CN112498702A - Electronic parachute opening control device, electronic parachute opening control method and parachute - Google Patents
Electronic parachute opening control device, electronic parachute opening control method and parachute Download PDFInfo
- Publication number
- CN112498702A CN112498702A CN202011490310.8A CN202011490310A CN112498702A CN 112498702 A CN112498702 A CN 112498702A CN 202011490310 A CN202011490310 A CN 202011490310A CN 112498702 A CN112498702 A CN 112498702A
- Authority
- CN
- China
- Prior art keywords
- parachute
- microprocessor
- opening control
- control device
- satellite positioning
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 15
- 238000012545 processing Methods 0.000 claims abstract description 4
- 239000000284 extract Substances 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 abstract description 5
- 230000007613 environmental effect Effects 0.000 abstract description 2
- 230000008602 contraction Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000011982 device technology Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/40—Packs
- B64D17/52—Opening, e.g. manual
- B64D17/54—Opening, e.g. manual automatic
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
本发明属于航空救生技术，涉及一种电子式开伞控制装置及开伞控制方法和降落伞。所述电子式开伞控制装置包括卫星定位模块(1)、微处理器(2)、切割器(3)，其中，所述卫星定位模块(1)与卫星通信，实时获取降落伞的位置信息，并与微处理器连接，所述微处理器用于信号处理，并与切割器连接，所述切割器接收微处理器发送的开伞信号，打开降落伞。本发明高度信息获取稳定，不易受到环境气象因素影响，也不存在脱舱时的瞬时波动，安全可靠，相对于传统开伞方式具有较大的技术进步。
The invention belongs to aviation life-saving technology, and relates to an electronic parachute opening control device, a parachute opening control method and a parachute. The electronic parachute opening control device comprises a satellite positioning module (1), a microprocessor (2), and a cutter (3), wherein the satellite positioning module (1) communicates with satellites to obtain the position information of the parachute in real time, It is connected with the microprocessor, which is used for signal processing and connected with the cutter, and the cutter receives the parachute opening signal sent by the microprocessor and opens the parachute. The present invention obtains the altitude information stably, is not easily affected by environmental meteorological factors, does not have instantaneous fluctuations when unpacking, is safe and reliable, and has great technical progress compared with the traditional parachute opening method.
Description
Technical Field
The invention belongs to the aviation lifesaving technology, and relates to an electronic parachute opening control device, a parachute opening control method and a parachute.
Background
At present, the domestic parachute is mostly applied to a mechanical power type parachute opening control technology, and an electronic type automatic parachute opening technology is still under research. The mechanical power type parachute opening control technology uses a diaphragm box to sense the height change of air pressure, and the measurement precision is low; because the mechanical spring is adopted as the output power, the product structure is large in size, heavy in weight and the like, and the requirements of modern airborne troops on training and fighting are not met.
Even though the conventional electronic automatic parachute opening still uses the air pressure sensor to perform the parachute-releasing control by sensing the height, as disclosed in CN203200605823U, the electronic parachute opener, which is an electronic parachute opener and is controlled by a microprocessor, is still used to sense the height. However, when the air pressure sensor senses the height, the air pressure sensor is greatly influenced by the external air pressure, particularly when the parachute leaves the cabin, the instantaneous air pressure of the parachute is greatly fluctuated, an error instruction is easily generated, an error parachute opening signal is issued, and great potential safety hazards are caused.
Disclosure of Invention
The purpose of the invention is: the electronic parachute opening control device is simple in structure, safe and reliable, and based on GPS positioning, the parachute can be automatically opened under the condition that the height of the electronic parachute opening control device is lower than a set height.
In addition, the invention also provides an umbrella opening method based on the electronic umbrella opening control device.
The invention also protects a parachute adopting the electronic parachute opening control device.
