CN111899376A - Fire balloon flight monitoring system - Google Patents

Fire balloon flight monitoring system Download PDF

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Publication number
CN111899376A
CN111899376A CN202010639810.7A CN202010639810A CN111899376A CN 111899376 A CN111899376 A CN 111899376A CN 202010639810 A CN202010639810 A CN 202010639810A CN 111899376 A CN111899376 A CN 111899376A
Authority
CN
China
Prior art keywords
weather
module
flight
data
monitoring system
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202010639810.7A
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Chinese (zh)
Inventor
徐新材
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Qiaofeng Aviation Technology Co Ltd
Original Assignee
Shanghai Qiaofeng Aviation Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Qiaofeng Aviation Technology Co Ltd filed Critical Shanghai Qiaofeng Aviation Technology Co Ltd
Priority to CN202010639810.7A priority Critical patent/CN111899376A/en
Publication of CN111899376A publication Critical patent/CN111899376A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G07CHECKING-DEVICES
    • G07CTIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00Registering or indicating the working of vehicles
    • G07C5/08Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
    • G07C5/0841Registering performance data
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/40Balloons
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073Surveillance aids
    • G08G5/0078Surveillance aids for monitoring traffic from the aircraft
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073Surveillance aids
    • G08G5/0086Surveillance aids for monitoring terrain
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073Surveillance aids
    • G08G5/0091Surveillance aids for monitoring atmospheric conditions

Abstract

The utility model provides a fire balloon flight monitoring system, includes weather module, position module, display module, data processing module, weather module for monitoring weather condition, the position module for monitoring flight position and flight track, data processing module for receiving the weather data that weather module sent, the position data that receive position module sent, and send weather data and position data for display module, display module for the demonstration.

