CN104867371B - The training guide and method of a kind of aircraft - Google Patents
The training guide and method of a kind of aircraft Download PDFInfo
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- CN104867371B CN104867371B CN201510290670.6A CN201510290670A CN104867371B CN 104867371 B CN104867371 B CN 104867371B CN 201510290670 A CN201510290670 A CN 201510290670A CN 104867371 B CN104867371 B CN 104867371B
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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
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Abstract
The invention discloses the training guide and method of a kind of aircraft, belong to technical field of aerospace.Training guide includes that guiding user's operation aircraft is implemented to specify the guiding module of flare maneuver, guiding module to further include operating database, sensing unit and Tip element, wherein, operating database is applied to the program of storage operation aircraft；Sensing unit is applied to the state of sensing aircraft, produces feedback information；According to the feedback information of sensing unit, corresponding operating or action in read operation database issue the user with cue, point out user to complete to specify flare maneuver Tip element.User is set by the present invention and instructs program, assist the functions such as the flare maneuver and application operating of user learning aircraft, greatly improve the operating experience of user, and the enjoyment for driving aircraft can be enjoyed.
Description
Technical field
The present invention relates to aviation and automatic control technology field, and in particular to a kind of training guide of aircraft and side
Method.
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.With
Developing rapidly for electronic technology, small-sized, MAV has obvious prominent in Remote, cruising time, flight quality
It is broken, become the General Aviation field focus risen in recent years, it is generally considered with good development prospect.
Current unmanned plane has begun to enter consumer level market, especially multi-rotor aerocraft, typically, is revolved such as four axles more
Rotor aircraft is had become in consumer level market for implementing the preferred unit taken photo by plane.
Prior art is positioned concern is primarily with Navigation of Pilotless Aircraft and how realized by various methods, for example：Application No.
201310059457.5th, it is entitled《The unmanned plane dynamic target tracking and localization method of a kind of view-based access control model》Middle promulgated by the State Council
Bright patent application discloses the unmanned plane dynamic target tracking and localization method of a kind of view-based access control model, and the present invention is completed to motion mesh
Target detection, image trace, deflect optical axis automatically, dynamic object is presented on imaging plane center all the time, are obtaining unmanned plane
The distance between unmanned plane and dynamic object are measured in real time according to the model set up on the basis of elevation information, so as to realize to dynamic
The positioning of state target, in this, as feedback signal, forms closed-loop control, guides the tracking flight of unmanned plane.
Because multi-rotor aerocraft is a kind of airflight equipment, manipulation gets up to acquire a certain degree of difficulty, in the air flight course
In, once failure is possible to airflight accident occur.In the prior art, Application No. 201410006690.1, hair
It is bright entitled《For the system of the task guiding of operational administrative in aircraft cockpit》Chinese invention patent application disclose
For the system and computer-readable medium of the task guiding of operational administrative in aircraft cockpit, including draw for providing task
The system and computer-readable medium led, fly for being managed during the abnormal conditions that normal operating procedure or anomalous event cause
Row operation.System for providing task guiding can include processor, memory and be configured to be connect from multiple servers
Receive the flight supplementary module of data.Supplementary module can show possible aircraft flight rank while mission phase is indicated
Section.Supplementary module can also be shown for mission phase operation to be performed, and the action corresponding with these operations.The hair
It is bright to be operated for convenience of crew, standard and exception program and control device is arranged into a center system.
But above-mentioned patent application does not provide how to help user-friendly study multi-rotor aerocraft driving efficiency
Technical scheme.And active user is only capable of being realized by specification or operation interface for the use of multi-rotor aerocraft, learn
Habit process is unfriendly, so as to reduce the Consumer's Experience of multi-rotor aerocraft.Also, learnt in this uncertain mode, it is right
Safe flight, functional development of multi-rotor aerocraft etc. can all bring great hidden danger.User is probably because be unfamiliar with many rotations
The performance of rotor aircraft and cause aircraft accident, also likely because not knowing that multi-rotor aerocraft can accomplish more flights
Action, and lose to interest of multi-rotor aerocraft etc..
Therefore, it is necessary to an incremental process can be set, help user gradually complete in the way of intelligently guiding
The study that paired multi-rotor aerocraft is manipulated, by well-designed bootstrap, can allow novice users correctly to be grasped many
The manipulation skill of rotor craft, can also allow novice users to understand the repertoire achieved by multi-rotor aerocraft.
The content of the invention
Goal of the invention of the invention is to provide the training guide and method of a kind of aircraft, regarding to the issue above, leads to
Cross the intelligently guiding program that design is combined with aircraft, the driving efficiency of teaching user association aircraft and integrated application, pole
The manipulation experience of big lifting user, and the enjoyment for driving aircraft can be enjoyed.
