the flight training of mouth word.
Preferred in the utility model embodiment, described in self-inspection boot of taking off comprise flight state training and/or aircraft and telepilot code is trained.
Preferred in the utility model embodiment, described combination flare maneuver boot to comprise before spiraling training and/or head formula mouth word train and/or pinpoint landing training and/or given line training.
Training bootstrap technique basic design principle in the utility model embodiment designs with guidance mode in introductory content design.Wherein, introductory content adopts incremental design, guides user to learn to handle aircraft; Guidance mode be then the prompting of employing information, etc. to be operated, results verification, flow process judge, the recycle design of next information prompting realizes.
In the utility model embodiment, other content is with reference to above-mentioned utility model embodiment one to four, does not repeat them here.
The bootstrap technique process flow diagram that climbs of Throttle Opening Control training in the training guiding device that Fig. 6 is the aircraft according to the utility model embodiment one to five or method, is specifically described composition graphs 6.
As shown in Figure 6, the bootstrap technique that climbs described in comprises the following steps:
Step S601: prompting user selects introductory content;
Step S602: prompting user starts Throttle Opening Control training;
Step S603: prompting user carries out ramp-up period training;
Step S604: wait for the instruction of climbing that user sends;
Step S605: judge whether to receive instruction; If receive the instruction of climbing of user, then enter next step; Otherwise, jump to step S611;
Step S606: judge that whether the instruction of climbing of user is correct; If instruction is correct, then enter next step; Otherwise, jump to step S612;
Step S607: judge whether the instruction of climbing of user exceeds restriction of climbing; If do not exceed restriction of climbing, then enter next step; Otherwise, jump to step S613;
Step S608: the instruction of climbing performing user;
Step S609: judge whether to achieve the goal; If achieved the goal, then enter next step; Otherwise, jump back to step S603 and continue to point out user to climb;
Step S610: terminate to climb training.
Step S611: judge that whether the stand-by period is overtime; If there is no time-out, then jump back to step S604 and continue to wait for that user climbs instruction; If overtime, then jump to step S610 and terminate training of climbing.
Step S612: prompting user current instruction errors of climbing, and jump back to step S603 and continue prompting user and carry out training of climbing.
Step S613: prompting user exceed restriction of climbing, provide restricted information, and jump back to step S603 continue point out user carry out training of climbing.
In several embodiment provided by the utility model, should be understood that, disclosed apparatus and method, can realize by another way.Such as, device embodiment described above is only schematic, such as, the division of described module or unit, be only a kind of logic function to divide, actual can have other dividing mode when realizing, such as multiple unit or assembly can in conjunction with or another system can be integrated into, or some features can be ignored, or do not perform.Another point, shown or discussed coupling each other or direct-coupling or communication connection can be by some interfaces, and the indirect coupling of device or unit or communication connection can be electrical, machinery or other form.
The described module that illustrates as separating component or unit or can may not be and physically separate, parts as unit display can be or may not be physical location, namely can be positioned at a place, or also can be distributed in multiple network element.Some or all of unit wherein can be selected according to the actual needs to realize the object of the present embodiment scheme.
In addition, each functional unit in each embodiment of the utility model can be integrated in a processing unit, also can be that the independent physics of unit exists, also can two or more unit in a unit integrated.Above-mentioned integrated unit both can adopt the form of hardware to realize, and the form of SFU software functional unit also can be adopted to realize.
If described integrated unit using the form of SFU software functional unit realize and as independently production marketing or use time, can be stored in a computer read/write memory medium.Based on such understanding, the part that the technical solution of the utility model contributes to prior art in essence in other words or all or part of of this technical scheme can embody with the form of software product, this computer software product is stored in a storage medium, comprising some instructions in order to make a computer equipment (can be personal computer, server, or the network equipment etc.) or processor (processor) perform all or part of step of method described in each embodiment of the utility model.And aforesaid storage medium comprises: USB flash disk, portable hard drive, ROM (read-only memory) (ROM, Read-OnlyMemory), random access memory (RAM, RandomAccessMemory), magnetic disc or CD etc. various can be program code stored medium.
