CN103888591A - Method and system for managing wireless communication device under flight condition - Google Patents
Method and system for managing wireless communication device under flight condition Download PDFInfo
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- CN103888591A CN103888591A CN201210559879.4A CN201210559879A CN103888591A CN 103888591 A CN103888591 A CN 103888591A CN 201210559879 A CN201210559879 A CN 201210559879A CN 103888591 A CN103888591 A CN 103888591A
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Abstract
The invention provides a method and system for managing a wireless communication device under a flight condition. The system comprises: a reading module used for reading the accelerated speed, detected by an acceleration sensor of a wireless communication device, of the wireless communication device in real time; a starting module used for starting an air pressure detection gauge for detecting the air pressure in an airplane cabin when the read accelerated speed of the wireless communication device surpasses a first preset value; a judgment module used for judging whether the accelerated speed of the wireless communication device surpasses a second preset value and judging whether the pressure in the airplane cabin changes quickly and remains above a preset air pressure value stably; and a closing module used for closing the wireless communication function of the wireless communication device. With the method and system, passengers are reminded to open or close the communication function of the wireless communication devices in time when an airplane takes off or is landed, thereby guaranteeing air safety of the airplane more effectively.
Description
Technical field
The present invention relates to a kind of wireless telecommunications system management method and system, relate in particular to wireless telecommunications system management method and system under a kind of state of flight.
Background technology
When carrying out communication, wireless telecommunications system need to account for certain frequency spectrum resource, if the wireless navigation frequency range of aircraft has other wireless signal to exist, just likely affect the normal flight of aircraft, consequence is hardly imaginable, therefore, and before taking off, crew member can reminding passengers shut down the wireless telecommunications system of carrying, but still exist passenger not listen advice, or inadvertent forgets the situation of shutdown, this impacts the normal flight of giving aircraft.
Summary of the invention
In view of above content, be necessary to provide wireless telecommunications system management method and system under a kind of state of flight.
Under described state of flight, wireless telecommunications system management method comprises: read step, reads the acceleration of the wireless telecommunications system that the acceleration transducer of wireless telecommunications system detects in real time; Open step, in the time that the acceleration of the wireless telecommunications system reading exceedes the first preset value, the air pressure of open wireless communication apparatus detects meter and detects aircraft cabin internal gas pressure; The first determining step, judges whether the acceleration of wireless telecommunications system exceedes the second preset value, in the time that the acceleration of wireless telecommunications system exceedes the second preset value, enters the second determining step; The second determining step, more than judging whether aircraft cabin internal gas pressure changes fast and be stabilized in default atmospheric pressure value, when aircraft cabin internal gas pressure changes fast and is stabilized in default atmospheric pressure value when above, enters and closes step; Close step, close the wireless communication function of wireless telecommunications system.
Under described state of flight, wireless telecommunications system management system comprises: read module, for reading in real time the acceleration of the wireless telecommunications system that the acceleration transducer of wireless telecommunications system detects; Opening module, while exceeding the first preset value for the acceleration when the wireless telecommunications system reading, the air pressure of open wireless communication apparatus detects meter and detects aircraft cabin internal gas pressure; Whether judge module, exceed the second preset value for the acceleration that judges wireless telecommunications system; Described judge module, also in the time that the acceleration of wireless telecommunications system exceedes the second preset value, more than continuing to judge whether aircraft cabin internal gas pressure changes fast and be stabilized in default atmospheric pressure value; Closing module, for changing fast and be stabilized in default atmospheric pressure value and close when above the wireless communication function of wireless telecommunications system when aircraft cabin internal gas pressure.
Pressure when the present invention takes off by detecting or lands in acceleration and the aircraft cabin of wireless telecommunications system, while making take off or land, the wireless communication function of wireless telecommunications system is closed or opened to timely reminding passengers, more effectively ensured Flight Safety.
