CN110291012A - Control method, device and control device, aircraft, the flight system of searchlight - Google Patents

Control method, device and control device, aircraft, the flight system of searchlight Download PDF

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Publication number
CN110291012A
CN110291012A CN201880010549.5A CN201880010549A CN110291012A CN 110291012 A CN110291012 A CN 110291012A CN 201880010549 A CN201880010549 A CN 201880010549A CN 110291012 A CN110291012 A CN 110291012A
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CN
China
Prior art keywords
searchlight
working condition
high brightness
brightness
work
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Granted
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CN201880010549.5A
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Chinese (zh)
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CN110291012B (en
Inventor
刘煜程
高诗经
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Shenzhen Dajiang Innovations Technology Co Ltd
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Shenzhen Dajiang Innovations Technology Co Ltd
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Priority to CN202111566909.XA priority Critical patent/CN114281106A/en
Publication of CN110291012A publication Critical patent/CN110291012A/en
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Publication of CN110291012B publication Critical patent/CN110291012B/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/02Arrangements or adaptations of signal or lighting devices
    • B64D47/04Arrangements or adaptations of signal or lighting devices the lighting devices being primarily intended to illuminate the way ahead
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B47/00Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
    • H05B47/10Controlling the light source
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02BCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B20/00Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
    • Y02B20/40Control techniques providing energy savings, e.g. smart controller or presence detection

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Circuit Arrangement For Electric Light Sources In General (AREA)

Abstract

Provide control method, device and control device, aircraft, the flight system of a kind of searchlight, the described method includes: when the working condition of the searchlight is high brightness working condition, the first job information for obtaining the searchlight, refers in high brightness working condition: the light emission luminance of the searchlight work at present is higher than preset first luminance threshold;If the first job information meets preset control condition, it is adjusted according to light emission luminance of the predetermined luminance value to the searchlight work at present;The predetermined luminance value is lower than first luminance threshold.The embodiment of the present invention can not only realize searchlight function on board the aircraft, additionally it is possible to automate, intelligently guarantee searchlight safe handling, the flight safety of the aircraft also guaranteed.

Description

Control method, device and control device, aircraft, the flight system of searchlight
Technical field
The present invention relates to electronic technology field more particularly to a kind of light-emitting control methods of searchlight, device and control dress It sets, aircraft, flight system.
Background technique
With the development of electronic technology and the communication technology, aircraft has obtained great development, especially some consumer levels The aircraft of remote-controlled control can execute various tasks in many occasions, such as pass through and carry video camera Aircraft executes video capture, geology monitoring, electric inspection process etc..
In some aircraft products, some night missions are needed to be implemented sometimes or in light than under darker environment Task.Such as some farmers night inspection task that needs to make an inspection tour farm at night or some mining sites are at night Between it is on duty, need aircraft temporarily to execute illumination task etc..Under these scenes, how these are executed by aircraft Business has become a hot topic of research problem.
Summary of the invention
The embodiment of the invention provides a kind of light-emitting control method of searchlight, device and control device, aircraft, flights On the one hand system can be realized illumination by the searchlight of carry on aircraft, on the other hand can also be to the brightness of searchlight Carry out intelligent control.
On the one hand, the embodiment of the invention provides a kind of light-emitting control method of searchlight, the searchlight setting is flying On row device, which comprises
Detect the working condition for the searchlight being arranged on board the aircraft;
When the working condition of the searchlight is high brightness working condition, the first work letter of the searchlight is obtained Breath, refers in high brightness working condition: the light emission luminance of the searchlight work at present is higher than preset first luminance threshold;
If the first job information meets preset control condition, according to predetermined luminance value to the current work of the searchlight The light emission luminance of work is adjusted;
The predetermined luminance value is lower than first luminance threshold.
On the other hand, the embodiment of the invention also provides a kind of emission control device of searchlight, the searchlight settings On board the aircraft, described device includes:
Obtain module, for the working condition in the searchlight be high brightness working condition when, obtain the searchlight The first job information, refer in high brightness working condition: the light emission luminance of the searchlight work at present be higher than it is preset First luminance threshold;
Processing module, if meeting preset control condition for the first job information, according to predetermined luminance value to institute The light emission luminance for stating searchlight work at present is adjusted;The predetermined luminance value is lower than first luminance threshold.
In another aspect, the embodiment of the invention also provides a kind of emission control device of searchlight, the searchlight setting On board the aircraft, the control device includes: memory and processor;
Program instruction is stored in the memory;
The processor calls the program instruction stored in the memory, for executing following steps:
When the working condition of the searchlight is high brightness working condition, the first work letter of the searchlight is obtained Breath, refers in high brightness working condition: the light emission luminance of the searchlight work at present is higher than preset first luminance threshold;
If the first job information meets preset control condition, according to predetermined luminance value to the current work of the searchlight The light emission luminance of work is adjusted;
The predetermined luminance value is lower than first luminance threshold.
Another aspect, the embodiment of the invention also provides a kind of aircraft, the aircraft includes: aircraft body, visits Illuminator and control device, the searchlight carry is in the aircraft body, the control device and the searchlight phase Even, the control device is used to execute the light-emitting control method of searchlight as described above.
Correspondingly, the embodiment of the invention also provides a kind of flight system, the flight system includes: aircraft, carry In the carry-on searchlight, control device and user terminal;The control device is connected with the searchlight, and The control device is connected with the user terminal, and the control device is used to execute the light emitting control of searchlight as described above Method.
The embodiment of the present invention can not only realize searchlight function on board the aircraft, and can also refer to the work of searchlight Make state to control searchlight, can automate, intelligently guarantee searchlight safe handling, the aircraft also guaranteed Flight safety.
Detailed description of the invention
It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be to institute in embodiment Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the invention Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings Obtain other attached drawings.
Fig. 1 is a kind of operative scenario schematic diagram of aircraft based on carry searchlight of the embodiment of the present invention;
Fig. 2 is a kind of flow diagram of the control method of searchlight of the embodiment of the present invention;
Fig. 3 is the method flow schematic diagram for issuing brightness adjustment instruction of the embodiment of the present invention;
Fig. 4 is a kind of structural schematic diagram of the emission control device of searchlight of the embodiment of the present invention;
Fig. 5 is a kind of structural schematic diagram of control device of the embodiment of the present invention.