In order to solve the above-mentioned technical problem, the technical solution adopted by the present invention is as follows：
A kind of training guide of aircraft, the training guide includes that guiding user operates the aircraft reality
The guiding module that specified flare maneuver specifies flare maneuver is applied, the guiding module further includes that operating database, sensing are single
Unit and Tip element, wherein,
The operating database is applied to the program of the storage operation aircraft；
The sensing unit is applied to the state of the sensing aircraft, produces feedback information, the state of the aircraft
Including flight attitude and/or flare maneuver；
The Tip element reads the corresponding operating in the operating database according to the feedback information of the sensing unit
Or action, cue is issued the user with, point out user to complete the specified flare maneuver.
According to another aspect of the present invention, there is provided a kind of training bootstrap technique of aircraft, comprise the following steps：
The program of the storage operation aircraft；
Sense the aircraft state in which, produce feedback information；
According to the induction information, corresponding operating or the action of the storage are read, issue the user with cue, carried
Show that user completes to specify flare maneuver.
Further, the program of the storage operation aircraft include storage Basic Flight Maneuver bootstrap and/
Or take off self-inspection bootstrap and/or combination flare maneuver bootstrap and/or malfunction elimination bootstrap and/or integrated application
Bootstrap.
Further, the induction mode includes the flight of GPS location signal and/or altimeter signal and/or remote control
Control instruction judges signal and/or sensor sensing signal.
Further, the prompting mode includes that voice signal is pointed out and/or picture signal is pointed out and/or letter signal is carried
Show.
Further, the user profile and the airmanship corresponding to the user of the aircraft are also driven including identification
Information, the airmanship information according to the user, provides corresponding operation guide.
Further, also including determining the aircraft flight during the specified flare maneuver flight path with it is described
Deviation between aircraft current location, corresponding prompt message is given according to the deviation information.
Further, the Basic Flight Maneuver bootstrap include Throttle Opening Control train and/or front and rear flight training and/
Or left and right sides flies training and/or mouth word flight training.
Further, the self-inspection bootstrap of taking off is trained and/or aircraft and remote control including flight state
Code is trained.
Further, the combination flare maneuver bootstrap includes formula mouthful word train before spiraling training and/or head
And/or pinpoint landing training and/or given line training.The invention discloses a kind of training guide of aircraft and side
Method, by well-designed intelligently guiding program, incremental guiding user completes the study to aircraft control, can either
Novice users are allowed correctly to grasp the driving skills of aircraft, it is also possible to allow novice users to understand the whole work(achieved by aircraft
Can, the manipulation experience of user is greatly improved, and allow users to enjoy the enjoyment for driving aircraft.
Described above is only the general introduction of technical solution of the present invention, in order to cause technological means of the invention clearer
Understand, reach the degree that those skilled in the art can be practiced according to the content of specification, and in order to allow the present invention
Above and other objects, features and advantages can become apparent, illustrated with specific embodiment of the invention below
Explanation.
Brief description of the drawings
By reading the detailed description in hereafter preferred embodiment, the present invention various other advantage and benefit
Will be clear understanding for those of ordinary skill in the art.Figure of description is only used for showing the purpose of preferred embodiment,
And it is not considered as limitation of the present invention.It should be evident that drawings discussed below is only some embodiments of the present invention,
For those of ordinary skill in the art, on the premise of not paying creative work, can also be obtained according to these accompanying drawings
Other accompanying drawings.And in whole accompanying drawing, identical part is denoted by the same reference numerals.In the accompanying drawings：
Fig. 1 shows the training guiding arrangement structure block diagram of according to embodiments of the present invention one aircraft；
Fig. 2 shows the training guiding arrangement structure block diagram of according to embodiments of the present invention two aircraft；
Fig. 3 shows the training guiding arrangement structure block diagram of according to embodiments of the present invention three aircraft；
Fig. 4 shows the training guiding arrangement structure block diagram of according to embodiments of the present invention four aircraft；
Fig. 5 shows the training bootstrap technique flow chart of according to embodiments of the present invention five aircraft；
Fig. 6 shows throttle in the training guide or method of the aircraft described according to embodiments of the present invention to five
The bootstrap technique flow chart that climbs of controlled training.
Specific embodiment
Specific embodiment of the invention is more fully described below with reference to accompanying drawings.Although being shown in accompanying drawing of the invention
Specific embodiment, it being understood, however, that may be realized in various forms the present invention without that should be limited by embodiments set forth here
System.Conversely, there is provided these embodiments are able to be best understood from the present invention, and can be complete by the scope of the present invention
Convey to those skilled in the art.