Accompanying drawing explanation
Fig. 1 is the running environment figure of the preferred embodiments of wireless telecommunications system management system under state of flight of the present invention.
Fig. 2 is the functional block diagram of the preferred embodiments of wireless telecommunications system management system under state of flight of the present invention.
Fig. 3 is the flow chart of the preferred embodiments of wireless telecommunications system management method under state of flight of the present invention.
Main element symbol description
| Wireless telecommunications system | 1 |
| Wireless telecommunications system management system under state of |
10 |
| |
12 |
| |
14 |
| |
16 |
| Air |
18 |
| Read module | 100 |
| Opening module | 101 |
| Judge module | 102 |
| Reminding module | 103 |
| Closing module | 104 |
| Inquiry module | 105 |
Following embodiment further illustrates the present invention in connection with above-mentioned accompanying drawing.
Embodiment
As shown in Figure 1, be wireless telecommunications system management system running environment figure under state of flight of the present invention.Under this state of flight, wireless telecommunications system management system 10 operates on wireless telecommunications system 1, this wireless telecommunications system 1 can be mobile phone, panel computer, personal digital assistant etc., and comprises that memory 12, processor 14, acceleration transducer 16, air pressure detect meter 18.
Described acceleration transducer 16 is for detecting in real time the acceleration of gravity of wireless telecommunications system 1.
Described air pressure detects meter 18 for detection of the air pressure in aircraft cabin, and it can be a transducer that cabin internal gas pressure can be detected that this air pressure detects meter.
In the present embodiment, under described state of flight, wireless telecommunications system management system 10 can be divided into one or more modules, described one or more module is stored in the memory 12 of described wireless telecommunications system 1 and is configured to and carried out by one or more processors (the present embodiment is a processor 14), to complete the present invention.For example, consult shown in Fig. 2, under described state of flight, wireless telecommunications system management system 10 is divided into read module 100, opening module 101, judge module 102, reminding module 103, closing module 104 and inquiry module 105.The alleged module of the present invention has been the program segment of a specific function, is more suitable in describing the implementation of software in wireless telecommunications system 1, the description of consulting Fig. 3 about the function of each module than program.
As shown in Figure 3, be the flow chart of the preferred embodiment of wireless telecommunications system management method under state of flight of the present invention.
Step S10, read module 100 reads the acceleration of the wireless telecommunications system 1 that acceleration sensor 16 detects in real time.
Step S11, in the time that the acceleration of the wireless telecommunications system 1 reading exceedes the first preset value, the air pressure of opening module 101 open wireless communication apparatus 1 detects meter 18 and starts to detect aircraft cabin internal gas pressure, described the first preset value can independently be set by the user of wireless telecommunications system 1, but can not set too low, the too low meeting of the first preset value causes the safe flight pattern of opening wireless telecommunications system regular and that there is no need, can not set too high, if the first preset value exceeds the minimum acceleration when taking off or landing, will cause aircraft to enter to take off or landing state after can not open in time safe flight pattern.In present embodiment, this first preset value can be set as 0.4m/s
2.
Step S12, judge module 102 judges whether the acceleration of wireless telecommunications system 1 exceedes the second preset value, in the time that the acceleration of wireless telecommunications system 1 exceedes the second preset value, enter step S13, described the second preset value is the minimum acceleration while taking off, this second preset value can be set by the user of wireless telecommunications system 1, and the second preset value is greater than the first preset value, this second preset value is because of aircraft type difference difference, for example, in existing each model aircraft, the minimum acceleration that takes off is 3m/s
2so can set the second preset value in present embodiment is 3m/s
2.
