CN117437705A - Flight target detection control system and device - Google Patents
Flight target detection control system and device Download PDFInfo
- Publication number
- CN117437705A CN117437705A CN202210844366.1A CN202210844366A CN117437705A CN 117437705 A CN117437705 A CN 117437705A CN 202210844366 A CN202210844366 A CN 202210844366A CN 117437705 A CN117437705 A CN 117437705A
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- power supply
- initiating explosive
- explosive device
- time sequence
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- 238000001514 detection method Methods 0.000 title claims abstract description 22
- 238000012360 testing method Methods 0.000 claims abstract description 48
- 239000002360 explosive Substances 0.000 claims abstract description 47
- 230000000977 initiatory effect Effects 0.000 claims abstract description 47
- 238000012544 monitoring process Methods 0.000 claims abstract description 32
- 238000013500 data storage Methods 0.000 claims abstract description 12
- 238000005259 measurement Methods 0.000 claims abstract description 12
- 238000004891 communication Methods 0.000 claims abstract description 11
- 230000003750 conditioning effect Effects 0.000 claims abstract description 10
- 238000002955 isolation Methods 0.000 claims abstract description 10
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 8
- 238000007726 management method Methods 0.000 claims abstract description 8
- 238000000926 separation method Methods 0.000 claims description 10
- 238000000605 extraction Methods 0.000 claims description 4
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000011160 research Methods 0.000 claims description 3
- 230000004044 response Effects 0.000 claims description 3
- 230000006870 function Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
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- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME 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
- G07C5/00—Registering or indicating the working of vehicles
- G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
- G07C5/0841—Registering performance data
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Alarm Systems (AREA)
Abstract
The invention discloses a flight target detection control system and device, comprising a lithium battery, a ground voltage-stabilized power supply, a power supply switching unit, a power supply isolation unit, a power supply management unit, a voltage monitoring unit, a temperature monitoring unit, a switching value input signal conditioning unit, an Inertial Measurement Unit (IMU), a storage unit, a time sequence control unit, a time sequence stoping unit, an initiating explosive device online test unit, an Ethernet communication unit, an external data storage interface, an online debugging unit and a microcontroller unit, wherein the power supply switching of the lithium battery and the ground voltage-stabilized power supply, the power supply voltage monitoring, the internal temperature monitoring, the equipment state and time sequence acquisition, the motion state monitoring, the information storage management, the motion time sequence control and acquisition, the initiating explosive device state test, the network communication, the data backup and the online program refreshing can be realized.
Description
Technical Field
The invention relates to a flight target detection control system and a device, and belongs to the technical field of electrical equipment control.
Background
The flight target detection control system and the flight target detection control device are the minimum control system for controlling the flight target to finish the specified operation, mainly finish the operations of flight target measurement information acquisition, flight attitude recording, control signal time sequence recording, stope control signal, initiating explosive device online test and the like, judge whether the flight target operates according to the specified signal according to the stored information, and provide data support for subsequently improving the execution accuracy and efficiency of the flight target.
Disclosure of Invention
Aiming at the application, the invention provides a flight target detection control system and a device, and the system can complete the following functions: (1) realizing the power supply switching between the ground and the flying target according to the instruction; (2) collecting measurement information, such as power supply voltage monitoring, internal temperature monitoring, equipment state and time sequence collection and motion state monitoring; (3) real-time recording, reading and storing flight target data; (4) monitoring signals such as discrete signals of a flying target, in-place actions and the like; (5) outputting an external timing control signal; (6) on-line testing and protecting functions of initiating explosive devices; (7) data backup and online program refreshing.
In order to achieve the above purpose, the invention provides a flight target detection control system and device, comprising a lithium battery (1), a ground stabilized voltage supply (2), a power supply switching unit (3), a power supply isolation unit (4), a power supply management unit (5), a voltage monitoring unit (6), a temperature monitoring unit (7), a switching value input signal conditioning unit (8), an inertial measurement unit (9), an internal storage unit (10), a microcontroller (11), a time sequence control unit (12), a time sequence extraction unit (13), an initiating explosive device online test unit (14), an initiating explosive device test protection unit (15), an Ethernet communication unit (16), an external data storage interface (17) and an online program upgrading unit (18);
preferably, the lithium battery (1) and the ground stabilized voltage supply (2) are connected with the power supply switching unit (3), and the power supply switching unit (3) realizes power supply protection and power supply switching of the flying object.