Specific embodiment
The mechanical interface and electric interfaces of carry searchlight are provided on the aircraft of the embodiment of the present invention, it is convenient to fly Carry searchlight and the light emission luminance of searchlight, the even luminous parameters such as luminous frequency are controlled on row device.The searchlighting Lamp can be arranged at the positions such as the top, bottom or side of the aircraft with carry, realize different searchlighting functions, searchlighting Mechanical connection manner between lamp and aircraft can be movable connection, can according to need load on board the aircraft in this way Searchlight, or mounted searchlight is removed from aircraft.Also, aircraft can also as needed carry others it is attached Part device, such as carry video camera.
In embodiments of the present invention, it other than carry searchlight can realize searchlighting function on board the aircraft, is also automating Control aspect has planned the corresponding light emitting control logic for being directed to detecting lamp.On the one hand, it can control searchlight work highlighted It spends under working condition, continues to be higher than the high luminance values of the first luminance threshold and shine, such as the first bright threshold value can be equal to Nominal operation brightness or a brightness value greater than nominal operation brightness, such as 120% brightness value of nominal operation brightness, Realize high-intensitive shine preferably to meet certain illumination tasks in special circumstances;On the other hand, it is also considered that long to searchlight It when phase is in high brightness working condition, is easily damaged or power consumption is accelerated, joined high brightness work in logic in light emitting control When defencive function, i.e. searchlight are in high brightness working condition, the first job information for monitoring searchlight can be continued, if first Job information meets preset control condition, then turns down the brightness of searchlight.It in some embodiments, can be in the first work letter When the first represented operating temperature of breath is excessively high, and/or when operating time represented by the first job information is longer, and/or the When electricity represented by one job information is lower, all think to meet control condition, turn down the brightness of searchlight, guarantees searchlight more Safely and steadly work.
It referring to Figure 1, is that a kind of operative scenario of aircraft based on carry searchlight 101 of the embodiment of the present invention is shown It is intended to, user passes through aircraft described in remote controler wireless remote control.Searchlight 101 can be with carry in aircraft in one embodiment Top, can be arranged in aircraft body by way of rotation connection, in this way can according to need adjustment searchlight Light emission direction, to realize searchlighting function.Certainly, searchlight 101 can be with carry in the side or bottom of aircraft.In a reality It applies in example, on the one hand aircraft flight can control by remote controler, on the other hand can also be used to manually control as needed Searchlight 101.The scene includes a flight system, which includes aircraft, carry in the carry-on spy Illuminator, control device and user terminal;The control device is connected with the searchlight, and the control device can also be with It is connected with the user terminal.The control device is mainly used for executing the light emitting control to searchlight.In one embodiment, The control device is arranged on the aircraft, as shown in Figure 1, the aircraft includes aircraft body part, specifically Including rotor arm, propeller, undercarriage, and the various electric devices inside aircraft body are set, such as flight control Device, compass etc..Searchlight and control device are further comprised on the aircraft, the searchlight carry is in the flight In device main body, the control device is connected with the searchlight.In some other embodiment, the control device can also be set It sets on the user terminal namely the user terminal is by installing corresponding application program, realize being used for for control device Execute the function to the light emitting control of searchlight.
The aircraft can be automatic flight, and user can pass through remote controler or smart phone, tablet computer, intelligence Cruise route is arranged in the intelligent terminals such as wearable device, and sends control instruction to aircraft, and the aircraft can be according to this Control instruction executes the cruise route, flies in the cruise route.At this point, user can also be arranged in cruise route The working strategies of searchlight 101, by carry-on controller (such as flight controller or be separately provided one control that shines Device processed) or the control device 102 of the compositions such as controller on searchlight 101 control searchlight 101 according to the working strategies work Make.In one embodiment, which may include: and works on one section of cruise route or multistage course line in height Under Brightness Duty state;On cruise route other one section or multistage course lines, work is (or normal in low-light level working condition Brightness Duty state) under.The brightness value required under low-light level working condition is bright lower than requiring under the high brightness working condition Angle value.Certainly, in other embodiments, more Brightness Duty states can also be set, such as in brightness value in low-light level work Make the intermediate light working condition etc. between brightness value required by state and high brightness working condition.
The embodiment of the present invention can carry out such as above-mentioned automatic control to the searchlight 101, can also carry out manually Control.User increases the brightness of searchlight 101 when required by the mode manually adjusted, it is above-mentioned refer to can be to searchlight 101 control devices 102 controlled can be warm based on the first current work of the searchlight 101 that temperature sensor senses Degree, and/or the remaining battery power powered to searchlight 101, calculating searchlight 101 can be corresponding to the high brightness working condition Brightness value under the first maximum functional duration for working, and reminded by a prompt information to user.User believes according to prompt The first maximum functional duration in breath can according to need selection and open high brightness mode, searchlight 101 is made to be in high brightness work Make under state.After working under searchlight 101 is in high brightness working condition, control device 102 can carry out Intelligent treatment, with Convenient for automatically turning down the brightness of searchlight 101 when needed, guarantee the safe and stable operation of searchlight 101.
Fig. 2 is referred to, is a kind of flow diagram of the light-emitting control method of searchlight of the embodiment of the present invention, the present invention The method of embodiment can be applied on control device.The control device for example can be the dress of setting on board the aircraft It sets, such as the flight controller of aircraft.Aircraft is controlled by the controlling terminal of user, and the control of the control device and user are whole It can wirelessly be connected between end.The control device be also possible to one be exclusively used in controlling searchlight set It is standby, the control device at this time can directly wirelessly be established with the controlling terminal of user connection or one end with The associated components (such as communication interface) of aircraft carry out wired connection, whole by the communication interface of aircraft and the control of user Connection is established at end, and the other end and searchlight are electrically connected.The control device is also possible to be arranged in a control on searchlight The flight controller of device, one end of the control device at this time and aircraft carries out wired connection, by flight controller with The controlling terminal of user establishes connection, and the other end and searchlight are electrically connected.