The technical scheme of the invention is as follows: the utility model provides an electronic type parachute opening controlling means, parachute opening controlling means installs in the parachute, parachute opening controlling means includes satellite positioning module 1, microprocessor 2, cutterbar 3, wherein, satellite positioning module 1 and satellite communication acquire the positional information of parachute in real time to be connected with microprocessor, microprocessor is used for signal processing to be connected with the cutterbar, the parachute opening signal that microprocessor sent is received to the cutterbar, opens the parachute.
The satellite positioning module 1 and the microprocessor are integrated on the same circuit board, so that the size is small, the installation and the carrying are easy, and the satellite positioning module is suitable for being installed on a single parachute.
All be provided with the metal shield cover outside satellite positioning module 1 and the microprocessor to can provide effective protection for satellite positioning module and microprocessor, avoid receiving the interference of external environment and airborne magnetic field, improve parachute opening fail safe nature.
The microprocessor is internally provided with a comparator, and an umbrella opening instruction is given by comparing the height value preset inside with the height information given by the satellite positioning module.
The satellite positioning module is a GPS module or a Beidou satellite positioning module, acquires the actual position information of the parachute by receiving satellite signals, and converts the actual position information into height information.
The electronic automatic umbrella opening control device further comprises a power circuit which is connected with the satellite positioning module, the microprocessor and the cutter and used for providing power.
A parachute opening control method based on the electronic automatic parachute opening control device is characterized in that a satellite positioning module detects parachute position information in real time and sends the parachute position information to a microprocessor, the microprocessor extracts and converts the parachute position information into a height signal, the height signal is compared with the height of an internally-arranged parachute, when the height of the internally-arranged parachute is achieved, the microprocessor sends a parachute opening instruction to control a cutter to cut a contraction rope, a parachute pack is opened, and parachute opening is completed.
A parachute comprises the electronic automatic parachute opening control device.
The invention has the beneficial effects that: the electronic automatic parachute opening control device obtains real-time altitude through satellite positioning, the microprocessor judges whether the height of the parachute system is lower than a set height, and if the height of the parachute system is lower than the set height, the parachute is automatically opened. Therefore, the height information of the aircraft is stable to acquire, is not easily influenced by environmental meteorological factors, does not have instantaneous fluctuation during the taking off of the aircraft cabin, and is safe and reliable.
Drawings
FIG. 1 is a schematic diagram of the electronic controller for opening the umbrella according to the present invention;
wherein, the device comprises a 1-GPS module, a 2-microprocessor, a 3-cutter and a 4-power circuit.
Fig. 2 is a program control diagram of a parachute height control parachute opening technique of the present invention.
Detailed Description
The following further describes the embodiments of the present invention with reference to the drawings.
Example 1: referring to fig. 1, the parachute opening control apparatus of the present invention includes a satellite positioning module 1, a microprocessor 2, and a cutter 3, wherein:
the satellite positioning module adopts a GPS module and is used for acquiring position information in real time and transmitting a signal to the microprocessor;
the microprocessor is an intelligent component with a single chip microcomputer as a core, can receive and process the position information transmitted by the GPS module, converts the ground height H in the position information into the altitude height H, namely, carries out a series of processing on the received data through a software program, judges the current altitude value, and outputs an parachute opening control signal to the cutter when the altitude is smaller than the parachute opening altitude set value.
The GPS module performs the height signal conversion process as follows:
if the measured height of the ground at a certain point p is H and the altitude is H, the elevation anomaly zeta is
ζ＝H-h
According to the Bruns formula, the calculation formula of the model elevation anomaly of one point on the earth surface is
In the formula: p is obtained by the process of the step of,
lambda is the geocentric radial, geocentric latitude and geocentric longitude of the calculation point p respectively;
GM is the product of the universal gravitation constant and the earth mass;
γpcalculating the normal gravity value of the point;
alpha is the earth's major semiaxis;
n is the highest order of the earth gravity field model expansion, and N and m are natural numbers;
α＝6378137.0m，GM＝3.986004417×1014m13/S2。
the cutter is a fuse device, is connected with a contraction rope of the parachute, and starts to work when receiving a parachute opening control signal to cut off the contraction rope.
