CN109724467B - Joint debugging joint test system and method for space launching - Google Patents
Joint debugging joint test system and method for space launching Download PDFInfo
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- CN109724467B CN109724467B CN201810932922.4A CN201810932922A CN109724467B CN 109724467 B CN109724467 B CN 109724467B CN 201810932922 A CN201810932922 A CN 201810932922A CN 109724467 B CN109724467 B CN 109724467B
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Abstract
The invention relates to the technical field of target range communication, and discloses a joint debugging joint test system and method for space launching. Wherein, this system includes: the receiving device is used for receiving the transmitting and scheduling instruction sent by the command terminal; and the control device is connected with the receiving device and used for generating and outputting corresponding signals according to the emission scheduling instruction and a preset time sequence under the joint debugging working mode. Therefore, the corresponding signals can be sequentially and automatically generated and output without respectively and independently sending the corresponding scheduling passwords, and the condition that a commander forgets to send the scheduling passwords or mistakenly sends the scheduling passwords is avoided; in addition, the control device does not respond to the transmission scheduling command in the working mode of self-checking and transmission, and allows the controller to respond to the transmission scheduling command only in the mode of joint debugging and joint debugging.
Description
Technical Field
The invention relates to the technical field of target range communication, in particular to a joint debugging joint test system and method for space launching.
Background
In the space launching (such as missile test) task, multiple joint debugging joint test works are required to be carried out so as to check the working condition and the cooperative working condition of each system. For example, it includes: the method comprises the following steps of intra-system joint test, inter-system joint test, unidirectional joint debugging, general examination, first area co-training, whole area co-training, launching implementation and the like. In the joint debugging and joint testing process, the operations of takeoff zero signal inspection, theoretical trajectory inspection, comprehensive inspection, model flight and the like are completed according to the requirements of a task program. The takeoff zero signal is T0 information for short, is important information of missile test and space launching, and is time coding information generated by a takeoff contact signal (takeoff signal for short) of missiles and rockets by a target range communication system.
At present, when a transmitting field organizes these works, a commander needs to issue command and scheduling passwords such as 'five minutes equipment', 'one minute equipment', 'pull', 'take-off' and the like to each system through a command and scheduling system. The transmitting take-off zero time signal control console of the transmitting field communication system operates the pulling and take-off buttons of the transmitting take-off zero time signal control console according to the scheduling password of the commander, and the transmitting take-off zero time signal control console generates pulling buzz, take-off buzz and T0 information and sends the information to the outside. The signal console for transmitting the takeoff zero time is a T0 console for short, and is a device for converting the takeoff signal into standard Beijing time information.
Therefore, when the joint debugging joint test is carried out each time, the commander needs to respectively and successively send the corresponding scheduling passwords to the T0 console of the launching field communication system, and then the generation of 'pulling' buzz, 'take-off' buzz and T0 information can be correspondingly completed. That is, each operation requires the commander to separately send the corresponding scheduling password, for example, the commander sends the command scheduling passwords of "five minutes equipment", "one minute equipment", "dragging", and "take off" at the corresponding time. However, in such a manner, the commander forgets to send the scheduling password or mistakenly sends the scheduling password, and the joint debugging work of the transmitting field is seriously affected.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides a joint debugging joint test system and method for space launching, which can solve the problems in the prior art.
The technical solution of the invention is as follows: a joint debugging joint trial system for space launch, wherein the system comprises:
the receiving device is used for receiving the transmitting and scheduling instruction sent by the command terminal;
and the control device is connected with the receiving device and used for generating and outputting corresponding signals according to the emission scheduling instruction and a preset time sequence under the joint debugging working mode.
Preferably, the generating and outputting the corresponding signal according to the transmission scheduling instruction by the control device according to the predetermined time sequence in the joint debugging working mode includes:
generating and outputting a dragging prompt signal according to a first time in a preset time sequence;
and generating and outputting a takeoff prompt signal and a takeoff zero point signal according to a second moment in the preset time sequence, wherein the second moment is later than the first moment.