During aircraft flight, the control device can in real time or periodically detect in S201 The working condition for the searchlight being arranged on aircraft;In embodiments of the present invention, it based on the light emission luminance of searchlight, can will visit The working condition of illuminator divides into high brightness working condition and low-light level working condition, refers in high brightness working condition: institute The light emission luminance for stating searchlight work is higher than preset first luminance threshold, and if the light emission luminance of searchlight work is lower than pre- If the first luminance threshold or searchlight work light emission luminance be lower than preset second luminance threshold, it may be considered that searchlighting Lamp is in low-light level working condition, wherein second luminance threshold is lower than first luminance threshold.In addition, described first Luminance threshold is to be arranged according to the nominal operation brightness of the searchlight, such as the first highlighted threshold value can be set as volume Determine operating brightness or nominal operation brightness 120%, even more greatly.In the flight course of aircraft, control device can be examined It surveys and whether receives high brightness control instruction, if receiving high brightness control instruction, trigger the searchlight and enter high brightness Working condition meets the highlight illumination demand of user with this.High brightness control instruction can be the control of user terminal sending Brightness control instruction processed, be also possible to it is for example above-mentioned refer to according in the automatic flight course of cruise route, according to working strategies The brightness control instruction automatically generated.
It, can be with before the working condition for the searchlight that detection is arranged on board the aircraft in addition, in one embodiment Obtain the current state of flight of aircraft.If being in the first state of flight, control searchlight work is in low-light level working condition, work Work refers under low-light level working condition: the light emission luminance of the searchlight is lower than preset second luminance threshold;If in the Two state of flights, the work of control searchlight refer under normal brightness working condition in normal brightness working condition, work: described The light emission luminance of searchlight is nominal operation brightness.Aircraft is in the first state of flight, can't trigger and visit on aircraft The detection of the working condition of illuminator, because at this point, in order to avoid being made when aircraft just takes off not far to the eyes of control user At stimulation, searchlight can be arranged under low-light level working condition work in embodiments of the present invention, because high brightness may be made At the momentary blindness of user, eyes are damaged, therefore, in embodiments of the present invention, if the aircraft is in first State of flight then controls the searchlight work under low-light level working condition.In one embodiment, second luminance threshold Value is less than or equal to the nominal operation brightness, and the nominal operation brightness is less than or equal to above-mentioned the first luminance threshold referred to Value.
Aircraft, which is in the first state of flight, to be referred to: the flying height that flight parameter includes is high lower than preset flight Threshold value is spent, and/or, the distance between the aircraft that flight parameter includes and controlling terminal are less than preset distance threshold. And aircraft is in the second state of flight and refers to: the flying height that flight parameter includes is greater than or equal to preset flying height threshold Value, and/or, the distance between the aircraft that flight parameter includes and controlling terminal are more than or equal to preset apart from threshold Value.The controlling terminal can refer to controlling terminal relevant to aircraft, such as the control for controlling the aircraft flight Terminal processed etc..Such as if it is less than 10m, (10m is empirical value to flying height represented by the flight parameter of aircraft, adjustable It is whole) and/or flight parameter represented by flying distance be less than 10m (10m empirical value, can adjust), then automatically with the second luminance threshold Value (such as work normally brightness value 30%) and its brightness below control searchlight shine.Searchlight can be both made in this way Can normal use prompt, also avoid damaging eyes of user.
Further, in one embodiment, if aircraft is in the second state of flight, it can control searchlight work Make in normal brightness working condition, work refers under normal brightness working condition: the light emission luminance of the searchlight is specified Operating brightness.Under normal circumstances, a nominal operation brightness, under the second state of flight, searchlight can be arranged in lamps and lanterns Brightness may can't bring adverse effect to the eyes of user, for example, flying height represented by the flight parameter of aircraft It is greater than 10m (10m experience if it is greater than flying distance represented by 10m (10m is empirical value, be can adjust) and/or flight parameter Value can adjust), then it is shone automatically with nominal operation brightness control searchlight.
After the working condition of searchlight has been determined, control device is height in the working condition of the searchlight in S202 When Brightness Duty state, the first job information of the searchlight is obtained.It is such as above-mentioned during aircraft flight, it is possible to Working strategies based on pre-set searchlight work under being manually adjusted by user to the brightness for being higher than the first luminance threshold, Searchlight is in high brightness working condition at this time, needs to obtain in real time or obtains the searchlighting in shorter period periodically First job information of lamp.In embodiments of the present invention, first job information include operating time, the first operating temperature, In battery capacity any one or it is multiple.Wherein, battery capacity refers to the electricity of the battery to searchlight power supply, to searchlighting The battery of lamp power supply can be the battery of the aircraft, or an individual supplying cell.In one embodiment, The working condition of searchlight can be operated according to the control to searchlight to judge, such as is being received in control interface Searchlight is adjusted to the user's operation of high brightness working condition, in another example detecting searchlight through physical buttons such as knobs Brightness adjustment to maximum value user's operation.The working condition of searchlight can also determine according to current brightness, such as Determine that the brightness of searchlight is higher than nominal brightness threshold value (or first luminance threshold) and then thinks searchlight within the scope of certain time Work determines that the brightness of searchlight is equal to nominal brightness threshold value and then thinks under high brightness working condition within the scope of certain time Searchlight works in normal operation, determines that the brightness of searchlight is lower than nominal brightness threshold value within the scope of certain time (or second luminance threshold) then thinks searchlight work under low-light level working condition.
After getting the first job information of searchlight, control device judges the first job information, control dress It sets in S203, if the first job information meets preset control condition, the searchlight is worked as according to predetermined luminance value The light emission luminance of preceding work is adjusted;The predetermined luminance value is lower than first luminance threshold, the preset brightness value It can be nominal operation brightness or a brightness value lower than nominal operation brightness, the first luminance threshold can be nominal operation Brightness or a brightness value greater than nominal operation brightness.The control condition is to keep searchlight safe and stable Work and be arranged, if meeting control condition, need to control the working condition of searchlight, avoid the occurrence of safe thing Therefore.
In one embodiment, first job information for obtaining the searchlight may include: to obtain the searchlighting Lamp has been in the operating time under the high brightness working condition, and the control condition indicates the first duration threshold value, described It includes: that the operating time is greater than or equal to the first duration threshold value that first job information, which meets preset control condition,.It should First duration threshold value indicated by control condition can be an empirical value, which can be in actual flight And using during searchlight, determined by multiple actual measurement durations of the multiple searchlight of record, when multiple actual measurements Length refers to searchlight at varying environment temperature and/or operating temperature, works under high brightness working condition and operating temperature is rigid Reach the duration of some warning temperature threshold well.Warning temperature threshold is mainly based upon the emergency lighting of searchlight because usually determining , operating temperature is that the searchlight of warning temperature threshold is possible to damage, or even causes to explode because temperature is excessively high, Need to be arranged warning temperature threshold to guarantee the safe operation of searchlight.