When the electronic automatic parachute opening control device is used for controlling parachute opening, the GPS module detects the position information of the parachute in real time and sends the position information to the microprocessor, the microprocessor extracts and converts the position information into a height signal, the height signal is compared with the height of the internally-arranged parachute, and when the height of the internally-arranged parachute is reached, the microprocessor sends a parachute opening instruction to control the cutter to cut the contraction rope, open the parachute pack and complete parachute opening.
The electronic automatic parachute opening control device technology is based on GPS, Beidou and other satellite positioning systems, parachute opening is carried out by utilizing height information converted by the obtained ground position information, signals are stable and reliable, the device is not easily influenced by the environment, safety and reliability of parachute opening are effectively improved, the device can be used in the fields of airborne landing and air drop, and the device has a large practical application value.
The above-mentioned embodiments are merely illustrative of the technical ideas and features of the present invention, and the purpose thereof is to enable those skilled in the art to understand the contents of the present invention and to implement the same, and not to limit the scope of the present invention, and all equivalent changes or modifications made according to the spirit of the present invention should be covered by the scope of the present invention. The techniques, shapes, and configurations not described in detail in the present invention are all known techniques.
Claims (9)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011490310.8A CN112498702A (en) | 2020-12-16 | 2020-12-16 | Electronic parachute opening control device, electronic parachute opening control method and parachute |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011490310.8A CN112498702A (en) | 2020-12-16 | 2020-12-16 | Electronic parachute opening control device, electronic parachute opening control method and parachute |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112498702A true CN112498702A (en) | 2021-03-16 |
Family
ID=74972934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011490310.8A Pending CN112498702A (en) | 2020-12-16 | 2020-12-16 | Electronic parachute opening control device, electronic parachute opening control method and parachute |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112498702A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113428367A (en) * | 2021-08-02 | 2021-09-24 | 武汉永力技术有限公司 | Method for controlling parachute opening of parachute and electronic automatic parachute opening system thereof |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101819688A (en) * | 2010-04-12 | 2010-09-01 | 中国科学院长春光学精密机械与物理研究所 | Parachuting height early warning record device and method thereof |
| CN102147475A (en) * | 2010-02-09 | 2011-08-10 | 武汉大学 | Method and device for simultaneously determining three-dimensional geometry position and gravity potential by utilizing global position system (GPS) signal |
| US9145212B1 (en) * | 2014-06-12 | 2015-09-29 | Shenzhen Hubsan Intelligent Co., Ltd. | Parachute control system and method for an aircraft |
| CN105366037A (en) * | 2015-11-27 | 2016-03-02 | 成都飞机工业（集团）有限责任公司 | Unmanned aerial vehicle with changeable flight mode |
| CN205168921U (en) * | 2015-12-03 | 2016-04-20 | 武汉航空仪表有限责任公司 | Parachute altitude control parachute -opening mechanism |
| CN205256682U (en) * | 2015-12-21 | 2016-05-25 | 威海三智科技有限公司 | Control system is retrieved in unmanned aerial vehicle parachuting |
| CN207450275U (en) * | 2017-07-11 | 2018-06-05 | 南昌航空大学 | A kind of anti-crash landing system of unmanned plane |
-
2020
- 2020-12-16 CN CN202011490310.8A patent/CN112498702A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102147475A (en) * | 2010-02-09 | 2011-08-10 | 武汉大学 | Method and device for simultaneously determining three-dimensional geometry position and gravity potential by utilizing global position system (GPS) signal |