It should be noted that having used some vocabulary to censure specific components in the middle of specification and claim.Ability
Field technique personnel it would be appreciated that, hardware manufacturer may call same component with different nouns.This specification and power
Profit is required not in the way of the difference of noun is used as distinguishing component, but the difference with component functionally is used as distinguishing
Criterion.As the "comprising" in specification in the whole text and claim mentioned in or " including " be an open language, therefore should
It is construed to " include but be not limited to ".To implement better embodiment of the invention, so description is specification subsequent descriptions
For the purpose of the rule of specification, the scope of the present invention is not limited to.Protection scope of the present invention is when regarding appended power
Profit requires that the person of defining is defined.
For ease of the understanding to the embodiment of the present invention, done by taking several specific embodiments as an example further below in conjunction with accompanying drawing
Explanation, and each accompanying drawing does not constitute the restriction to the embodiment of the present invention.
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.Can be divided into from technical standpoint definition：Depopulated helicopter, unmanned fixed-wing aircraft,
Unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc..
Preferred unmanned plane is multi-rotor unmanned aerial vehicle (or being multi-rotor aerocraft) in the embodiment of the present invention, can be four
Rotor, six rotors and rotor quantity are more than six and are the unmanned plane of even number, and the multi-rotor unmanned aerial vehicle includes streamlined in strip
Fuselage, fuselage substantially rectangular structure, its corner and corner be flowing transition so that air fuselage table
Surface current is out-of-date to show as laminar flow, so as to reduce resistance of the multi-rotor unmanned aerial vehicle in flight course.Preferably, fuselage is by carbon fiber
Material is made, and on the premise of use intensity higher and rigidity is met, can significantly mitigate the weight of fuselage, so as to reduce many rotors
The power demand of unmanned plane and the mobility of raising multi-rotor unmanned aerial vehicle.Certainly, in other embodiments of the invention, fuselage
Can also be made up of plastics or other arbitrarily used materials.Fuselage be provided with it is multiple relative to the fuselage in it is symmetrical flat
The slurry arm that face is symmetric, each slurry arm is provided with paddle components away from one end of the fuselage, and the paddle components include
Motor and the blade being connected on the output shaft of the motor on the slurry arm, the rotation axis per a piece of blade are equal
On the same face of cylinder.
Certainly, the explanation of the multi-rotor unmanned aerial vehicle is a simple declaration, specifically also includes many other compositions
Component, also also has other many kinds of unmanned plane types, may be incorporated for realizing the purpose of the present invention, will not be repeated here.
But, come for the development trend of the manipulation convenience that flight shoots from the demand in consumer level market and user
See, the flight capture apparatus of technical solution of the present invention are primarily referred to as small, miniature multi-rotor unmanned aerial vehicle, this unmanned plane small volume,
Preferably, it is low that flight shoots cost for low cost, flight stability.The aircraft that the present invention is used, typically with many rotors of four axles
Aircraft is representative.Also, this aircraft have begun to be widely used in take photo by plane, the field such as aerial work, logistics.
Embodiment one, a kind of training guide of aircraft.
Fig. 1 is the training guiding arrangement structure block diagram of the aircraft of the embodiment of the present invention one, and the embodiment of the present invention will be combined
Fig. 1 is specifically described.
As shown in figure 1, the embodiment of the invention provides a kind of training guide 101 of aircraft 100, the training is drawn
Leading device 101 includes that guiding user operates the aircraft to implement to specify the guiding module 102 of flare maneuver, the guiding module
102 further include operating database 103, sensing unit 104 and Tip element 105, wherein,
The operating database 103 is applied to the program of the storage operation aircraft 100；
The sensing unit 104 is applied to the state of the sensing aircraft 100, produces feedback information；Shape described here
State includes the flight attitude and/or flare maneuver of the aircraft 100, it might even be possible to senses the aircraft 100 and is currently in
Inactive state, open state, takeoff condition etc..
The Tip element 105 according to the feedback information of the sensing unit 104, in reading the operating database 103
Corresponding operating or action, issue the user with cue, point out user to complete the specified flare maneuver.
Core content is to guide user to learn to drive the work(of aircraft by gradual and orderly approach in the technical program
Can module.
Preferred in the embodiment of the present invention, the training guide 101 can be with integrated design in the aircraft 100
In, or a single physical unit, can also be integrated in the central control system of ground, the training guide
101 particular locations for setting are unimportant, as long as having the functional module.
Preferred in the embodiment of the present invention, the induction mode of the sensing unit 104 includes GPS location signal and/or height
The flight control instruction of degree instrument signal and/or remote control judges signal and/or sensor sensing signal.Sensor described here
Including gyroscope, acceleration transducer etc..