Preferably, the system further comprises a sound prompting device, which is used for sending out a dragging prompt tone according to the dragging prompt signal and sending out a takeoff prompt tone different from the dragging prompt tone according to the takeoff prompt signal.
Preferably, the receiving device is further configured to receive a link connection signal sent by a command terminal, and the control device is further configured to output a signal indicating that a link state is normal when the receiving device receives the link connection signal, and output a signal indicating that the link state is abnormal when the receiving device does not receive the link connection signal.
Preferably, the system further comprises a display device for displaying the transmission-related information, the transmission-related information including a transmission task code, real time, link status, countdown, and flight time.
The invention also provides a joint debugging joint test method for space launching, wherein the method comprises the following steps:
receiving a transmitting and scheduling instruction sent by a command terminal by using a receiving device;
and generating and outputting corresponding signals according to the emission scheduling instruction and a preset time sequence by using a control device in a joint debugging joint trial working mode.
Preferably, the generating and outputting the corresponding signal according to the transmission scheduling instruction according to the predetermined timing sequence in the joint debugging working mode includes:
generating and outputting a dragging prompt signal according to a first time in a preset time sequence;
and generating and outputting a takeoff prompt signal and a takeoff zero point signal according to a second moment in the preset time sequence, wherein the second moment is later than the first moment.
Preferably, the method further comprises the step of sending out a dragging prompt tone according to the dragging prompt signal and sending out a takeoff prompt tone different from the dragging prompt tone according to the takeoff prompt signal by utilizing a sound prompt device.
Preferably, the method further comprises:
receiving a link connection signal sent by a command terminal by using the receiving device;
and outputting a signal indicating that the link state is normal when the receiving means receives the link connection signal, and outputting a signal indicating that the link state is abnormal when the receiving means does not receive the link connection signal.
Preferably, the method further comprises displaying, with a display device, transmission-related information including a transmission task code, real time, link status, countdown, and time of flight.
Through the technical scheme, the receiving device can be used for receiving the transmitting and scheduling instruction sent by the command terminal, and the control device is used for generating and outputting the corresponding signal according to the transmitting and scheduling instruction according to the preset time sequence in the joint debugging joint testing working mode. Therefore, the corresponding signals can be sequentially and automatically generated and output without respectively and independently sending the corresponding scheduling passwords, and the condition that a commander forgets to send the scheduling passwords or mistakenly sends the scheduling passwords is avoided; and the control device does not respond to the transmission scheduling command in the working mode of self-checking and transmission, and allows the control device to respond to the transmission scheduling command only in the mode of joint debugging and joint debugging.
Drawings
The accompanying drawings, which are included to provide a further understanding of the embodiments of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention. It is obvious that the drawings in the following description are only some embodiments of the invention, and that for a person skilled in the art, other drawings can be derived from them without inventive effort.
Fig. 1 is a block diagram of a joint debugging joint test system for space launch according to an embodiment of the present invention;
fig. 2 is a flowchart of a joint debugging joint test method for space launch according to an embodiment of the present invention.
Detailed Description
Specific embodiments of the present invention will be described in detail below with reference to the accompanying drawings. In the following description, for purposes of explanation and not limitation, specific details are set forth in order to provide a thorough understanding of the present invention. However, it will be apparent to one skilled in the art that the present invention may be practiced in other embodiments that depart from these specific details.
It should be noted that, in order to avoid obscuring the present invention with unnecessary details, only the device structures and/or processing steps that are closely related to the scheme according to the present invention are shown in the drawings, and other details that are not so relevant to the present invention are omitted.
Fig. 1 is a block diagram of a joint debugging joint test system for space launch according to an embodiment of the present invention.
As shown in fig. 1, an embodiment of the present invention provides a joint debugging joint test system for space launch, where the system may include:
a receiving device 10, configured to receive a transmission scheduling instruction sent by a command terminal;
and the control device 12 is connected to the receiving device 10, and is configured to generate and output a corresponding signal according to the transmission scheduling instruction according to a predetermined time sequence in the joint debugging working mode, that is, the control device 12 responds to the transmission scheduling instruction only in the joint debugging working mode, and accordingly generates and outputs a corresponding signal.