| CN101819688A (en) * | 2010-04-12 | 2010-09-01 | 中国科学院长春光学精密机械与物理研究所 | Parachuting height early warning record device and method thereof |
| US9145212B1 (en) * | 2014-06-12 | 2015-09-29 | Shenzhen Hubsan Intelligent Co., Ltd. | Parachute control system and method for an aircraft |
| CN105366037A (en) * | 2015-11-27 | 2016-03-02 | 成都飞机工业（集团）有限责任公司 | Unmanned aerial vehicle with changeable flight mode |
| CN205168921U (en) * | 2015-12-03 | 2016-04-20 | 武汉航空仪表有限责任公司 | Parachute altitude control parachute -opening mechanism |
| CN205256682U (en) * | 2015-12-21 | 2016-05-25 | 威海三智科技有限公司 | Control system is retrieved in unmanned aerial vehicle parachuting |
| CN207450275U (en) * | 2017-07-11 | 2018-06-05 | 南昌航空大学 | A kind of anti-crash landing system of unmanned plane |
Non-Patent Citations (1)
| Title |
|---|
| 田桂娥主编: "大地测量学基础", 31 December 2014, 武汉大学出版社, pages: 56 - 58 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113428367A (en) * | 2021-08-02 | 2021-09-24 | 武汉永力技术有限公司 | Method for controlling parachute opening of parachute and electronic automatic parachute opening system thereof |
| CN113428367B (en) * | 2021-08-02 | 2024-04-05 | 武汉永力技术有限公司 | Method for controlling parachute opening and electronic automatic parachute opening system thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103744429B (en) | A kind of small-sized depopulated helicopter flight control system | |
| CN107272740B (en) | Novel four-rotor unmanned aerial vehicle control system | |
| CN108303995A (en) | A kind of substation inspection unmanned plane during flying security system | |
| CN104417759B (en) | A kind of Intelligent parachute based on the many sensings of multiparameter | |
| CN106443831A (en) | All-weather meteorological detection system based on unmanned aerial vehicle | |
| CN107402583B (en) | Light remote sensing sensor carrying device with power helium balloon | |
| CN107145158B (en) | Rotor unmanned aerial vehicle, and abnormal landing processing device and processing method thereof | |
| CN205418093U (en) | A multiaxis aircraft for atmospheric sampling | |
| CN103927798B (en) | A kind of recording method suitable in middle-size and small-size unmanned plane during flying data and device | |
| CN105607640B (en) | Pose controller of quadrotor aircraft | |
| CN106125755B (en) | Atmospheric boundary layer environment autonomous detection system and method for unmanned aerial vehicle | |
| CN213398935U (en) | Miniaturized VTOL fixed wing unmanned aerial vehicle aeromagnetic detection system | |
| CN102431643A (en) | Automatic pilot of unmanned aerial vehicle | |
| CN105974494A (en) | Radio-sondage system based on dual-redundancy fixed wing unmanned aerial vehicle | |
| CN114384938B (en) | Unmanned aerial vehicle take-off and landing course correction method and system | |
| CN113968349B (en) | A photoelectric pod fixation and signal transmission device used on a sprinkler helicopter | |
| CN202345910U (en) | Fixed-height flight control system of fixed-wing unmanned aerial vehicle | |
| CN112498702A (en) | Electronic parachute opening control device, electronic parachute opening control method and parachute | |
| CN110011032B (en) | Retraction control device and method for airborne emergency communication system antenna | |
| CN115793705A (en) | An unmanned aerial vehicle-based ground wire lap wire health detection and defect diagnosis system | |
| CN207232391U (en) | A kind of low-altitude surveillance system based on Beidou satellite communication | |
| CN207173952U (en) | A kind of rotor wing unmanned aerial vehicle and its control system for flying control plate based on APM | |
| CN206848818U (en) | A kind of automatic jettison system of unmanned plane express delivery based on high in the clouds control | |
| CN112285805A (en) | Wind speed fluctuation turbulence sounding system | |
| CN207281311U (en) | A kind of atmosphere elements survey meter and atmosphere elements detection system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20210316 |