In one embodiment, the first duration threshold value can also the first maximum functional duration based on searchlight come really Fixed.It can be evaluated whether first maximum functional duration of the searchlight under the high brightness working condition;First duration Threshold value is set according to the first maximum functional duration, for example, the first maximum functional duration is set as the first duration threshold Value, or a duration less than the first maximum functional duration is set as the first duration threshold value.When the first maximum functional It is long to can be when just taking off, or any one moment before controlling the searchlight and entering high brightness working condition calculate It arrives.And the first maximum functional duration be operating temperature according to the searchlight under the high brightness working condition or Person enters operating temperature when highlighting working condition to estimate.In certain embodiments, when estimating the first maximum functional duration The operating temperature under the high brightness working condition being based on is also a reference value, not in this task in high brightness Measured value under working condition estimates a rough first maximum functional duration based on the reference value, is based on the maximum work The first duration threshold value in control condition is set as duration.In certain embodiments, which can also be with It is a pre-set steady state value.
In one embodiment, first job information for obtaining the searchlight also may include: to obtain the spy First operating temperature of the illuminator under the high brightness working condition;The control condition indicates the first temperature threshold, described It includes: that first operating temperature is greater than or equal to the first temperature threshold that first job information, which meets preset control condition,.It should First temperature threshold can be related to the above-mentioned warning temperature threshold referred to, in one embodiment, first temperature threshold Value can be the absolute of the difference between the warning temperature threshold or first temperature threshold and the warning temperature threshold Value is less than preset numerical value.First temperature threshold alert in other words temperature threshold be according to the operating temperature ratings of searchlight come Determining.Searchlight can be acquired in high brightness working condition by the way that temperature sensor is arranged at the lamp holder position of searchlight Under temperature.
And if detecting that the first operating temperature of the searchlight is greater than preset warning temperature threshold, issues high temperature Warning prompt.Once reaching the warning temperature threshold, then need to issue the user with prompting message, it in one embodiment, can be with It is reminded by way of controlling carry-on other lamps flashing, it in one embodiment, can also be by communication link On the mode that sends a notification message user is notified in controlling terminal.The effect that the warning temperature threshold is arranged is: upper It is long at work to be less than the first duration indicated by the control condition in the case that the first job information stated is operating time When threshold value, it if the first operating temperature has been more than the warning temperature threshold, can also give a warning, can grow at work in this way When being unsatisfactory for control condition, also user temperature can be reminded excessively high, in order to which user executes corresponding security control, such as turned down Brightness even switches off searchlight.The effect that the warning temperature threshold is arranged also resides in: though the searchlight do not enter into it is highlighted Working condition is spent, but if detecting that operating temperature is higher than the warning temperature threshold, similarly may remind the user that work temperature Height is spent, in order to which user executes corresponding security control, such as brightness is turned down and even switches off searchlight.
In one embodiment, referring to FIG. 3, be in the embodiment of the present invention according to predetermined luminance value to the searchlight After the light emission luminance of work at present is adjusted, that is, after the light emission luminance for turning down searchlight, issue the side of brightness adjustment instruction Method schematic diagram, in embodiments of the present invention, control device obtain the searchlight after carrying out light emission luminance adjustment in S301 The second job information, and issue brightness if second job information meets high brightness operating condition in S302 Adjustment instruction.
In one embodiment, the S301 may include obtaining the searchlight to carry out light emission luminance adjusted the Two operating temperatures;It again may be by being arranged in the temperature sensor at lamp holder of searchlight to obtain the second current work of searchlight Make temperature, under normal circumstances, after turning down brightness, the operating temperature of searchlight can be reduced.Control device can estimate the searchlighting The second maximum functional duration that lamp works under the second operating temperature and under the high brightness working condition;It can be based on pre- The appraising model being first arranged is input with the second operating temperature, calculates the second maximum functional duration of output.Control device is second Maximum functional duration is greater than preset second duration threshold value, then issues brightness adjustment instruction.That is, estimating second obtained Maximum functional duration is greater than preset second duration threshold value, such as the second duration threshold value such as 2 minutes, 5 minutes, then notifies user can To allow searchlight to be in high brightness working condition again.Preset second duration threshold value is mainly user previously according to being executed Searchlighting task be arranged, for example, control aircraft flies a circle around this equipment when mining site user needs to observe certain equipment And to the equipment checked when it is 2 minutes a length of, then, the second duration threshold value is arranged to two minutes, any moment, as long as estimating Calculating searchlight can work two minutes under high brightness working condition, then can issue brightness adjustment instruction.
In other embodiments, temperature and operating time can also be respectively based on to determine whether to issue brightness adjustment and refer to Show.The available searchlight is carrying out light emission luminance the second operating temperature adjusted, and the high brightness works item Part indicates second temperature threshold value, and it includes: second operating temperature that second job information, which meets high brightness operating condition, Less than or equal to the second temperature threshold value.Alternatively, can also estimate that the searchlight, can after carrying out light emission luminance adjustment The the second maximum functional duration to work under high brightness working condition, second duration information meet high brightness operating condition packet Include: the second maximum functional duration is greater than or equal to the second duration threshold value.
In embodiments of the present invention, brightness adjustment instruction be used to indicate issue the user with the searchlight can be in height The prompting message to work under Brightness Duty state;And/or the brightness adjustment instruction is highlighted for controlling the searchlight entrance Spend working condition.That is, brightness adjustment instruction can be only a prompting message, by communication link to user Terminal issues the prompt that can be worked with high brightness working condition.The brightness adjustment instruction is also possible to as a control instruction It directly controls under searchlight work to high brightness working condition.Or the effect of the brightness adjustment instruction is: issuing prompt After message, if not receiving the instruction for stopping high brightness work of user, searchlight work is directly controlled to high brightness work Make under state.
Other function attachment can also be arranged other than searchlight can be set in the aircraft, in one embodiment, Night flight lamp is also provided on the aircraft.In the embodiment of the present invention, the function of night flight lamp is mainly used in night or light It, can be to the skyborne position of aircraft in the environment of darker (light intensity of light sensor sensing is lower than preset threshold value) It sets and is positioned and prompted, can be under some emergency cases, such as searchlight cannot shine (such as searchlight failure) Situations such as, it can effectively prompt the user with the skyborne position of aircraft.In one embodiment, night flight lamp is carried out luminous The purpose of control, mainly meeting above can be to control user or other flight in 3 miles/5 kilometers even farther distances Device or other associated users prompt the skyborne position of aircraft.