Preferably, the power supply isolation unit (4) is connected with the power supply switching unit (3) to isolate the power supply part from the system power supply;
preferably, the power supply management unit (5) is connected with the power supply isolation unit (4) to realize the voltage conversion and power supply monitoring required by the system;
preferably, the voltage monitoring unit (6) monitors the voltages of the power supply front end, the power supply rear end, the external power supply output end and the initiating explosive device bus end;
preferably, the temperature monitoring unit (7) is used for monitoring the temperature of the system;
preferably, the switching value input signal conditioning unit (8) is used for receiving switching value signals such as an externally input timing signal, a flying target separation signal, an in-place signal and the like;
preferably, the inertial measurement unit (9) is used for recording attitude information of a flying target;
preferably, the internal storage unit (10) is used for storing self-checking information, monitored voltage information, temperature information, flying target attitude information, external time system signal receiving time, flying target separation time, in-place signals and other information.
Preferably, the voltage monitoring unit (6), the temperature monitoring unit (7), the switching value input signal conditioning unit (8), the inertial measurement unit (9), the internal storage unit (10), the time sequence control unit (12), the time sequence stoping unit (13), the initiating explosive device online test unit (14), the Ethernet communication unit (16), the external data storage interface (17) and the online program upgrading unit (18) are all connected with the microcontroller (11);
preferably, the time sequence control unit (12) outputs a designated time sequence control signal through research and judgment according to an external time system signal, a flying target separation signal, an in-place signal and the like;
preferably, the timing extraction unit (13) is used for judging whether the output timing of the timing control unit is correct;
preferably, the initiating explosive device online test unit (14) is connected with the time sequence control unit (12) and the initiating explosive device test protection unit (15) to complete initiating explosive device online test;
and the initiating explosive device testing protection unit (15) limits the online testing current of the initiating explosive device and reduces the damage risk of an online testing circuit of the initiating explosive device.
Preferably, the ethernet communication unit (16) is configured to receive a ground console command, and send a response frame and a data frame to the ground console.
Preferably, the external data storage interface (17) is used for connecting external solid-state memory data needing to be stored.
Preferably, the online program upgrading unit (18) is used for online completing programming.
Preferably, a flying object detection control system and device can complete local and self battery powered switching by instructions.
Preferably, the flight object detection control system and the flight object detection control device can monitor an external timing system signal, a flight object separation signal, an in-place signal and the like to output corresponding timing control signals.
Preferably, the flight target detection control system and device comprise a 5-path initiating explosive device online test unit, and the initiating explosive device test protection unit can limit the current of an initiating explosive device test circuit and reduce the damage risk of the initiating explosive device online test circuit.
Preferably, the internal memory of the flight target detection control system and the device is 2 storage spaces which are mutually backed up, one is a fixed storage area for storing data which are fixedly stored for a long time, and the other is an instant storage area for recording data acquired in the test process.
Preferably, the flight target detection control system and the device are characterized in that the program upgrading can be finished on line through an external data storage interface.
The invention has the beneficial effects that:
the flight target detection control system and the flight target detection control device provided by the invention can realize the power supply switching between the ground and the flight target according to the instruction; the data such as measurement information, flight attitude, time system signals, in-place signal output time and the like can be acquired, stored and read in real time; the signals such as discrete signals, in-place actions and the like of the flying targets can be monitored; an external timing control signal may be output; the device has the functions of online testing and protecting 5 paths of initiating explosive devices; the memory is 2 storage spaces which are mutually backed up.
Drawings
FIG. 1 is a system diagram of a preferred embodiment of a flying-target detection control system and apparatus according to the present invention
Detailed Description
The present invention will be further described with reference to examples and drawings, but embodiments of the present invention are not limited thereto, in order to make the technical solutions of the present invention more clear and clear to those skilled in the art.