That is, corresponding signals can be generated and output according to different time sequences in the joint debugging joint test working mode so as to be sent to the command control center.
The transmission scheduling instruction may be, for example, a predetermined length of time preparation instruction (e.g., a five-minute preparation instruction, a one-minute preparation instruction, etc.), and the control device may count down from the predetermined length of time (e.g., a five-minute count down) according to the predetermined length of time preparation instruction and generate and output a corresponding signal according to a predetermined timing.
Through the technical scheme, the receiving device can be used for receiving the transmitting and scheduling instruction sent by the command terminal, and the control device is used for generating and outputting the corresponding signal according to the transmitting and scheduling instruction according to the preset time sequence in the joint debugging joint testing working mode. Therefore, the corresponding signals can be sequentially and automatically generated and output without respectively and independently sending the corresponding scheduling passwords, and the condition that a commander forgets to send the scheduling passwords or mistakenly sends the scheduling passwords is avoided; and the control device does not respond to the transmission scheduling command in the working mode of self-checking and transmission, and allows the control device to respond to the transmission scheduling command only in the mode of joint debugging and joint debugging.
For example, the control device 12 may be a takeoff zero signal console (abbreviated as T0 console) of the transmission field communication system.
According to an embodiment of the present invention, the generating and outputting the corresponding signal according to the transmission scheduling instruction by the control device 12 according to the predetermined timing sequence in the joint debugging mode may include:
generating and outputting a dragging prompt signal according to a first time in a preset time sequence;
and generating and outputting a takeoff prompt signal and a takeoff zero signal (T0 signal for short) according to a second time in the preset time sequence, wherein the second time is later than the first time.
For example, the dragging prompt signal may be automatically generated at, for example, -30 seconds or-40 seconds (i.e., the first time instant); at 0 second (i.e., the second moment), the takeoff prompt signal and the T0 message are automatically generated and sent to the outside.
The predetermined time sequence can be configured in advance by those skilled in the art according to actual situations, and the present invention is not limited thereto.
According to an embodiment of the present invention, the system may further include a sound prompt device, configured to send a drag prompt tone according to the drag prompt signal and send a takeoff prompt tone different from the drag prompt tone according to the takeoff prompt signal.
For example, the sound prompt device may be a buzzer or a speaker. Taking a buzzer as an example, the buzzer can send out continuous buzzing sound according to the dragging prompt signal; for the purpose of distinction, the buzzer may sound with a certain time interval (i.e., a discontinuous beep) according to the takeoff prompt signal, and vice versa.
According to an embodiment of the present invention, the receiving apparatus 10 may be further configured to receive a link connection signal sent by a command terminal, and the control apparatus 12 may be further configured to output a signal indicating that a link state is normal if the receiving apparatus 10 receives the link connection signal, and output a signal indicating that a link state is abnormal if the link connection signal is not received.
That is, when the link state (for example, the connection state of the IP network) is normal, the receiving apparatus may receive the link connection signal sent by the command terminal in real time, otherwise, the receiving apparatus may not receive the link connection signal (at this time, due to the link abnormality, the receiving apparatus may not receive the transmission scheduling instruction sent by the command terminal, and accordingly, the subsequent operation may not be performed). Therefore, the link state can be judged according to whether the link connection signal sent by the command terminal in real time is received (namely, the link state is monitored in real time), and in case of abnormity, a signal indicating the abnormity of the link state is output so as to inform related staff to process in time, and then the link connection is recovered.
According to an embodiment of the invention, the system further comprises a display device for displaying transmission-related information, the transmission-related information comprising a transmission mission code, real-time (e.g. beijing time), link status (normal or abnormal), countdown, and time of flight (i.e. time of flight after takeoff).
Therefore, various types of transmitted information can be visually displayed.
Fig. 2 is a flowchart of a joint debugging joint test method for space launch according to an embodiment of the present invention.