In an alternative embodiment of the invention, the sensing unit 104 can also manually select the sensing of triggering using user
Mode, the self-inspection guidance unit for example, the selection of active user's point touching screen is taken off.
In an alternative embodiment of the invention, the working method of the Tip element 105 is actively prompting, sends guiding letter
Number, now sensing unit described here 104 can to the operation on a certain device on the aircraft 100 or automatic running to certain
One state is detected, for example, it is possible to after the aircraft 100 1 is started shooting, the sensing unit 104 detects the start
Action, then provide a prompt message first, and then the sensing unit 104 further gathers the information of the aircraft 100,
The indication of next step is carried out according to the information for being gathered.
In the embodiment of the present invention preferred, the guiding module 102 is achieved in that：The aircraft 100 is according to pre-
If program, sound/light/image/letter signal is issued the user with, point out user to complete guiding action, the aircraft 100 passes through institute
State sensing unit 104 sense user be basically completed guiding action (this induction mode, both can be according to GPS location signal, height
Degree instrument signal etc., it is also possible to according to the judgement of the flight control instruction from remote control, both modes can also be comprehensively utilized
Obtain more accurately judged result), then prompting is provided, and according to the preset strategy of the guiding module 102, carry out next drawing
Lead the prompting of action.
It is preferred in the embodiment of the present invention, the Tip element include voice signal point out and/or picture signal prompting and/
Or letter signal prompting.The concrete mode of guiding, including the mode reminded with the voice signal for pre-storing, or
The image that to pre-store, letter signal include the mode on user's controller at one's side or other-end, can also be and appoint
What can effectively pass on the mode of guidance information or signal.
Embodiment two, a kind of training guide of aircraft.
Fig. 2 is a kind of training guiding arrangement structure block diagram of aircraft of the embodiment of the present invention two, and the embodiment of the present invention will
It is specifically described with reference to Fig. 2.
As shown in Fig. 2 the embodiment of the invention provides a kind of training guide 101 of aircraft 100, the training is drawn
Leading device 101 includes that guiding user operates the aircraft to implement to specify the guiding module 102 of flare maneuver, the guiding module
102 further include operating database 103, sensing unit 104 and Tip element 105, wherein, the operating database 103 is wrapped
Include 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, the Basic Flight Maneuver guidance unit 201 includes that Throttle Opening Control training is single
First and/or front and rear flight training subelement and/or left and right sides fly training subelement and/or mouth word flight training subelement.
Specifically, being illustrated by taking Throttle Opening Control training subelement as an example：
With left hand control throttle by aircraft heading about 100, guiding user learning aircraft 100 climbs and flies
The decline of row device 100.
The guiding of climbing of aircraft 100, its main points is：Power is provided with fast speed, it is ensured that aircraft 100 exists by throttle
When reaching high height in visual range, some throttles are decreased slightly as, are properly done hovering；
The landing of aircraft 100 is guided, and its main points is：Should not rapidly allow the stall of aircraft 100, allow aircraft 100 slowly
Fall earthward；
Repeat the process climbed-hover-land three times of aircraft 100；
The lifting of aircraft 100 combines guiding, and its main points is：By training above aircraft 100 can be risen rapidly
High height in visual range, slowly can stably be down to ground again.
The hovering of aircraft 100 is guided, and its main points is：Allow aircraft 100 in visual range a period of time its height protect
Hold constant, when aircraft 100 occurs height change, in time according to situation of change, suitably increase and decrease throttle.
Again for example, being illustrated by taking the front and rear flight training subelement as an example：
With flight before and after right hand control aircraft 100, after aircraft 100 is maintained at certain altitude by left hand, before and after training
Flight.
The preceding winged guiding of aircraft 100, its main points is：With ground mark as object of reference, control aircraft 100 is forward
One unit length of flight；
The rear winged guiding of aircraft 100, its main points is：With ground mark as object of reference, control aircraft 100 is backward
One unit length of flight；
The front and rear flight guiding of aircraft 100 is repeated, its main points is：The control one length list of advance of aircraft 100
Then position, hovering controls aircraft 100 to retreat a long measure again, repeats three times.
Illustrated so that left and right sides flies training as an example：
Flown with right hand control aircraft 100 left and right sides, aircraft 100 is maintained at certain altitude by left hand, trains left and right sides
Fly.Mode is similar with above-mentioned front and rear flight training.
Illustrated by taking mouth word flight training subelement as an example：
By mouth word formula flight training, the above-mentioned flare maneuver of combined training：
Left hand control aircraft 100 hovers in the air, is maintained at the safe altitude of liftoff 30 cm；
Right hand control aircraft 100 decomposes the action of completion mouth word flight clockwise several times in the air, specific as follows：Before
Fly a long measure, flight one long measure in right side flies a long measure, one long measure of left side flight afterwards；
Right hand control aircraft 100 decomposes the action of completion mouth word flight counterclockwise several times in the air, specific as follows：Before
Fly a long measure, flight one long measure in left side flies a long measure, one long measure of right side flight afterwards.