As shown in fig. 1, the flight target detection control system and device provided in this embodiment include a lithium battery (1), a ground regulated power supply (2), a power supply switching unit (3), a power supply isolation unit (4), a power supply management unit (5), a voltage monitoring unit (6), a temperature monitoring unit (7), a switching value input signal conditioning unit (8), an inertial measurement unit (9), an internal storage unit (10), a microcontroller (11), a time sequence control unit (12), a time sequence extraction unit (13), an initiating explosive device online test unit (14), an initiating explosive device test protection unit (15), an ethernet communication unit (16), an external data storage interface (17) and an online program upgrading unit (18);
in the embodiment, the lithium battery (1) and the ground stabilized voltage supply (2) are connected with the power supply switching unit (3), and the power supply switching unit (3) realizes power supply protection and power supply switching of a flying target.
In the embodiment, the power supply isolation unit (4) is connected with the power supply switching unit (3) to isolate the power supply part from the system power supply;
in the embodiment, the power supply management unit (5) is connected with the power supply isolation unit (4) to realize voltage conversion and power supply monitoring required by the system;
in the embodiment, the voltage monitoring unit (6) monitors the voltages of the power supply front end, the power supply rear end, the external power supply output end and the initiating explosive device bus end;
in this embodiment, the temperature monitoring unit (7) is configured to monitor a temperature of the system;
in this embodiment, the switching value input signal conditioning unit (8) is configured to receive switching value signals such as a timing signal, a flight target separation signal, and an in-place signal that are input from the outside;
in this embodiment, the inertial unit (9) is configured to record attitude information of a flight target;
in this embodiment, the internal storage unit (10) is configured to store information such as self-checking information, monitored voltage information, temperature information, flight target attitude information, external time system signal receiving time, flight target separation time, and in-place signal.
In the embodiment, a voltage monitoring unit (6), a temperature monitoring unit (7), a switching value input signal conditioning unit (8), an inertial measurement unit (9), an internal storage unit (10), a time sequence control unit (12), a time sequence stoping unit (13), an initiating explosive device online test unit (14), an Ethernet communication unit (16), an external data storage interface (17) and an online program upgrading unit (18) are all connected with a microcontroller (11);
in this embodiment, the timing control unit (12) outputs a specified timing control signal through a research and judgment according to an external timing signal, a flight object separation signal, an in-place signal, and the like;
in this embodiment, the timing recovery unit (13) is configured to determine whether the output timing of the timing control unit is correct;
in the embodiment, the initiating explosive device online test unit (14) is connected with the time sequence control unit (12) and the initiating explosive device test protection unit (15) to complete initiating explosive device online test;
in this embodiment, the initiating explosive device testing protection unit (15) limits the online testing current of the initiating explosive device, and reduces the risk of damage to the online testing circuit of the initiating explosive device.
In this embodiment, the ethernet communication unit (16) is configured to receive a ground console command, and send a response frame and a data frame to the ground console.
In this embodiment, the external data storage interface (17) is used to connect with external solid-state memory data to be stored.
In this embodiment, the online program upgrade unit (18) is configured to complete programming online.
In this embodiment, local and self battery powered switching can be accomplished by instruction.
In this embodiment, the external timing signal, the flying target separating signal, the in-place signal, and the like may be monitored to output the corresponding timing control signal.
In this embodiment, the on-line testing device comprises a 5-path initiating explosive device on-line testing unit, and the initiating explosive device testing protection unit can limit the current of the initiating explosive device testing circuit and reduce the damage risk of the initiating explosive device on-line testing circuit.
In this embodiment, the internal memory is 2 storage spaces that are backup to each other, one is a fixed storage area, and stores data that is fixedly stored for a long time, and the other is an instant storage area, which is used for recording data collected in the test process.
In this embodiment, the program upgrade can be completed online through the external data storage interface.
The above description is merely a further embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art will be able to apply equivalents and modifications according to the technical solution and the concept of the present invention within the scope of the present invention disclosed in the present invention.