As shown in fig. 2, an embodiment of the present invention provides a joint debugging joint test method for space launch, where the method may include:
s200, receiving a transmitting scheduling instruction sent by a command terminal by using a receiving device;
and S202, generating and outputting corresponding signals according to a preset time sequence according to the emission scheduling instruction by using a control device in a joint scheduling joint test working mode.
Through the technical scheme, the receiving device can be used for receiving the transmitting and scheduling instruction sent by the command terminal, and the control device is used for generating and outputting the corresponding signal according to the transmitting and scheduling instruction according to the preset time sequence in the joint debugging joint testing working mode. Therefore, the corresponding signals can be sequentially and automatically generated and output without respectively and independently sending the corresponding scheduling passwords, and the condition that a commander forgets to send the scheduling passwords or mistakenly sends the scheduling passwords is avoided; and the control device does not respond to the transmission scheduling command in the working mode of self-checking and transmission, and allows the control device to respond to the transmission scheduling command only in the mode of joint debugging and joint debugging.
According to an embodiment of the present invention, the generating and outputting the corresponding signal according to the transmission scheduling instruction according to the predetermined timing sequence in the joint debugging mode in S202 may include:
generating and outputting a dragging prompt signal according to a first time in a preset time sequence;
and generating and outputting a takeoff prompt signal and a takeoff zero point signal according to a second moment in the preset time sequence, wherein the second moment is later than the first moment.
According to an embodiment of the invention, the method may further include sending out a drag prompt tone according to the drag prompt signal and sending out a takeoff prompt tone different from the drag prompt tone according to the takeoff prompt signal by using an acoustic prompt device.
According to an embodiment of the invention, the method may further comprise:
receiving a link connection signal sent by a command terminal by using the receiving device;
and outputting a signal indicating that the link state is normal when the receiving means receives the link connection signal, and outputting a signal indicating that the link state is abnormal when the receiving means does not receive the link connection signal.
According to an embodiment of the present invention, the method may further include displaying, with a display device, transmission-related information including a transmission task code, a real-time (e.g., beijing time), a link status, a countdown, and a flight time.
The method described in fig. 2 corresponds to the system described in fig. 1, and for a specific example, reference may be made to the description of the system described in fig. 1, which is not described herein again.
Features that are described and/or illustrated above with respect to one embodiment may be used in the same way or in a similar way in one or more other embodiments and/or in combination with or instead of the features of the other embodiments.
It should be emphasized that the term "comprises/comprising" when used herein, is taken to specify the presence of stated features, integers, steps or components but does not preclude the presence or addition of one or more other features, integers, steps, components or groups thereof.
The above systems and methods of the present invention may be implemented by hardware, or by a combination of hardware and software. The present invention relates to a computer-readable program which, when executed by a logic section, enables the logic section to realize the above-described apparatus or constituent section, or to realize the above-described various methods or steps. The present invention also relates to a storage medium such as a hard disk, a magnetic disk, an optical disk, a DVD, a flash memory, or the like, for storing the above program.
The many features and advantages of these embodiments are apparent from the detailed specification, and thus, it is intended by the appended claims to cover all such features and advantages of these embodiments which fall within the true spirit and scope thereof. Further, since numerous modifications and changes will readily occur to those skilled in the art, it is not desired to limit the embodiments of the invention to the exact construction and operation illustrated and described, and accordingly, all suitable modifications and equivalents may be resorted to, falling within the scope thereof.
The invention has not been described in detail and is in part known to those of skill in the art.
Claims (8)
1. A joint debugging joint trial system for space launch, the system comprising:
the receiving device is used for receiving the transmitting and scheduling instruction sent by the command terminal;
the control device is connected with the receiving device and used for generating and outputting corresponding signals according to the emission scheduling instruction and a preset time sequence under the joint debugging working mode,
the control device generates and outputs corresponding signals according to the emission scheduling instruction according to a preset time sequence under the joint debugging joint test working mode, and the control device comprises:
generating and outputting a dragging prompt signal according to a first time in a preset time sequence;
and generating and outputting a takeoff prompt signal and a takeoff zero point signal according to a second moment in the preset time sequence, wherein the second moment is later than the first moment.