Detect that the flight parameter of the aircraft meets night flight lamp control if carrying out light emitting control to night flight lamp and specifically including that Condition processed controls the night flight lamp work under low brightness levels then according to the first night flight lamp prompt rules;Alternatively, if detection Flight parameter to the aircraft is unsatisfactory for night flight lamp control condition, then according to the second night flight lamp prompt rules, described in control Night flight lamp works under high brightness level.The flight parameter includes the flying height and/or the flight of the aircraft The flying distance of controlling terminal during device execution aerial mission apart from terrestrial user.Detect the flight ginseng of the aircraft Number whether meet night flight lamp control condition include: detect the aircraft flying height whether less than the first height threshold with/ Or whether the flying distance of the detection aircraft is less than preset first distance threshold value.If it is judged that being yes, then it is assumed that The flight parameter of the aircraft meets night flight lamp control condition.And if it is judged that the flying height of the aircraft whether Whether the flying distance greater than the first height threshold and/or the detection aircraft is greater than preset first distance threshold value, then recognizes Night flight lamp control condition is unsatisfactory for for the flight parameter of the aircraft.First height threshold for example can be the warp such as 4.5m Value is tested, the first distance threshold value is for example also possible to the empirical values such as 4.5m.
Second luminance threshold indicated by the low brightness levels is less than the first brightness indicated by the high brightness level Threshold value.Second luminance threshold for example can be 30% equal empirical values of night flight lamp brightness, and high brightness level for example can be night flight 100% preset value of lamp brightness.First height threshold and/or first distance threshold value be set, and the first luminance threshold of setting and Second luminance threshold is as the purpose of the light emitting control foundation of night flight lamp: on the one hand, low latitude or apart from user it is closer In the case where, will not the eyes of user be caused with stimulation, interference, the vision of user is will not influence, user can be guaranteed to flight Device carries out security control, on the other hand, after aircraft flies far, can also reach aircraft and prompt aircraft under night flight mode The function of position, such as reach during aircraft flies in the sky, it is even farther apart from upper, control at 3 miles/5 kilometers User processed or other aircraft or other associated users are also it can be found that the presence of the aircraft.
The embodiment of the present invention is illustrated with an example below.
When taking off at night, user can select to open on night flight lamp on APP unmanned plane, and after selection is opened, control is visited Illuminator with compared with low-light level (within 30%, user is adjustable) (can using searchlight working condition at this time as low-light level work shape State) it shines, searchlight is controlled when more than user 8m (user is adjustable) with 100% Intensity LEDs, 100% brightness is The nominal operation brightness (can be using searchlight working condition at this time as normal operating conditions) of the searchlight.User at this time Searchlight, and unrestricted random adjustment in 0%~100% brightness section can be used according to self-demand.
User when needing the interim light emission luminance for promoting searchlight, can in a short time hand hoisting it is bright to 100% Degree, at this point, unmanned plane searchlight can calculate that searchlight can work under 120% brightness according to factors such as environment temperatures the One maximum functional duration, and be pushed to user, user can be used that work under 120% brightness (can within this period Using by searchlight working condition at this time as high brightness working condition).If user's control searchlight work under 120% brightness Make, (is greater than or equal to the then after detecting that operating time in the first job information reaches the first maximum functional duration One duration threshold value), searchlight can drop back to 100% Brightness Duty of highest automatically, and reappraise the second work after turning down brightness Information, i.e. the second operating temperature and the second maximum functional duration.Meet the certain time that works under 120% brightness to own temperature After the condition of (user can choose), user can select control searchlight to shine under 120% brightness again.For example, at least exist Work 1min or the certain time that at least works (such as aforementioned the first maximum functional duration referred to or when first under 120% brightness Long threshold value) and/or lamp bead temperature at a temperature of certain environment be lower than certain temperature such as second temperature threshold value.
Meanwhile when unmanned plane searchlighting lamp module detects that own temperature is excessively high, related letter actively can be pushed to unmanned plane Breath, user terminal also will receive corresponding warning, and user can reduce brightness or according to systemic presupposition by nobody according to prompt at this time Machine searchlight independently reduces brightness.
For night flight lamp, when taking off at night, user can select to open on night flight lamp on APP unmanned plane, and selection is opened Qi Hou can control night flight lamp to flash compared with low-light level (10%), to indicate that night flight lamp flashing function has turned on;User's operation nobody Machine takes off, and in takeoff phase, night flight lamp can be always to flash compared with low-light level (10% brightness, user are adjustable);Night flight lamp is flying More than highly 4.5 (user is adjustable) rice, night flight lamp is controlled with intermediate light (such as 30% brightness, user are adjustable) flashing;Away from When from the ground or apart from user 50m (user is adjustable) or more, night flight lamp is controlled with full brightness (100% brightness) flashing.? During this, night flight lamp can actively obtain the flying height of unmanned plane and/or the distance apart from user, and autonomous automatic choosing Select corresponding brightness and flicker frequency.Unmanned plane is carried out when landing at night also based on the above-mentioned flying height referred to and brightness The light emitting control of night flight lamp.
Using in the embodiment of the present invention, searchlight function can be not only realized on board the aircraft, additionally it is possible to be automated, intelligence Change the safe handling that ground guarantees searchlight, the flight safety of the aircraft also guaranteed.
Fig. 4 is referred to again, is a kind of structural schematic diagram of the emission control device of searchlight of the embodiment of the present invention, this hair The emission control device of the searchlight of bright embodiment can be set in an individual control device, also can be set In the flight controller of aircraft.The control device includes following module.
Obtain module 401, for the working condition in the searchlight be high brightness working condition when, obtain the searchlighting First job information of lamp, refers in high brightness working condition: the light emission luminance of the searchlight work at present is higher than default The first luminance threshold;Processing module 402, if meeting preset control condition for the first job information, according to default Brightness value is adjusted the light emission luminance of the searchlight work at present;The predetermined luminance value is lower than first luminance threshold Value.
In one embodiment, described device can also include: detection module 403, for detecting whether receiving highlighted Spend control instruction;If receiving high brightness control instruction, triggers the searchlight and enter high brightness working condition.
In one embodiment, preset first luminance threshold is set according to the nominal operation brightness of the searchlight It sets.