Preferred in the embodiment of the present invention, the self-inspection guidance unit 202 that takes off trains subelement including flight state
And/or aircraft trains subelement with remote control to code.
Illustrated by taking flight state training subelement as an example：
Aircraft 100 sends prompt message, asks user to confirm whether the state warning lamp of aircraft 100 is all working properly,
Such as：Whether power supply indicator is evergreen, and (evergreen expression electric power is sufficient, and flicker represents that voltage is less than 50%, and red represents that voltage is low
Can not be taken off in 10%), whether malfunction indicator lamp is extinguished, and whether fore-and-aft direction indicator lamp is lighted.
Illustrated so that the aircraft trains subelement with remote control to code as an example：
Aircraft 100 is pointed out currently to code state, judges whether to have completed to code；
When aircraft 100 points out to have does not complete the remote control to code, be given to code prompt message, such as prompting user will
Aircraft 100 is placed on horizontal departure location, point out in user's remote controller to code function key, and be given to code signal
(such as, can shift throttle onto maximum rapidly, the command signal that minimum is then pushed back rapidly is used as to code cue).
It is preferred in the embodiment of the present invention, for maiden flight aircraft 100 described in aircraft with remote control to code
Training subelement also includes setting the prompting subelement for reminding subelement and/or remote control pattern to set of horizontal alignment.
Specifically, the calibrated prompting subelement of the setting level can be：
User is reminded to be placed on horizontal position by aircraft 100 is static；
Two control sticks of user's remote control are reminded to get to special angle, such as the lower left corner simultaneously；
User is reminded to unclamp control stick when the fore-and-aft direction lamp of aircraft 100 flashes simultaneously；
User is reminded to confirm whether aircraft 100 gives the signal of fore-and-aft direction lamp Chang Liang to represent calibration completion.
Adopt and reminded in this way, can allow complicated horizontal alignment for a user, resolved into step by step
Clear and easy to understand instruction, reduces the study understanding cost of user.
Specifically, the prompting subelement that the remote control pattern is set refers to：
After remote control first time is to code, default setting is 4 channel patterns, now issues the user with prompt message, informs use
Family：The left side control stick above-below direction of remote control is throttle, controls the rising and decline of aircraft 100, left side control stick or so
Direction is control rotation；Right-hand joystick above-below direction is the forward-reverse for controlling aircraft 100, and left and right directions is control flight
The left and right sides direction flight of device 100.
According to the difference of remote control, may there are other auxiliary key mappings, now aircraft 100 is also issued the user with and carried successively
Show information, such as：The fine setting of four direction is good for, and the function of LR key mappings, 3 channel patterns (are carried with the function of 4 channel pattern switch keys
Show long by one second switch mode).
For another example, may there are speed key and rolling key：The speed key divides speed step with gear, and (prompting user is not
Corresponding what situation of same speed step)；The rolling key need to coordinate with right control stick, after the rolling key function setting is good,
Realized being rolled to respective direction with right control stick.
Preferred in the embodiment of the present invention, the combination flare maneuver guidance unit 203 includes that spiraling training is single
Formula mouthful word train subelement and/or pinpoint landing training subelement and/or given line training subelement before unit and/or head.
Specifically, the spiraling training subelement includes：
By taking the control spiraling of left and right as an example, while aircraft 100 is maintained at certain altitude by left hand, training rotation flies
OK.
Mode is similar with above-mentioned front and rear flight training, including a left side turn 90 degrees, reduction, repeats consolidation；The right side turn 90 degrees, also
Original, repeats consolidation.
Specifically, formula mouthful word train subelement includes before the head：
The head orientation movements direction all the time of aircraft 100 is kept, with work and the spinning movement of preceding flying, is sequentially completed suitable
Hour hands flight mouth word, the training of flight mouth word counterclockwise.Specific training method is similar with aforementioned schemes, repeats no more.
Specifically, the pinpoint landing training subelement includes：
One landing place is provided on map by aircraft at random, it is desirable to which user within a specified time, completes original place and rises
Fly the task with pinpoint landing, training is several times.
Specifically, the given line training subelement includes：
One given line is provided on map by aircraft at random, wherein being set with some anchor points, user need to specify
In time, the aerial mission of given line is completed, and hovering verification is completed in each anchor point, training is several times.
Other contents of the embodiment of the present invention will not be repeated here with reference to foregoing invention embodiment one.
Embodiment three, a kind of training guide of aircraft.