Step S13, more than judge module 102 judges whether aircraft cabin internal gas pressure changes fast and be stabilized in default atmospheric pressure value, when aircraft cabin internal gas pressure changes fast and is stabilized in default atmospheric pressure value when above, enters step S14.In present embodiment, in the time judging whether aircraft cabin internal gas pressure changes fast, can adopt following methods: suppose that it is 100ms that air pressure detects meter 18 sense cycle, will detect in 1s 10 times, in 1s, the mean value δ of cabin internal gas pressure be Pa1+Pa2+Pa3+... + Pa10/10.If the air pressure detecting for the first time after 1s is Pa, get Pa/ δ gained remainder, and this remainder is turned to percentage, if in continuous 5s, above-mentioned percentage variation exceedes 5%, judges that aircraft cabin internal gas pressure changes violent.In addition, in present embodiment, can set default atmospheric pressure value is 0.6 handkerchief.Generally, before taking off, aircraft cabin is communicated with outside, equates, after taking off in aircraft cabin with the outer air pressure of aircraft, along with aircraft altitude rises, ambient pressure reduces, aircraft cabin air pressure thereupon fast-descending when mush more than 3000 meters height time, aircraft unlatching cabin compression system, make at least to maintain in cabin 0.6 handkerchief upper and lower, to prevent that the discomfort of health from appearring in passenger.Landing process is contrary, along with the reduction of flying height, ambient pressure raises, cabin internal gas pressure also raises thereupon fast, but it is upper and lower at least to maintain 0.6 handkerchief, in the time that aircraft lands, in cabin, return to and air pressure identical outside cabin, therefore, when aircraft cabin internal gas pressure changes fast and be stabilized in 0.6 handkerchief when above, aircraft is in taking off or landing state.
Step S14, closing module 104 is closed the wireless communication function of wireless telecommunications system 1.
In present embodiment, under described state of flight, wireless telecommunications system management method can also comprise: when the acceleration of wireless telecommunications system 1 exceedes the second preset value again, and aircraft cabin internal gas pressure again changes fast and is stabilized in default atmospheric pressure value when above, reminding module 103 point out user now aircraft in landing state, after aircraft lands completely, can open the wireless communication function of wireless telecommunications system 1.
In present embodiment, after the wireless communication function that can also work as wireless telecommunications system 1 is closed, by inquiry module 105 further inquiry user whether wireless telecommunications system 1 is shut down, and wireless telecommunications system 1 is shut down in the input that receives user.In present embodiment, can inquire that the mode at interface inquires whether user shuts down wireless telecommunications system 1, and this selection interface may further include a confirming button, and user can click this confirming button wireless telecommunications system 1 is shut down by ejection.
Pressure when described step S10 to S14 takes off by detecting or lands in acceleration and the aircraft cabin of wireless telecommunications system 1, the wireless communication function of automatically closing wireless telecommunications system 1 in the time taking off will, and reminding passengers can be opened the wireless communication function of wireless telecommunications system 1 in the time of landing, thereby more effectively ensure Flight Safety.
Above execution mode is only unrestricted in order to technical scheme of the present invention to be described, although the present invention is had been described in detail with reference to preferred embodiment, those of ordinary skill in the art is to be understood that, can modify or be equal to replacement technical scheme of the present invention, and not depart from the spirit and scope of technical solution of the present invention.
Claims (8)
1. a wireless telecommunications system management method under state of flight, is characterized in that, the method comprises:
Read step, reads the acceleration of the wireless telecommunications system that the acceleration transducer of wireless telecommunications system detects in real time;
Open step, in the time that the acceleration of the wireless telecommunications system reading exceedes the first preset value, the air pressure of open wireless communication apparatus detects meter and detects aircraft cabin internal gas pressure;
The first determining step, judges whether the acceleration of wireless telecommunications system exceedes the second preset value, in the time that the acceleration of wireless telecommunications system exceedes the second preset value, enters the second determining step;
The second determining step, more than judging whether aircraft cabin internal gas pressure changes fast and be stabilized in default atmospheric pressure value, when aircraft cabin internal gas pressure changes fast and is stabilized in default atmospheric pressure value when above, enters and closes step;
Close step, close the wireless communication function of wireless telecommunications system.