Claims (6)
1. A flight target detection control system and device is characterized in that: the system comprises a lithium battery (1), a ground stabilized voltage supply (2), a power supply switching unit (3), a power supply isolation unit (4), a power supply management unit (5), a voltage monitoring unit (6), a temperature monitoring unit (7), a switching value input signal conditioning unit (8), an inertial measurement unit (9), an internal storage unit (10), a microcontroller (11), a time sequence control unit (12), a time sequence stoping unit (13), an initiating explosive device online test unit (14), an initiating explosive device test protection unit (15), an Ethernet communication unit (16), an external data storage interface (17) and an online program upgrading unit (18);
the lithium battery (1) and the ground stabilized voltage supply (2) are connected with the power supply switching unit (3), and the power supply switching unit (3) realizes power supply protection and power supply switching of a flying target.
The power supply isolation unit (4) is connected with the power supply switching unit (3) to isolate a power supply part from a system power supply;
the power supply management unit (5) is connected with the power supply isolation unit (4) to realize voltage conversion and power supply monitoring required by the system;
the voltage monitoring unit (6) monitors the voltage of the power supply front end, the power supply rear end, the external power supply output end and the initiating explosive device bus end;
the temperature monitoring unit (7) is used for monitoring the temperature of the system;
the switching value input signal conditioning unit (8) is used for receiving switching value signals such as timing system signals, flight target separation signals, in-place signals and the like which are input from the outside;
the inertial measurement unit (9) is used for recording attitude information of a flying target;
the internal storage unit (10) is used for storing self-checking information, monitored voltage information, temperature information, flight target attitude information, external time system signal receiving time, flight target separation time, in-place signals and other information.
The voltage monitoring unit (6), the temperature monitoring unit (7), the switching value input signal conditioning unit (8), the inertial measurement unit (9), the internal storage unit (10), the time sequence control unit (12), the time sequence stoping unit (13), the initiating explosive device online test unit (14), the Ethernet communication unit (16), the external data storage interface (17) and the online program upgrading unit (18) are all connected with the microcontroller (11);
the time sequence control unit (12) outputs a designated time sequence control signal through research and judgment according to an external time system signal, a flying target separation signal, an in-place signal and the like;
the time sequence extraction unit (13) is used for judging whether the output time sequence of the time sequence control unit is correct;
the initiating explosive device online test unit (14) is connected with the time sequence control unit (12) and the initiating explosive device test protection unit (15) to complete initiating explosive device online test;
and the initiating explosive device testing protection unit (15) limits the online testing current of the initiating explosive device and reduces the damage risk of an online testing circuit of the initiating explosive device.
The Ethernet communication unit (16) is used for receiving the ground console instruction and sending response frames and data frames to the ground console.
The external data storage interface (17) is used for connecting external solid-state memory data needing to be stored.
The online program upgrading unit (18) is used for completing programming online.
2. The flying object detection control system and apparatus according to claim 1, wherein local and self battery powered switching is accomplished by command.
3. The system and apparatus according to claim 1, wherein the external timing signal, the separated signal, the in-place signal, etc. are monitored to output corresponding timing control signals.
4. The flying object detection control system and device according to claim 1, wherein the flying object detection control system comprises a 5-path initiating explosive device on-line test unit, and the initiating explosive device test protection unit can limit the current of an initiating explosive device test circuit and reduce the damage risk of the initiating explosive device on-line test circuit.
5. The flying object detecting and controlling system and device as claimed in claim 1, wherein the internal memory is 2 storage spaces backed up each other, one is a fixed storage area for storing data fixedly stored for a long time, and the other is an instant storage area for recording data collected during the test.
6. The flying object detecting and controlling system and device as claimed in claim 1, wherein the program refreshing can be accomplished on-line by an on-line program upgrading unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210844366.1A CN117437705A (en) | 2022-07-12 | 2022-07-12 | Flight target detection control system and device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210844366.1A CN117437705A (en) | 2022-07-12 | 2022-07-12 | Flight target detection control system and device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN117437705A true CN117437705A (en) | 2024-01-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210844366.1A Pending CN117437705A (en) | 2022-07-12 | 2022-07-12 | Flight target detection control system and device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN117437705A (en) |
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2022
- 2022-07-12 CN CN202210844366.1A patent/CN117437705A/en active Pending
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