The utility model can bring these useful technique effects: the training guiding device of aircraft disclosed in the utility model embodiment and method, by designing intelligentized boot, user is guided to learn to handle aircraft in incremental mode, prestore the relevant procedures of operate aircraft, state residing for current according to aircraft and the airmanship of user, cue is sent to user, prompting user completes appointment flare maneuver, be convenient to the driving efficiency that user grasps aircraft fast, reduce the learning cost of user, add the security in learning process, the manipulation greatly improving user is experienced.
One of ordinary skill in the art will appreciate that: accompanying drawing is the schematic diagram of an embodiment, the module in accompanying drawing or flow process might not be that enforcement the utility model is necessary.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model instructions and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Obviously, those skilled in the art can carry out various change and modification to the utility model and not depart from spirit and scope of the present utility model.Like this, if these amendments of the present utility model and modification belong within the scope of the utility model claim and equivalent technologies thereof, then the utility model is also intended to comprise these change and modification.
Claims (10)
1. the training guiding device of an aircraft, it is characterized in that: described training guiding device comprises the bootstrap module guiding aircraft described in user operation to implement to specify flare maneuver, described bootstrap module comprises operating database, sensing unit and Tip element further, wherein
Described operating database is applicable to the program that storage operates described aircraft;
Described sensing unit is applicable to the state responding to described aircraft, produces feedback information;
Described Tip element, according to the feedback information of described sensing unit, reads the corresponding operating in described operating database or action, sends cue to user, and prompting user completes described appointment flare maneuver.
2. the training guiding device of aircraft according to claim 1, is characterized in that: the program stored in described operating database comprises Basic Flight Maneuver guidance unit and/or take off self-inspection guidance unit and/or combination flare maneuver guidance unit and/or malfunction elimination guidance unit and/or integrated application guidance unit.
3. the training guiding device of aircraft according to claim 1 and 2, is characterized in that: described sensing unit comprises the flight steering order judgment sub-unit of GPS locator and/or altimeter and/or telepilot and/or gyroscope and/or acceleration transducer.
4. the training guiding device of aircraft according to claim 1, it is characterized in that: described Tip element comprises subunits of speech and/or image subelement and/or word subelement, be applicable to send voice signal prompting and/or picture signal prompting and/or letter signal prompting respectively.
5. the training guiding device of aircraft according to claim 1, is characterized in that: also comprise User Information Database, and it is applicable to therefrom identify the user profile of driving described aircraft and the airmanship information corresponding to this user.
6. the training guiding device of aircraft according to claim 1 or 5, it is characterized in that: also comprise electronic control module, deviation between the flight path of its described appointment flare maneuver during being applicable to determine described aircraft flight and described aircraft current location, comprise positioning unit and processor unit, described electronic control module is electrically connected with described bootstrap module.
7. the training guiding device of aircraft according to claim 2, is characterized in that: described Basic Flight Maneuver guidance unit comprises Throttle Opening Control training subelement and/or front and back flight training subelement and/or left and right sides and flies training subelement and/or mouth word flight training subelement.
8. the training guiding device of aircraft according to claim 2, is characterized in that: described in take off that self-inspection guidance unit comprises flight state training subelement and/or aircraft and telepilot subelement is trained to code.
9. the training guiding device of aircraft according to claim 8, is characterized in that: the prompting subelement of training subelement also to comprise to arrange the prompting subelement of horizontal alignment and/or telepilot pattern to arrange to code of described aircraft and telepilot.