In one embodiment, the acquisition module 401 is used for when obtaining the first job information of the searchlight Obtain the operating time that the searchlight has been under the high brightness working condition;First job information meets default Control condition include: the operating time be greater than or equal to the first duration threshold value.
In one embodiment, the acquisition module 401 is used for when obtaining the first job information of the searchlight Obtain first operating temperature of the searchlight under the high brightness working condition;First job information meets preset Control condition includes: that first operating temperature is greater than or equal to first temperature threshold.
In one embodiment, described device can also include: estimation block 404, for estimating the searchlight in institute State the first maximum functional duration under high brightness working condition;Wherein, the first duration threshold value is maximum according to described first Operating time setting.
In one embodiment, the first maximum functional duration is according to the searchlight in high brightness work shape Operating temperature under state or operating temperature when entering highlighted working condition are estimated.
In one embodiment, the acquisition module 401, is adjusted to the light emission luminance of the searchlight work at present After whole, it is also used to obtain the searchlight and is carrying out light emission luminance the second job information adjusted;If second work Information meets high brightness operating condition, then issues brightness adjustment instruction.
In one embodiment, the acquisition module 401 is carrying out light emission luminance adjustment for obtaining the searchlight When rear the second job information, light emission luminance the second operating temperature adjusted is being carried out for obtaining the searchlight;It is described It includes: that second operating temperature is less than or equal to second temperature threshold value that second job information, which meets high brightness operating condition,.
In one embodiment, the acquisition module 401 is carrying out light emission luminance adjustment for obtaining the searchlight When rear the second job information, for estimating that the searchlight after carrying out light emission luminance adjustment, can work shape in high brightness The the second maximum functional duration to work under state;It includes: described second most that second duration information, which meets high brightness operating condition, Big operating time is greater than or equal to the second duration threshold value.
In one embodiment, brightness adjustment instruction be used to indicate issue the user with the searchlight can be highlighted The prompting message to work under degree working condition;And/or the brightness adjustment instruction enters high brightness for controlling the searchlight Working condition.
In one embodiment, described device can also include: alarm module 405, if for detecting the searchlighting First operating temperature of lamp is greater than preset warning temperature threshold, issues high temperature warning prompt.
In one embodiment, the acquisition module 401, is also used to obtain the current state of flight of aircraft;The place Module 402 is managed, if being also used in the first state of flight, the work of control searchlight works in low-light level working condition low bright Refer under degree working condition: the light emission luminance of the searchlight is lower than preset second luminance threshold;If being in the second flight shape State, the work of control searchlight refer under normal brightness working condition in normal brightness working condition, work: the searchlight Light emission luminance is nominal operation brightness.
In one embodiment, refer in the first state of flight: the flying height that flight parameter includes is lower than preset Flying height threshold value, and/or, the distance between the aircraft that flight parameter includes and controlling terminal are less than preset distance Threshold value;Refer in the second state of flight: the flying height that flight parameter includes is greater than or equal to preset flying height threshold value, And/or the distance between the flight parameter aircraft that includes and controlling terminal are greater than or equal to preset distance threshold.
In one embodiment, second luminance threshold is less than or equal to the nominal operation brightness, the specified work Make brightness less than or equal to first luminance threshold.
Using in the embodiment of the present invention, searchlight function can be not only realized on board the aircraft, additionally it is possible to be automated, intelligence Change the safe handling that ground guarantees searchlight, the flight safety of the aircraft also guaranteed.
Fig. 5 is referred to again, is a kind of structural schematic diagram of control device of the embodiment of the present invention, which includes: Memory 501 and processor 502.Further, which can also include power supply, communication interface etc. as needed Module.
The memory 501 may include volatile memory (volatile memory), such as random access memory (random-access memory, RAM);Memory 501 also may include nonvolatile memory (non-volatile Memory), such as flash memory (flash memory), solid state hard disk (solid-state drive, SSD) etc.;Memory 501 can also include the combination of the memory of mentioned kind.
The processor 502 can be central processing unit (central processing unit, CPU).The processor 502 can further include hardware chip.Above-mentioned hardware chip can be specific integrated circuit (application- Specific integrated circuit, ASIC), programmable logic device (programmable logic device, PLD) etc..In one embodiment, above-mentioned PLD can be field programmable gate array (field-programmable Gate array, FPGA), Universal Array Logic (generic array logic, GAL) etc..
The memory 501 is also used to store program instruction.The processor 502 can call described program to instruct, real The now method as involved in the above embodiments of the present application.It is stated about being described in detail below for processor 502.
In one embodiment, the processor 502, calls the program instruction stored in the memory, for executing Following steps:
When the working condition of the searchlight is high brightness working condition, the first work letter of the searchlight is obtained Breath, refers in high brightness working condition: the light emission luminance of the searchlight work at present is higher than preset first luminance threshold; If the first job information meets preset control condition, shone according to predetermined luminance value to the searchlight work at present Brightness is adjusted;The predetermined luminance value is lower than first luminance threshold.
In one embodiment, the processor 502, is also used to execute following steps:
It detects whether to receive high brightness control instruction;If receiving high brightness control instruction, the searchlight is triggered Into high brightness working condition.
In one embodiment, preset first luminance threshold is set according to the nominal operation brightness of the searchlight It sets.
In one embodiment, the processor 502, for executing following steps:
Obtain the operating time that the searchlight has been under the high brightness working condition;First job information Meeting preset control condition includes: that the operating time is greater than or equal to the first duration threshold value.
In one embodiment, the processor 502, for executing following steps:
Obtain first operating temperature of the searchlight under the high brightness working condition;First job information is full The preset control condition of foot includes: that first operating temperature is greater than or equal to the first temperature threshold.
In one embodiment, the processor 502, is also used to execute following steps:
Estimate first maximum functional duration of the searchlight under the high brightness working condition;Wherein, described first Duration threshold value is set according to the first maximum functional duration.
In one embodiment, the first maximum functional duration is according to the searchlight in high brightness work shape Operating temperature under state or operating temperature when entering high brightness working condition are estimated.
In one embodiment, the processor 502, is also used to execute following steps:
It obtains the searchlight and is carrying out light emission luminance the second job information adjusted;If second job information Meet high brightness operating condition, then issues brightness adjustment instruction.
In one embodiment, the processor 502, is also used to execute following steps:
It obtains the searchlight and is carrying out light emission luminance the second operating temperature adjusted;Second job information meets High brightness operating condition includes: that second operating temperature is less than or equal to the second temperature threshold value.
