CN104867371A - Aircraft training guiding device and method - Google Patents
Aircraft training guiding device and method Download PDFInfo
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- CN104867371A CN104867371A CN201510290670.6A CN201510290670A CN104867371A CN 104867371 A CN104867371 A CN 104867371A CN 201510290670 A CN201510290670 A CN 201510290670A CN 104867371 A CN104867371 A CN 104867371A
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
Abstract
The invention discloses an aircraft training guiding device and a method, which belongs to the technical field of aviation. The training guiding device comprises a guiding module for guiding a user to operate on the aircraft to implement a specified flight action. The guiding module further comprises an operation database, a sensing unit and a prompting unit, wherein the operation database is used for storing programs for operating on the aircrafts; the sensing unit is used for sensing the state of the aircraft and generating feedback information; and the prompting unit is used for reading corresponding operation or action in the operation database according to the feedback information of the sensing unit and sending a prompting signal to the user to prompt the user to complete the specified flight action. Through setting the user teaching programs, the user is assisted to learn the flight actions and application operation of the aircraft, operation experience of the user is greatly enhanced, and fun of driving the aircraft can be enjoyed.
Description
Technical field
The present invention relates to aviation and automatic control technology field, be specifically related to a kind of training guiding device and method 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.
Summary of the invention
Goal of the invention of the present invention is to provide a kind of training guiding device and method 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 used in the present invention is as follows:
A kind of training guiding device of aircraft, described training guiding device comprises the bootstrap module guiding aircraft described in user operation to implement to specify flare maneuver appointment 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.
According to another aspect of the present invention, provide a kind of training bootstrap technique of aircraft, comprise the following steps:
Store the program of the described aircraft of operation;
Respond to the state residing for described aircraft, produce feedback information;
According to described induction information, read corresponding operating or the action of described storage, send cue to user, prompting user completes appointment flare maneuver.
Further, the described program storing the described aircraft of operation comprises and stores 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.
Further, 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.
Further, described prompting mode comprise voice signal prompting and/or picture signal prompting and/or letter signal prompting.
Further, 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.
Further, 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.
Further, described Basic Flight Maneuver boot comprises Throttle Opening Control training and/or front and back flight training and/or left and right sides fly training and/or the flight training of mouth word.
Further, self-inspection boot of taking off described in comprises training code of flight state training and/or aircraft and telepilot.
Further, 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.The invention discloses a kind of training guiding device and method 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 solution of the present invention, clearly understand in order to technological means of the present invention 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 and other objects of the present invention, feature and advantage can be allowed to become apparent, be illustrated with the specific embodiment of the present invention below.
Accompanying drawing explanation
By reading the detailed description in hereafter preferred embodiment, the present invention 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 does not think limitation of the present invention.Apparently, accompanying drawing described below is only some embodiments of the present invention, 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 embodiment of the present invention one;
Fig. 2 shows the training guiding arrangement structure block diagram of the aircraft according to the embodiment of the present invention two;
Fig. 3 shows the training guiding arrangement structure block diagram of the aircraft according to the embodiment of the present invention three;
Fig. 4 shows the training guiding arrangement structure block diagram of the aircraft according to the embodiment of the present invention four;
Fig. 5 shows the training bootstrap technique process flow diagram of the aircraft according to the embodiment of the present invention 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 embodiment of the present invention one to five or method.
Embodiment
In more detail specific embodiments of the invention are described below with reference to accompanying drawings.Although show specific embodiments of the invention in accompanying drawing, however should be appreciated that can realize the present invention 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 present invention can be understood, and complete for scope of the present invention 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 invention, and right described description is for the purpose of the rule of instructions, and is not used to limit scope of the present invention.Protection scope of the present invention is when being as the criterion depending on the claims person of defining.
For ease of the understanding to the embodiment of the present invention, 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 embodiment of the present invention.
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 embodiment of the present invention, 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 invention, 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 object of the present invention, 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 solution of the present invention 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 present invention 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 the aircraft of the embodiment of the present invention one, and composition graphs 1 is specifically described by the embodiment of the present invention.
As shown in Figure 1, embodiments provide 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 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 embodiment of the present invention, 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 embodiment of the present invention, the flight steering order that the induction mode of described sensing unit 104 comprises GPS positioning signal and/or altimeter signal and/or telepilot judges signal and/or sensor sensing signal.Sensor described here comprises gyroscope, acceleration transducer etc.