2. wireless telecommunications system management method under state of flight according to claim 1, it is characterized in that, the method also comprises: when the acceleration of wireless telecommunications system exceedes the second preset value again, and aircraft cabin internal gas pressure again changes fast and is stabilized in default atmospheric pressure value when above, now aircraft is in landing state for prompting user, and backwardness completely falls in aircraft can open the wireless communication function of wireless telecommunications system.
3. wireless telecommunications system management method under state of flight according to claim 1, is characterized in that, the method also comprises: described close step after further inquiry user whether wireless telecommunications system is shut down.
4. wireless telecommunications system management method under state of flight according to claim 1, is characterized in that, described the first preset value is 0.4m/s
2, described the second preset value is 3m/s
2, described default atmospheric pressure value is 0.6 handkerchief.
5. a wireless telecommunications system management system under state of flight, is characterized in that, this system comprises:
Read module, for reading in real time the acceleration of the wireless telecommunications system that the acceleration transducer of wireless telecommunications system detects;
Opening module, while exceeding the first preset value for the acceleration when the wireless telecommunications system reading, the air pressure of open wireless communication apparatus detects meter and detects aircraft cabin internal gas pressure;
Whether judge module, exceed the second preset value for the acceleration that judges wireless telecommunications system;
Described judge module, also in the time that the acceleration of wireless telecommunications system exceedes the second preset value, more than continuing to judge whether aircraft cabin internal gas pressure changes fast and be stabilized in default atmospheric pressure value;
Closing module, for changing fast and be stabilized in default atmospheric pressure value and close when above the wireless communication function of wireless telecommunications system when aircraft cabin internal gas pressure.
6. wireless telecommunications system management system under state of flight according to claim 5, is characterized in that, this system also comprises:
Reminding module, again exceed the second preset value for the acceleration when wireless telecommunications system, and aircraft cabin internal gas pressure again changes fast and is stabilized in default atmospheric pressure value when above, now aircraft is in landing state for prompting user, and backwardness completely falls in aircraft can open the wireless communication function of wireless telecommunications system.
7. wireless telecommunications system management system under state of flight according to claim 5, is characterized in that, this system also comprises:
Inquiry module, after being closed when the wireless communication function of wireless telecommunications system, further inquires whether user shuts down wireless telecommunications system.
8. wireless telecommunications system management system under state of flight according to claim 5, is characterized in that, described the first preset value is 0.4m/s
2, described the second preset value is 3m/s
2, described default atmospheric pressure value is 0.6 handkerchief.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210559879.4A CN103888591B (en) | 2012-12-21 | 2012-12-21 | Wireless telecommunications system management method and system under state of flight |
| TW101150718A TW201436607A (en) | 2012-12-21 | 2012-12-27 | System and method for managing a wireless communication device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210559879.4A CN103888591B (en) | 2012-12-21 | 2012-12-21 | Wireless telecommunications system management method and system under state of flight |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103888591A true CN103888591A (en) | 2014-06-25 |
| CN103888591B CN103888591B (en) | 2018-03-20 |
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ID=50957306
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210559879.4A Expired - Fee Related CN103888591B (en) | 2012-12-21 | 2012-12-21 | Wireless telecommunications system management method and system under state of flight |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN103888591B (en) |