In one embodiment, the processor 502, for executing following steps:
The searchlight is estimated after carrying out light emission luminance adjustment, can work under high brightness working condition second is most Big operating time;Second job information meet high brightness operating condition include: the second maximum functional duration be greater than or Equal to the second duration threshold value.
In one embodiment, brightness adjustment instruction be used to indicate issue the user with the searchlight can be highlighted The prompting message to work under degree working condition;And/or the brightness adjustment instruction enters high brightness for controlling the searchlight Working condition.
In one embodiment, the processor 502, is also used to execute following steps:
If detecting that the first operating temperature of the searchlight is greater than preset warning temperature threshold, high temperature warning is issued Prompt.
In one embodiment, the processor 502, is also used to execute following steps:
Obtain the current state of flight of aircraft;If being in the first state of flight, control searchlight work is in low-light level work Make state, work refers under low-light level working condition: the light emission luminance of the searchlight is lower than preset second luminance threshold; If being in the second state of flight, the work of control searchlight works under normal brightness working condition in normal brightness working condition Refer to: the light emission luminance of the searchlight is nominal operation brightness.
In one embodiment, refer in the first state of flight: the flying height that flight parameter includes is lower than preset Flying height threshold value, and/or, the distance between the aircraft that flight parameter includes and controlling terminal are less than preset distance Threshold value;Refer in the second state of flight: the flying height that flight parameter includes is greater than or equal to preset flying height threshold value, And/or the distance between the flight parameter aircraft that includes and controlling terminal are greater than or equal to preset distance threshold.
In one embodiment, second luminance threshold is less than or equal to the nominal operation brightness, the specified work Make brightness less than or equal to first luminance threshold.
In embodiments of the present invention, the specific implementation of the processor 502 can refer in previous embodiment and fill about control The description for the related content set, this will not be repeated here.Using in the embodiment of the present invention, searchlight can be not only realized on board the aircraft Function, additionally it is possible to automate, intelligently guarantee searchlight safe handling, the flight safety of the aircraft also guaranteed.
Those of ordinary skill in the art will appreciate that realizing all or part of the process in above-described embodiment method, being can be with Relevant hardware is instructed to complete by computer program, the program can be stored in a computer-readable storage medium In, the program is when being executed, it may include such as the process of the embodiment of above-mentioned each method.Wherein, the storage medium can be magnetic Dish, CD, read-only memory (Read-Only Memory, ROM) or random access memory (Random Access Memory, RAM) etc..
Above disclosed is only section Example of the present invention, cannot limit the right model of the present invention with this certainly It encloses, therefore equivalent changes made in accordance with the claims of the present invention, is still within the scope of the present invention.

Claims (34)

1. a kind of light-emitting control method of searchlight, which is characterized in that the searchlight is arranged on board the aircraft, the method packet It includes:
When the working condition of the searchlight is high brightness working condition, the first job information of the searchlight is obtained, is located Refer in high brightness working condition: the light emission luminance of the searchlight work at present is higher than preset first luminance threshold;
If the first job information meets preset control condition, according to predetermined luminance value to the searchlight work at present Light emission luminance is adjusted;
The predetermined luminance value is lower than first luminance threshold.
2. the method as described in claim 1, which is characterized in that further include:
It detects whether to receive high brightness control instruction;
If receiving high brightness control instruction, triggers the searchlight and enter high brightness working condition.
3. the method as described in claim 1, which is characterized in that preset first luminance threshold is according to the searchlight Nominal operation brightness setting.
4. the method as described in claim 1, which is characterized in that first job information for obtaining the searchlight, comprising:
Obtain the operating time that the searchlight has been under the high brightness working condition;
It includes: that the operating time is greater than or equal to the first duration threshold that first job information, which meets preset control condition, Value.
5. the method as described in claim 1, which is characterized in that first job information for obtaining the searchlight, comprising:
Obtain first operating temperature of the searchlight under the high brightness working condition;
It includes: that first operating temperature is greater than or equal to the first temperature that first job information, which meets preset control condition, Threshold value.
6. method as claimed in claim 4, which is characterized in that further include:
Estimate first maximum functional duration of the searchlight under the high brightness working condition;
Wherein, the first duration threshold value is set according to the first maximum functional duration.
7. method as claimed in claim 6, which is characterized in that the first maximum functional duration is existed according to the searchlight Operating temperature under the high brightness working condition or operating temperature when entering highlighted working condition are estimated.
8. the method as described in claim 1, which is characterized in that adjusted to the light emission luminance of the searchlight work at present After whole, the method also includes:
It obtains the searchlight and is carrying out light emission luminance the second job information adjusted;
If second job information meets high brightness operating condition, brightness adjustment instruction is issued.
9. method according to claim 8, which is characterized in that described to obtain the searchlight after carrying out light emission luminance adjustment The second job information, comprising:
It obtains the searchlight and is carrying out light emission luminance the second operating temperature adjusted;
It includes: that second operating temperature is less than or equal to second temperature that second job information, which meets high brightness operating condition, Threshold value.
10. method according to claim 8, which is characterized in that described to obtain the searchlight in progress light emission luminance adjustment The second job information afterwards, comprising:
The searchlight is estimated after carrying out light emission luminance adjustment, the maximum work of can work under high brightness working condition second Make duration;
It includes: that the second maximum functional duration is greater than or equal to second that second job information, which meets high brightness operating condition, Duration threshold value.
11. method according to claim 8, which is characterized in that the brightness adjustment instruction, which is used to indicate, issues the user with institute State the prompting message that searchlight can work under high brightness working condition;And/or the brightness adjustment instruction is for controlling It states searchlight and enters high brightness working condition.
12. such as the described in any item methods of claim 1-11, which is characterized in that further include:
If detecting that the first operating temperature of the searchlight is greater than preset warning temperature threshold, issues high temperature warning and mention Show.
13. the method according to claim 1 to 7, which is characterized in that further include:
Obtain the current state of flight of aircraft;
If being in the first state of flight, the work of control searchlight works under low-light level working condition in low-light level working condition Refer to: the light emission luminance of the searchlight is lower than preset second luminance threshold;
If being in the second state of flight, the work of control searchlight is in normal brightness working condition, and work is in normal brightness work shape Refer under state: the light emission luminance of the searchlight is nominal operation brightness.