Description

Fire balloon flight monitoring system
Technical Field
The invention relates to the field of aircrafts, in particular to a fire balloon flight monitoring system.
Background
The aviation market in China is relatively small at present, but has great potential to become the largest general aviation private consumer market all over the world. At present, the technology related to the domestic low-altitude tourism market is blank, and the technology is less in the related field of low-altitude aircrafts, particularly aircrafts for air touring by using hot air balloons.
Disclosure of Invention
The invention provides a fire balloon flight monitoring system, which comprises a weather module, a position module, a display module and a data processing module, wherein the weather module is used for monitoring weather conditions, the position module is used for monitoring flight positions and flight tracks, the data processing module is used for receiving weather data sent by the weather module, receiving position data sent by the position module and sending the weather data and the position data to the display module, and the display module is used for displaying.
In some embodiments, the weather module may monitor weather and wind.
In some embodiments, the weather data includes weather at the current time point of the different altitude layer and weather after the current time point of the different altitude layer.
In some embodiments, the location data includes altitude, longitude, and latitude.
In some embodiments, the location data further includes hot-balloon intrinsic information.
In some embodiments, the hot air balloon intrinsic information includes model of the hot air balloon, load, fuel information, weight of the passenger.
In some embodiments, the display module may display weather data in real-time.
In some embodiments, after the flight is completed, the data processing module records the data in a unified format as a flight record.
In some embodiments, it may be available to crew and crew members.
A second aspect of the invention provides the use of a hot-air balloon flight monitoring system as described above in the field of aerospace vehicles.
The invention has the beneficial effects that:
(1) the weather module and the position module are combined, so that the defects of a related system in the field of domestic low-altitude flight are overcome;
(2) the intrinsic information of the hot air balloon can be set, so that the safety of flight is greatly improved. The intrinsic information can be set by a user, so that the application range of the current monitoring system is widened;
(3) the monitoring system provided by the invention can be combined with map software commonly used in the market at present, such as a google map, a Baidu map, a Gaode map and the like, and a user can select the monitoring system according to the network condition of the location and the selection preference of the user;
(4) a destination or other place of interest may be marked in the monitoring system;
(5) after the flight is finished, the data recorded in the flight process, including the weather data, the position data and other unified formats, can be recorded into the flight record, so that the problem that the flight record is recorded with a great deal of energy and time due to the fact that formats in the prior art are not unified is avoided;
(6) the monitoring system provided by the invention can be used by the crew and the crew simultaneously, so that the crew can master the flight state in real time.
Drawings
FIG. 1 is a schematic diagram of a hot balloon flight monitoring system in accordance with one embodiment of the present invention.
Detailed Description
The invention is further illustrated by the following specific examples.
Examples
The utility model provides a fire balloon flight monitoring system, includes weather module, position module, display module, data processing module, weather module for monitoring weather condition, the position module for monitoring flight position and flight track, data processing module for receiving the weather data that weather module sent, the position data that receive position module sent, and send weather data and position data for display module, display module for the demonstration.
The weather module may monitor weather and wind. The weather data comprises the weather of the current time point of different height layers and the weather after the current time point of different height layers. Wind power has a large influence on the flight of the fire balloon, and wind power and weather of different height layers need to be monitored before the fire balloon flies. Not only the current wind power and weather conditions, but also the wind power and weather conditions in a future period and the change trend are known, so that the safety of the fire balloon flight is improved.
The location data includes altitude, longitude, and latitude. By recording the altitude, the current altitude of the hot air balloon and the rising or falling trend can be obtained in real time. The longitude and the latitude are helpful for realizing the positioning of the hot air balloon and recording the flight track and the flight state of the hot air balloon, so that all flight data can be traced, and the training of a hot air balloon pilot and the information exchange between a crew member and a crew member have great influence.
The location data also includes hot-balloon intrinsic information. The fire balloon intrinsic information comprises the model of the fire balloon, load, fuel information and weight of passengers. Different types of hot air balloons show different information such as sizes, specifications, weights and the like, and have corresponding different aviation requirements and different requirements on hot air balloon pilots aiming at different types of hot air balloons. The load can reflect the bearing capacity of the hot air balloon, the fuel information can reflect the cruising capacity of the hot air balloon, the safety of the flight required to be carried out, the risks possibly encountered and the like can be comprehensively analyzed by combining the weight of passengers and corresponding weather data, and the planning and optimization of the flight route can also be realized by combining a map.
The display module can display weather data in real time.
After the flight is completed, the data processing module records the data in a unified format as a flight record.
Can be used by the crew and crew.
When a user needs to use the monitoring system provided by the invention, the user can log in the system through the authentication of the user name and the password. The verification method is not limited to user names and passwords, and also comprises fingerprint identification verification, face identification verification and the like.
The display module can display the map in the interface, and the user can input the destination or directly select the destination on the map, click to start the flight, and enter the preparation stage before the flight. In the preparation stage before flight, the display module feeds the weather data, the position data and the intrinsic data of the hot air balloon back to the user, and the user can also input related data by himself.
Examples of layers of different heights include ground, 300, 600, 750, 900, 15002400, 3000m, etc. Corresponding weather data, wind power and other meteorological data can be acquired through the weather module. On a map interface displayed by the display module, a user can zoom, stretch, point length and angle on the map. The user can also select the map data provided by different map software according to the network environment or the use habit of the user.
After the flight is started, different colors can be used for indicating different flight state parameters. For example orange for the flight altitude and green for the vertical velocity, which can be displayed in real time. Of course, the user may also customize the color of the flight parameters.
After the flight is completed, the display module presents the data recorded by the flight to the user, and the user can derive the relevant data.

Claims (10)