Fig. 3 is a kind of training guiding arrangement structure block diagram of aircraft of the embodiment of the present invention three, and the embodiment of the present invention will
It is specifically described with reference to Fig. 3.
As shown in figure 3, the embodiment of the invention provides a kind of training guide 101 of aircraft 100, the training is drawn
Leading device 101 includes that guiding user operates the aircraft to implement to specify the guiding module 102 of flare maneuver, the guiding module
102 further include operating database 103, sensing unit 104 and Tip element 105.The training guide 101 also includes
User Information Database 301, it is applied to therefrom identification and drives the user profile of the aircraft and corresponding to the user's
Airmanship information.
Preferred in the embodiment of the present invention, the training guide 101 identifies currently drive the aircraft first
100 user, can be identified from the specific id information for sending, or from the life including fingerprint, recognition of face etc.
Thing information is identified, and reads the airmanship information of correspondence user, and root from the User Information Database 301 afterwards
According to the airmanship information, corresponding operation indicating is given.Airmanship information described here, can be manual entry
The personal considerations of the user, for example height and weight age health status, or from the guiding module 102 gather should
Operation note before user, according to operation note before, judges user driving ability residing at present, and selection is adapted to should
The bootstrap of user.If for example, user's airmanship is poor, can since most basic bootstrap, if
User's airmanship is very outstanding, then directly since grade of difficulty bootstrap high can so increase user
Driving experience.
Other contents refer to above-described embodiment one and embodiment two in the embodiment of the present invention, will not be repeated here.
Example IV, a kind of training guide of aircraft.
Fig. 4 is a kind of training guiding arrangement structure block diagram of aircraft of the embodiment of the present invention four, and the embodiment of the present invention will
It is specifically described with reference to Fig. 4.
As shown in figure 4, the embodiment of the invention provides a kind of training guide 101 of aircraft 100, the training is drawn
Leading device 101 includes that guiding user operates the aircraft to implement to specify the guiding module 102 of flare maneuver, the guiding module
102 further include operating database 103, sensing unit 104 and Tip element 105.The training guide 101 also includes
Electronic control module 401, its be applied to determine the aircraft 100 fly during the specified flare maneuver flight path with
Deviation between the current location of the aircraft 100, including positioning unit and processor unit, the electronic control module and institute
State operating database electrical connection.Here positioning unit can use GPS positioning technology, it would however also be possible to employ Beidou navigation technology,
Or any ripe technology suitable for aerial vehicle trajectory positioning.The electronic control module by with the operand
Electrically connected according to storehouse, the flight path of the specified flare maneuver during obtaining the aircraft flight, by the flight path information
With the input of the location information of the positioning unit and then the processor unit, by the treatment of the processor unit, obtain
Deviation during the aircraft flight between the flight path of the specified flare maneuver and the aircraft current location, will
The deviation information of acquisition is input into the Tip element, gives active user correct indication.
Preferred in the embodiment of the present invention, the current location information of the aircraft 100 can be by the sensing unit
104 obtain, it is also possible to obtained by other control process devices.The specified flare maneuver during the flight of the aircraft 100
Flight path can be obtained from the operating database 103.Believe when the electronic control module 401 obtains deviation by algorithm
During breath, then feedback information is provided to the guiding module 102 according to the deviation information, give the user corresponding prompting letter
Breath, for example, during the front and rear flight training, the Tip element 105 points out user with ground mark as reference
Thing, controls 100 flight forward of aircraft one unit length, because user operates unskilled, half of a flight forward
Unit length has exceeded a unit length, and at this moment the electronic control module 401 will be anti-to the guiding module 102
Present the deviation information of " the also poor half unit length of flight forward has been over a unit length ", the Tip element
105 can now point out user, and " you need to continue flight forward half unit length or you have exceeded a unit length！”.
Other contents will not be repeated here with reference to above-described embodiment one to embodiment three in the embodiment of the present invention.
The training bootstrap technique of embodiment five, a kind of aircraft.
Fig. 5 is the training bootstrap technique flow chart according to the aircraft of the embodiment of the present invention five, and the embodiment of the present invention will be tied
Fig. 5 is closed to be specifically described.
As shown in figure 5, a kind of training bootstrap technique of aircraft, comprises the following steps：
Step S501：The program of the storage operation aircraft；
Step S502：Sense the status information that the aircraft is presently in；
Step S503：According to the status information, the corresponding operating of the storage is read, issues the user with cue,
Prompting user completes to specify flare maneuver.
Preferred in the embodiment of the present invention, the program of the storage operation aircraft includes storage Basic Flight Maneuver
Bootstrap and/or take off self-inspection bootstrap and/or combination flare maneuver bootstrap and/or malfunction elimination bootstrap
And/or integrated application bootstrap.