14. method as claimed in claim 13, which is characterized in that refer in the first state of flight: what flight parameter included Flying height is lower than preset flying height threshold value, and/or, between the flight parameter aircraft for including and controlling terminal Distance is less than preset distance threshold;
Refer in the second state of flight: the flying height that flight parameter includes is greater than or equal to preset flying height threshold value, And/or the distance between the flight parameter aircraft that includes and controlling terminal are greater than or equal to preset distance threshold.
15. method as claimed in claim 13, which is characterized in that second luminance threshold is less than or equal to the specified work Make brightness, the nominal operation brightness is less than or equal to first luminance threshold.
16. a kind of emission control device of searchlight, which is characterized in that the searchlight is arranged on board the aircraft, described device Include:
Module is obtained, when for the working condition in the searchlight being high brightness working condition, obtains the of the searchlight One job information refers in high brightness working condition: the light emission luminance of the searchlight work at present is higher than preset first Luminance threshold;
Processing module, if meeting preset control condition for the first job information, according to predetermined luminance value to the spy The light emission luminance of illuminator work at present is adjusted;The predetermined luminance value is lower than first luminance threshold.
17. a kind of emission control device of searchlight, which is characterized in that the control on board the aircraft is arranged in the searchlight Device includes: memory and processor;
Program instruction is stored in the memory;
The processor calls the program instruction stored in the memory, for executing following steps:
When the working condition of the searchlight is high brightness working condition, the first job information of the searchlight is obtained, is located Refer in high brightness working condition: the light emission luminance of the searchlight work at present is higher than preset first luminance threshold;
If the first job information meets preset control condition, according to predetermined luminance value to the searchlight work at present Light emission luminance is adjusted;
The predetermined luminance value is lower than first luminance threshold.
18. control device as claimed in claim 17, which is characterized in that the processor is also used to execute following steps:
It detects whether to receive high brightness control instruction;
If receiving high brightness control instruction, triggers the searchlight and enter high brightness working condition.
19. control device as claimed in claim 17, which is characterized in that preset first luminance threshold is according to The nominal operation brightness setting of searchlight.
20. control device as claimed in claim 17, which is characterized in that the processor, for executing following steps:
Obtain the operating time that the searchlight has been under the high brightness working condition;
It includes: that the operating time is greater than or equal to the first duration threshold that first job information, which meets preset control condition, Value.
21. control device as claimed in claim 17, which is characterized in that the processor, for executing following steps:
Obtain first operating temperature of the searchlight under the high brightness working condition;
It includes: that first operating temperature is greater than or equal to the first temperature that first job information, which meets preset control condition, Threshold value.
22. such as the described in any item control devices of claim 17-21, which is characterized in that the processor is also used to execute such as Lower step:
Estimate first maximum functional duration of the searchlight under the high brightness working condition;
Wherein, the first duration threshold value is set according to the first maximum functional duration.
23. control device as claimed in claim 22, which is characterized in that the first maximum functional duration is according to the spy Operating temperature of the illuminator under the high brightness working condition or operating temperature when entering high brightness working condition are estimated 's.
24. control device as claimed in claim 17, which is characterized in that in the light emission luminance to the searchlight work at present After being adjusted, the processor is also used to execute following steps:
It obtains the searchlight and is carrying out light emission luminance the second job information adjusted;
If second job information meets high brightness operating condition, brightness adjustment instruction is issued.
25. control device as claimed in claim 24, which is characterized in that the processor is also used to execute following steps:
It obtains the searchlight and is carrying out light emission luminance the second operating temperature adjusted;
It includes: that second operating temperature is less than or equal to described second that second job information, which meets high brightness operating condition, Temperature threshold.
26. control device as claimed in claim 24, which is characterized in that the processor, for executing following steps:
The searchlight is estimated after carrying out light emission luminance adjustment, the maximum work of can work under high brightness working condition second Make duration;
It includes: that the second maximum functional duration is greater than or equal to second that second job information, which meets high brightness operating condition, Duration threshold value.
27. control device as claimed in claim 24, which is characterized in that the brightness adjustment instruction, which is used to indicate to user, to be sent out The prompting message that the searchlight can work under high brightness working condition out;And/or the brightness adjustment instruction is for controlling It makes the searchlight and enters high brightness working condition.
28. such as the described in any item control devices of claim 17-27, which is characterized in that the processor is also used to execute such as Lower step:
If detecting that the first operating temperature of the searchlight is greater than preset warning temperature threshold, issues high temperature warning and mention Show.
29. such as the described in any item control devices of claim 17-23, which is characterized in that the processor is also used to execute such as Lower step:
Obtain the current state of flight of aircraft;
If being in the first state of flight, the work of control searchlight is in low-light level working condition in low-light level working condition, work Refer to: the light emission luminance of the searchlight is lower than preset second luminance threshold;
If being in the second state of flight, the work of control searchlight is in normal brightness working condition, and work is in normal brightness work shape State refers to: the light emission luminance of the searchlight is nominal operation brightness.
30. control device as claimed in claim 29, which is characterized in that refer in the first state of flight: flight parameter packet The flying height included is lower than preset flying height threshold value, and/or, the aircraft that flight parameter includes and controlling terminal it Between distance be less than preset distance threshold;
Refer in the second state of flight: the flying height that flight parameter includes is greater than or equal to preset flying height threshold value, And/or the distance between the flight parameter aircraft that includes and controlling terminal are greater than or equal to preset distance threshold.
31. control device as claimed in claim 29, which is characterized in that second luminance threshold is less than or equal to the volume Determine operating brightness, the nominal operation brightness is less than or equal to first luminance threshold.
32. a kind of aircraft, which is characterized in that the aircraft includes: aircraft body, searchlight and control device, institute Searchlight carry is stated in the aircraft body, the control device is connected with the searchlight, and the control device is used for Execute the light-emitting control method such as the described in any item searchlights of claim 1-15.
33. a kind of flight system, which is characterized in that the flight system includes: aircraft, carry in the carry-on spy Illuminator, control device and user terminal;The control device is connected with the searchlight, and the control device with it is described User terminal is connected, and the control device is used to execute the light emitting control side such as the described in any item searchlights of claim 1-15 Method.
34. flight system as claimed in claim 33, which is characterized in that the control device is arranged on the aircraft, Alternatively, the control device is arranged on the user terminal.
CN201880010549.5A 2018-07-23 2018-07-23 Searchlight control method and device, searchlight control device, aircraft and flight system Expired - Fee Related CN110291012B (en)

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