1. A fire balloon flight monitoring system is characterized by comprising a weather module, a position module, a display module and a data processing module,
a weather module for monitoring a weather condition,
a position module for monitoring the flight position and the flight track,
the data processing module is used for receiving the weather data sent by the weather module, receiving the position data sent by the position module and sending the weather data and the position data to the display module,
and the display module is used for displaying.
2. The fire balloon flight monitoring system of claim 1, wherein the weather module is capable of monitoring weather and wind forces.
3. A fire balloon flight monitoring system according to claim 1, wherein the weather data includes weather at and after a current point in time in different altitudes.
4. A fire balloon flight monitoring system as claimed in claim 1, wherein the position data comprises altitude, longitude, latitude.
5. The fire balloon flight monitoring system of claim 4, wherein the location data further comprises fire balloon intrinsic information.
6. The fire balloon flight monitoring system of claim 5, wherein the fire balloon intrinsic information comprises a type of fire balloon, a payload, fuel information, and a weight of an occupant.
7. The fire balloon flight monitoring system of claim 1, wherein the display module is capable of displaying weather data in real time.
8. The fire balloon flight monitoring system of claim 1, wherein the data processing module records the data in a unified format as a flight record after completion of the flight.
9. A fire balloon flight monitoring system according to claim 1, available to crew and crew.
10. Use of a fire balloon flight monitoring system according to any one of claims 1 to 9 in the field of aeronautical vehicles.
CN202010639810.7A 2020-07-06 2020-07-06 Fire balloon flight monitoring system Pending CN111899376A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010639810.7A CN111899376A (en) 2020-07-06 2020-07-06 Fire balloon flight monitoring system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010639810.7A CN111899376A (en) 2020-07-06 2020-07-06 Fire balloon flight monitoring system

Publications (1)

Publication Number Publication Date
CN111899376A true CN111899376A (en) 2020-11-06

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113223207A (en) * 2021-05-13 2021-08-06 中南大学 Fire balloon safe flight intelligent monitoring system and method

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CN205910527U (en) * 2016-06-03 2017-01-25 西安航空电子科技有限公司 Low latitude airborne vehicle monitored control system
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CN207367391U (en) * 2017-08-11 2018-05-15 唐坚 Monitoring system for low-latitude flying
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CN108803656A (en) * 2018-06-12 2018-11-13 南京航空航天大学 A kind of flight control method and system based on complicated low latitude
CN109035872A (en) * 2018-08-08 2018-12-18 湖北河海科技发展有限公司 Weather information and Track Fusion display system and method
US20190033885A1 (en) * 2017-07-28 2019-01-31 X Development Llc Systems and methods for controlling aerial vehicles
CN109649628A (en) * 2018-12-11 2019-04-19 中国特种飞行器研究所 A kind of long endurance wind resistance dirigible system
CN110347073A (en) * 2018-04-02 2019-10-18 通用电气航空系统有限责任公司 Flight management system and update method
CN110466732A (en) * 2019-09-06 2019-11-19 刘晓民 Military spacecraft

Patent Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101582205A (en) * 2009-06-11 2009-11-18 山东大学 Method and device for monitoring flying state of low-altitude airspace aerocraft
CN102033546A (en) * 2010-11-09 2011-04-27 上海交通大学 Low-altitude airship flight control system and flight control method thereof
CN102682194A (en) * 2010-12-13 2012-09-19 波音公司 Temporally based weather symbology
CN202814522U (en) * 2012-09-14 2013-03-20 航宇救生装备有限公司 Balloon or hot air ship fuel monitoring device
US20180067499A1 (en) * 2015-12-08 2018-03-08 X Development Llc Selection between Explore Mode and Control Mode for Aerial Vehicle
CN205910527U (en) * 2016-06-03 2017-01-25 西安航空电子科技有限公司 Low latitude airborne vehicle monitored control system
US20190033885A1 (en) * 2017-07-28 2019-01-31 X Development Llc Systems and methods for controlling aerial vehicles
CN207367391U (en) * 2017-08-11 2018-05-15 唐坚 Monitoring system for low-latitude flying
CN207074380U (en) * 2017-08-24 2018-03-06 中国科学院测量与地球物理研究所 A kind of light weight remote sensor loading device of dynamic helium balloon
CN110347073A (en) * 2018-04-02 2019-10-18 通用电气航空系统有限责任公司 Flight management system and update method
CN108320586A (en) * 2018-04-04 2018-07-24 飞行家族(北京)科技有限公司 A kind of low altitude airspace obstacle information acquisition system and method
CN108803656A (en) * 2018-06-12 2018-11-13 南京航空航天大学 A kind of flight control method and system based on complicated low latitude
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CN110466732A (en) * 2019-09-06 2019-11-19 刘晓民 Military spacecraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113223207A (en) * 2021-05-13 2021-08-06 中南大学 Fire balloon safe flight intelligent monitoring system and method

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Application publication date: 20201106

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