It is preferred in the embodiment of the present invention, the induction mode include GPS location signal and/or altimeter signal and/or
The flight control instruction of remote control judges signal and/or sensor sensing signal.
It is preferred in the embodiment of the present invention, the prompting mode include voice signal point out and/or picture signal prompting and/
Or letter signal prompting.
It is preferred in the embodiment of the present invention, also drive the user profile of the aircraft and corresponding to the use including identification
The airmanship information at family, the airmanship information according to the user, provides corresponding operation guide.
It is preferred in the embodiment of the present invention, also including determining the aircraft flight during the specified flare maneuver fly
Deviation between row track and the aircraft current location, corresponding prompt message is given according to the deviation information.
Preferred in the embodiment of the present invention, the Basic Flight Maneuver bootstrap includes that Throttle Opening Control is trained and/or preceding
Flight training and/or left and right sides fly training and/or mouth word flight training afterwards.
Preferred in the embodiment of the present invention, the self-inspection bootstrap of taking off is trained and/or flown including flight state
Device is trained with remote control to code.
Preferred in the embodiment of the present invention, the combination flare maneuver bootstrap includes spiraling training and/or head
Preceding formula mouthful 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 is set with guidance mode in guiding content design
On meter.Wherein, guiding content uses incremental design, and guiding user association manipulates aircraft；And guidance mode is then
Be using information alert, etc. to be operated, results verification, flow judge, the endless form of next information alert is realized.
Other contents refer to foregoing invention embodiment one to four in the embodiment of the present invention, will not be repeated here.
Fig. 6 be the aircraft according to the embodiment of the present invention one to five training guide or method in Throttle Opening Control
The bootstrap technique flow chart that climbs of training, will be specifically described with reference to Fig. 6.
As shown in fig. 6, the bootstrap technique that climbs is comprised the following steps：
Step S601：Prompting user's selection guiding content；
Step S602：Prompting user starts Throttle Opening Control training；
Step S603：Prompting user carries out ramp-up period training；
Step S604：The instruction of climbing for waiting user to send；
Step S605：Judge whether to receive instruction；If the instruction of climbing of user is received, into next step；Conversely, jumping
Go to step S611；
Step S606：Judge whether the instruction of climbing of user is correct；If instruction is correct, into next step；Conversely, jumping
Go to step S612；
Step S607：Judge the instruction of climbing of user whether beyond limitation of climbing；If without departing from limitation of climbing, entered
Enter next step；Conversely, jumping to step S613；
Step S608：Perform the instruction of climbing of user；
Step S609：Judge whether to achieve the goal；If achieved the goal, into next step；Conversely, jumping back to step
S603 continues to point out user to be climbed；
Step S610：Terminate training of climbing.
Step S611：Judge whether the stand-by period is overtime；If not timed out, then jump back to step S604 continue waiting for use
Family is climbed instruction；If it times out, jumping to step S610 terminates training of climbing.
Step S612：Prompting user currently climbs instruction errors, and jumps back to step S603 and continue to point out user to be climbed
Rise training.
Step S613：Prompting user provides restricted information, and jumps back to step S603 and continue to point out to use beyond limitation of climbing
Family carries out training of climbing.
In several embodiments provided by the present invention, it should be understood that disclosed apparatus and method, can be by it
Its mode is realized.For example, device embodiment described above is only schematical, for example, the module or unit
Divide, only a kind of division of logic function there can be other dividing mode when actually realizing, for example multiple units or component
Can combine or be desirably integrated into another system, or some features can be ignored, or do not perform.It is another, it is shown or
The coupling each other for discussing or direct-coupling or communication connection can be the indirect couplings of device or unit by some interfaces
Close or communicate to connect, can be electrical, mechanical or other forms.
It is described as separating component illustrate module or unit can be or may not be it is physically separate, as
The part that unit shows can be or may not be physical location, you can with positioned at a place, or can also be distributed
Onto multiple NEs.Some or all of unit therein can be according to the actual needs selected to realize the present embodiment side
The purpose of case.
In addition, during each functional unit in each embodiment of the invention can be integrated in a processing unit, it is also possible to
It is that unit is individually physically present, it is also possible to which two or more units are integrated in a unit.Above-mentioned integrated list
Unit can both be realized in the form of hardware, it would however also be possible to employ the form of SFU software functional unit is realized.