In an alternative embodiment of the invention, 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 gathers the information of described aircraft 100 further, carries out next step indication according to gathered information.
Preferred in the embodiment of the present invention, 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 embodiment of the present invention, described Tip element comprises voice signal prompting and/or picture signal prompting and/or letter signal and points out.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 embodiment of the present invention two, and composition graphs 2 is specifically described by the embodiment of the present invention.
As shown in Figure 2, embodiments provide 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 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 embodiment of the present invention, 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 to be trained for example with 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 the flight training of mouth word formula, 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 embodiment of the present invention, 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 embodiment of the present invention, 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 embodiment of the present invention, 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 embodiment of the present invention, with reference to foregoing invention 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 embodiment of the present invention three, and composition graphs 3 is specifically described by the embodiment of the present invention.
As shown in Figure 3, embodiments provide 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 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 embodiment of the present invention, 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 embodiment of the present invention, 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 embodiment of the present invention four, and composition graphs 4 is specifically described by the embodiment of the present invention.
As shown in Figure 4, embodiments provide 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 operating database, comprise positioning unit and processor unit, described electronic control module is electrically connected with described operating database.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 operating database, 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 Tip element, to the indication that active user is correct.
Preferred in the embodiment of the present invention, the current location information of described aircraft 100 can be obtained by described sensing unit 104, also can be obtained by other control processor.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 embodiment of the present invention, 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 embodiment of the present invention five, and composition graphs 5 is specifically described by the embodiment of the present invention.
As shown in Figure 5, a kind of training bootstrap technique of aircraft, comprises the following steps:
Step S501: the program storing the described aircraft of operation;
Step S502: respond to the current residing status information of described aircraft;
Step S503: according to described status information, reads the corresponding operating of described storage, sends cue to user, and prompting user completes appointment flare maneuver.
Preferred in the embodiment of the present invention, the described program storing the described aircraft of operation comprises and stores 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 embodiment of the present invention, 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 embodiment of the present invention, described prompting mode comprises voice signal prompting and/or picture signal prompting and/or letter signal and points out.
Preferred in the embodiment of the present invention, 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 embodiment of the present invention, 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 embodiment of the present invention, 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 embodiment of the present invention, described in self-inspection boot of taking off comprise flight state training and/or aircraft and telepilot code is trained.
Preferred in the embodiment of the present invention, 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 embodiment of the present invention 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 embodiment of the present invention, other content is with reference to foregoing invention 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 embodiment of the present invention 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 present invention, 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 present invention 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 technical scheme of the present invention 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 present invention.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 present invention can bring these useful technique effects: the training guiding device of aircraft disclosed in the embodiment of the present invention and method, by designing intelligentized boot, user is guided to learn to handle aircraft in incremental mode, prestore the program 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 present invention is necessary.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize instructions of the present invention 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 invention.
Obviously, those skilled in the art can carry out various change and modification to the present invention and not depart from the spirit and scope of the present invention.Like this, if these amendments of the present invention and modification belong within the scope of the claims in the present invention and equivalent technologies thereof, then the present invention 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. a training bootstrap technique for aircraft, comprises the following steps:
Store the program of the described aircraft of operation;
Respond to the current residing status information of described aircraft;
According to described induction information, read corresponding operating or the action of described storage, send cue to user, prompting user completes appointment flare maneuver.
3. the training bootstrap technique of aircraft according to claim 2, is characterized in that: the described program storing the described aircraft of operation comprises and stores 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.
4. the training bootstrap technique of aircraft according to claim 2, is characterized in that: 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.
5. the training bootstrap technique of aircraft according to claim 2, is characterized in that: described prompting mode comprises voice signal prompting and/or picture signal prompting and/or letter signal and points out.
6. the training bootstrap technique of aircraft according to claim 2, it is characterized in that: 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.
7. the training bootstrap technique of the aircraft according to claim 2 or 6, it is characterized in that: 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.
8. the training bootstrap technique of aircraft according to claim 3, is characterized in that: 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.
9. the training bootstrap technique of aircraft according to claim 3, is characterized in that: described in self-inspection boot of taking off comprise flight state training and/or aircraft and telepilot code is trained.
10. the training bootstrap technique of aircraft according to claim 3, is characterized in that: 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.
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