| TW (1) | TW201436607A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105208216A (en) * | 2015-10-22 | 2015-12-30 | 小米科技有限责任公司 | Control method and device for terminal, and terminal |
| CN105204641A (en) * | 2015-09-24 | 2015-12-30 | 广州视源电子科技股份有限公司 | Method and device for controlling airplane mode |
| CN105721691A (en) * | 2016-01-29 | 2016-06-29 | 努比亚技术有限公司 | Mobile terminal and method for controlling flight mode thereof |
| CN109634303A (en) * | 2018-12-13 | 2019-04-16 | 歌联科技（上海）有限公司 | Portable electronic device aviation silent system and its automatic silent method automatically |
| CN110020705A (en) * | 2019-03-29 | 2019-07-16 | 上海宜链物联网有限公司 | A kind of active temperature measuring label and its implementation of self recovery starting communication |
| CN111912451A (en) * | 2019-05-09 | 2020-11-10 | 意法半导体公司 | Mobile device transportation mode management device, system and method |
| WO2021031851A1 (en) * | 2019-08-16 | 2021-02-25 | 华为技术有限公司 | Method for detecting flying state and terminal device |
| CN113034979A (en) * | 2021-02-24 | 2021-06-25 | 飞天联合（北京）系统技术有限公司 | Scene-based intelligent aviation container communication opening and closing method and device |
| CN113259800A (en) * | 2021-04-23 | 2021-08-13 | 歌尔股份有限公司 | Earphone, electronic equipment and method for controlling operation mode of electronic equipment |
| US20220229402A1 (en) * | 2021-01-15 | 2022-07-21 | Sony Group Corporation | Operating a portable electronic device to detect airplane flight events |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| TWI652954B (en) | 2018-01-30 | 2019-03-01 | 和碩聯合科技股份有限公司 | Operation mode switching method and electronic device using the same |
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- 2012-12-21 CN CN201210559879.4A patent/CN103888591B/en not_active Expired - Fee Related
- 2012-12-27 TW TW101150718A patent/TW201436607A/en unknown
Patent Citations (3)
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| US20080004040A1 (en) * | 2006-07-01 | 2008-01-03 | Bogart Dave W | Method and apparatus for actively monitoring personal cellular devices and controlling access to a cellular communications network within an airborne mobile platform |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105204641A (en) * | 2015-09-24 | 2015-12-30 | 广州视源电子科技股份有限公司 | Method and device for controlling airplane mode |
| CN105208216A (en) * | 2015-10-22 | 2015-12-30 | 小米科技有限责任公司 | Control method and device for terminal, and terminal |
| CN105721691A (en) * | 2016-01-29 | 2016-06-29 | 努比亚技术有限公司 | Mobile terminal and method for controlling flight mode thereof |
| CN109634303B (en) * | 2018-12-13 | 2024-02-09 | 歌联科技（上海）有限公司 | Aviation automatic silencing method for portable electronic equipment |
| CN109634303A (en) * | 2018-12-13 | 2019-04-16 | 歌联科技（上海）有限公司 | Portable electronic device aviation silent system and its automatic silent method automatically |
| CN110020705A (en) * | 2019-03-29 | 2019-07-16 | 上海宜链物联网有限公司 | A kind of active temperature measuring label and its implementation of self recovery starting communication |
| CN111912451A (en) * | 2019-05-09 | 2020-11-10 | 意法半导体公司 | Mobile device transportation mode management device, system and method |
| WO2021031851A1 (en) * | 2019-08-16 | 2021-02-25 | 华为技术有限公司 | Method for detecting flying state and terminal device |
| US20220229402A1 (en) * | 2021-01-15 | 2022-07-21 | Sony Group Corporation | Operating a portable electronic device to detect airplane flight events |
| US11782398B2 (en) * | 2021-01-15 | 2023-10-10 | Sony Group Corporation | Operating a portable electronic device to detect airplane flight events |
| CN113034979A (en) * | 2021-02-24 | 2021-06-25 | 飞天联合（北京）系统技术有限公司 | Scene-based intelligent aviation container communication opening and closing method and device |
| CN113259800A (en) * | 2021-04-23 | 2021-08-13 | 歌尔股份有限公司 | Earphone, electronic equipment and method for controlling operation mode of electronic equipment |
| CN113259800B (en) * | 2021-04-23 | 2023-01-17 | 歌尔股份有限公司 | Earphone and method for controlling operation mode of electronic equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| TW201436607A (en) | 2014-09-16 |
| CN103888591B (en) | 2018-03-20 |
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