If the integrated unit is to realize in the form of SFU software functional unit and as independent production marketing or use
When, can store in a computer read/write memory medium.Based on such understanding, technical scheme is substantially
The part for being contributed to prior art in other words or all or part of the technical scheme can be in the form of software products
Embody, the computer software product is stored in a storage medium, including some instructions are used to so that a computer
Equipment (can be personal computer, server, or network equipment etc.) or processor (processor) perform the present invention each
The all or part of step of embodiment methods described.And foregoing storage medium includes：USB flash disk, mobile hard disk, read-only storage
(ROM, Read-OnlyMemory), random access memory (RAM, RandomAccessMemory), magnetic disc or CD etc. are each
Planting can be with the medium of store program codes.
The present invention can bring these beneficial technique effects：The training guiding dress of aircraft disclosed in the embodiment of the present invention
Put and method, by designing intelligentized bootstrap, guide user to learn to manipulate aircraft in incremental mode, in advance
The program of storage operation aircraft, the state and the airmanship of user being presently according to aircraft issues the user with prompting
Signal, points out user to complete to specify flare maneuver, is easy to user quickly to grasp the driving efficiency of aircraft, reduces of user
Cost is practised, the security in learning process is increased, the manipulation experience of user is greatly improved.
One of ordinary skill in the art will appreciate that：Accompanying drawing is the schematic diagram of one embodiment, module in accompanying drawing or
Flow is not necessarily implemented necessary to the present invention.
Embodiments of the invention are the foregoing is only, the scope of the claims of the invention is not thereby limited, it is every to utilize this hair
Equivalent structure or equivalent flow conversion that bright specification and accompanying drawing content are made, or directly or indirectly it is used in other related skills
Art field, is included within the scope of the present invention.
Obviously, those skilled in the art can carry out various changes and modification without deviating from essence of the invention to the present invention
God and scope.So, if these modifications of the invention and modification belong to the scope of the claims in the present invention and its equivalent technologies
Within, then the present invention is also intended to comprising these changes and modification.
Claims (10)
1. the training guide of a kind of aircraft, it is characterised in that：The training guide includes guiding user's operation institute
Aircraft is stated to implement to specify the guiding module of flare maneuver, the guiding module to further include operating database, sensing unit
And Tip element, wherein,
The operating database is applied to the program of the storage operation aircraft；
The sensing unit is applied to the state of the sensing aircraft, produces feedback information, and the state of the aircraft includes
Flight attitude and/or flare maneuver；
The Tip element according to the feedback information of the sensing unit, read corresponding operating in the operating database or
Action, issues the user with cue, points out user to complete the specified flare maneuver.
2. a kind of training bootstrap technique of aircraft, comprises the following steps：
The program of the storage operation aircraft；
Sense the status information that the aircraft is presently in；
According to the induction information, corresponding operating or the action of the storage are read, issue the user with cue, point out to use
Family completes to specify flare maneuver.
3. the training bootstrap technique of aircraft according to claim 2, it is characterised in that：The storage operation flight
The program of device include storage Basic Flight Maneuver bootstrap and/or take off self-inspection bootstrap and/or combination flare maneuver draw
Helical pitch sequence and/or malfunction elimination bootstrap and/or integrated application bootstrap.
4. the training bootstrap technique of aircraft according to claim 2, it is characterised in that：The induction mode includes GPS
The flight control instruction of framing signal and/or altimeter signal and/or remote control judges signal and/or sensor sensing signal.
5. the training bootstrap technique of aircraft according to claim 2, it is characterised in that：The prompting mode includes voice
Signal prompt and/or picture signal prompting and/or letter signal prompting.
6. the training bootstrap technique of aircraft according to claim 2, it is characterised in that：Also include that identification drives described flying
The user profile of row device and the airmanship information corresponding to the user, the airmanship information according to the user provide phase
The operation guide answered.
7. the training bootstrap technique of the aircraft according to claim 2 or 6, it is characterised in that：Also include determining described flying
Deviation during the flight of row device between the flight path of the specified flare maneuver and the aircraft current location, according to described
Deviation information provides corresponding prompt message.
8. the training bootstrap technique of aircraft according to claim 3, it is characterised in that：The Basic Flight Maneuver guiding
Program includes that Throttle Opening Control is trained and/or front and rear flight training and/or the winged training of left and right sides and/or mouth word flight training.
9. the training bootstrap technique of aircraft according to claim 3, it is characterised in that：The self-inspection bootstrap of taking off
Code is trained with remote control including flight state training and/or aircraft.
10. the training bootstrap technique of aircraft according to claim 3, it is characterised in that：The combination flare maneuver draws
Helical pitch sequence includes formula mouthful word train and/or pinpoint landing training and/or given line training before spiraling training and/or head.
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| CN201510290670.6A CN104867371B (en) | 2015-05-29 | 2015-05-29 | The training guide and method of a kind of aircraft |
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| CN201510290670.6A CN104867371B (en) | 2015-05-29 | 2015-05-29 | The training guide and method of a kind of aircraft |
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