10. the training guiding device of aircraft according to claim 2, is characterized in that: described combination flare maneuver guidance unit comprise spiraling training subelement and/or head before formula mouth word train subelement and/or pinpoint landing training and/or given line training subelement.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520363991.XU CN204695614U (en) | 2015-05-29 | 2015-05-29 | A kind of training guiding device of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520363991.XU CN204695614U (en) | 2015-05-29 | 2015-05-29 | A kind of training guiding device of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204695614U true CN204695614U (en) | 2015-10-07 |
Family
ID=54235878
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520363991.XU Active CN204695614U (en) | 2015-05-29 | 2015-05-29 | A kind of training guiding device of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204695614U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109788140A (en) * | 2019-03-12 | 2019-05-21 | Oppo广东移动通信有限公司 | Reduce method, apparatus, mobile terminal and the storage medium of power consumption |
| CN110969724A (en) * | 2019-12-23 | 2020-04-07 | 拓攻（南京）机器人有限公司 | Method, device and equipment for analyzing flight performance of unmanned aerial vehicle and storage medium |
| WO2021056436A1 (en) * | 2019-09-27 | 2021-04-01 | 深圳市大疆创新科技有限公司 | Aircraft control method, control terminal, and computer-readable storage medium |
-
2015
- 2015-05-29 CN CN201520363991.XU patent/CN204695614U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109788140A (en) * | 2019-03-12 | 2019-05-21 | Oppo广东移动通信有限公司 | Reduce method, apparatus, mobile terminal and the storage medium of power consumption |
| WO2021056436A1 (en) * | 2019-09-27 | 2021-04-01 | 深圳市大疆创新科技有限公司 | Aircraft control method, control terminal, and computer-readable storage medium |
| CN110969724A (en) * | 2019-12-23 | 2020-04-07 | 拓攻（南京）机器人有限公司 | Method, device and equipment for analyzing flight performance of unmanned aerial vehicle and storage medium |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104867371A (en) | Aircraft training guiding device and method | |
| Bouabdallah | Design and control of quadrotors with application to autonomous flying | |
| US9383756B2 (en) | Automatic flight control method for a rotorcraft enabling the rotorcraft to maintain a path by tracking manual flight controls | |
| US20150212391A1 (en) | Flying camera with string assembly for localization and interaction | |
| KR20130081260A (en) | Apparatus for controlling unmanned vehicle and unmanned vehicle having the said apparatus | |
| CN105917283A (en) | Ground vehicle-link control for remote control aircraft | |
| CN204695614U (en) | A kind of training guiding device of aircraft | |
| US9696724B1 (en) | Takeoff automating system, device, and method | |
| CN105404308A (en) | Flight control unit for parafoil type unmanned plane | |
| CN104820428A (en) | Memory type track reproduction method of unmanned aerial vehicle and device | |
| US7616130B2 (en) | Method and a device for processing and displaying aircraft piloting information | |
| CN106354151B (en) | Control method and control device of unmanned aerial vehicle | |
| RU2514293C2 (en) | Method of pilotage promotion, pilotage aid and aircraft | |
| US11681301B2 (en) | System for a guidance interface for a vertical take-off and landing aircraft | |
| Prior | Optimizing small multi-rotor unmanned aircraft: A practical design guide | |
| US20240012432A1 (en) | Systems and methods for controlling a flight boundary of an aircraft | |
| WO2006076647A2 (en) | Autorotation flight control system | |
| US20230350199A1 (en) | Systems and methods for a heads-up display for an electric aircraft | |
| CN106774396A (en) | A kind of many rotor ultrasonic wave automatic obstacle-avoiding unmanned planes | |
| CN114115303A (en) | Aircraft control method and device, and storage medium | |
| Grobler | Automated recharging and vision-based improved localisation for a quadrotor UAV | |
| Ng et al. | Flight Systems and Control | |
| US10528063B2 (en) | Natural language mission planning and interface | |
| Hockley et al. | Development of a monocopter for exploration of GPS-denied indoor environments | |
| Lowe et al. | Applications of head-up displays in commercial transport aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160913 Address after: 100020 Beijing City West Road No. 12 Chaoyang District Building No. 2 (national advertising Industrial Park incubator 25978) Patentee after: High domain (Beijing) Intelligent Technology Research Institute Co., Ltd. Address before: 200032 Dongan Road, Xuhui District, Lane 149, building No. 8, No., No. 1201 Patentee before: Yang Shanshan |