2. The system as claimed in claim 1, further comprising an audio alert device for emitting an alert drag tone in response to the alert drag signal and an alert takeoff tone different from the alert drag tone in response to the alert takeoff signal.
3. The system according to claim 1, wherein the receiving means is further configured to receive a link connection signal sent by a command terminal, and the control means is further configured to output a signal indicating that the link state is normal if the receiving means receives the link connection signal, and output a signal indicating that the link state is abnormal if the link connection signal is not received.
4. The system of claim 3, further comprising a display device for displaying transmission-related information, the transmission-related information including a transmission mission code, real time, link status, countdown, and time of flight.
5. A joint debugging joint test method for space launching, characterized in that the method comprises:
receiving a transmitting and scheduling instruction sent by a command terminal by using a receiving device;
generating and outputting corresponding signals according to a preset time sequence according to the emission scheduling instruction by using a control device in a joint debugging joint test working mode;
generating and outputting corresponding signals according to the emission scheduling instruction and a preset time sequence under the joint debugging working mode comprises the following steps:
generating and outputting a dragging prompt signal according to a first time in a preset time sequence;
and generating and outputting a takeoff prompt signal and a takeoff zero point signal according to a second moment in the preset time sequence, wherein the second moment is later than the first moment.
6. The method of claim 5, further comprising emitting a drag alert tone in response to the drag alert signal and emitting a takeoff alert tone different from the drag alert tone in response to the takeoff alert signal using an audible alert device.
7. The method of claim 5, further comprising:
receiving a link connection signal sent by a command terminal by using the receiving device;
and outputting a signal indicating that the link state is normal when the receiving means receives the link connection signal, and outputting a signal indicating that the link state is abnormal when the receiving means does not receive the link connection signal.
8. The method of claim 7, further comprising displaying, with a display device, transmission-related information including a transmission mission code, real time, link status, countdown, and time of flight.
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| CN113780736B (en) * | 2021-08-10 | 2024-05-07 | 中国电子科技集团公司第二十七研究所 | Automatic joint debugging method for active section measurement and control multi-station combination |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202455368U (en) * | 2012-01-19 | 2012-09-26 | 北京宇航系统工程研究所 | Ground real-time network system for carrier rocket |
| CN103090724A (en) * | 2013-01-21 | 2013-05-08 | 北京航空航天大学 | Solid-liquid power sounding rocket land launching sequential control system |
| CN203658822U (en) * | 2013-12-30 | 2014-06-18 | 北京航天斯达新技术装备公司 | Command and control system of aerospace landing test site |
| CN104296596A (en) * | 2014-08-29 | 2015-01-21 | 北京宇航系统工程研究所 | Carrier rocket testing and launch control procedure command system and method |
| CN205228283U (en) * | 2015-12-21 | 2016-05-11 | 新疆维吾尔自治区人工影响天气办公室 | Rocket firing system |
| CN106941251A (en) * | 2016-01-05 | 2017-07-11 | 西安航天动力技术研究所 | A kind of initial firing current observation circuit for launching control equipment |
-
2018
- 2018-08-16 CN CN201810932922.4A patent/CN109724467B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202455368U (en) * | 2012-01-19 | 2012-09-26 | 北京宇航系统工程研究所 | Ground real-time network system for carrier rocket |
| CN103090724A (en) * | 2013-01-21 | 2013-05-08 | 北京航空航天大学 | Solid-liquid power sounding rocket land launching sequential control system |
| CN203658822U (en) * | 2013-12-30 | 2014-06-18 | 北京航天斯达新技术装备公司 | Command and control system of aerospace landing test site |
| CN104296596A (en) * | 2014-08-29 | 2015-01-21 | 北京宇航系统工程研究所 | Carrier rocket testing and launch control procedure command system and method |
| CN205228283U (en) * | 2015-12-21 | 2016-05-11 | 新疆维吾尔自治区人工影响天气办公室 | Rocket firing system |
| CN106941251A (en) * | 2016-01-05 | 2017-07-11 | 西安航天动力技术研究所 | A kind of initial firing current observation circuit for launching control equipment |
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