CN112596799A - Extensible universal airborne task management system - Google Patents
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Abstract
The invention discloses an extensible universal type machine-borne task management system, which comprises a main controller module, a power supply module, a load data interface module, a data transmission interface module, a storage downloading module and a reserved extension module, wherein the main controller module is used for storing a plurality of data; the main controller module comprises a first main controller module running with an unmanned aerial vehicle embedded operating system and a second main controller module running with a man-machine Windows operating system, and a task management module is installed on the main controller module and used for realizing a task management control function; the load data interface module is used for connecting one end with an external task load and connecting the other end with the data transmission interface module to convert and transmit data; one end of the data transmission interface module is used for connecting link equipment; the storage downloading module is used for storing and downloading task data; the reserved expansion module is used for carrying different load equipment according to requirements; the system is compatible with manned aircraft and unmanned aircraft systems, can be adapted according to different loading equipment requirements, and has strong expansion functions.
Description
Technical Field
The invention relates to the field of airplane load management, in particular to an extensible universal type airborne task management system.
Background
With the increasing types of special manned or unmanned aircraft products, the types of installed task loads are also increasing, and how to realize the comprehensive management of different types of task loads has more problems. In the prior art, different task loads are generally required to be provided with customized management devices required by the design of the management devices, so that the management of the task loads of the management devices is realized, when the multi-task loads are installed on the same aircraft platform, how to perform operations such as unified scheduling, management, interface conversion, data storage, data downloading and the like on task load equipment becomes very complicated, and more used equipment is needed. A generalized task load management system becomes very important, and the generalized goal is achieved from various aspects such as a load data interface, control and state feedback of task load, data storage, load data downloading and the like; the common task load system of the airplane consists of task loads such as an aerial camera, a photoelectric pod, a multifunctional radar, a laser fluorescence detector and the like, and a front-end detection unit and corresponding display and control equipment of the task loads. Limited by data link bandwidth, generally only one (or two) task load target information (such as images, traces and the like) is transmitted in real time, at the moment, gating equipment is needed to complete task load target information path selection, an airborne task management system is supposed to be adopted to complete the function, and the airborne task management system can realize the functions of accessing, managing, storing, displaying and controlling, downloading and the like of different types of airplanes and multi-task load equipment.
However, the design of the current airborne task management system is that two configurations of a windows operating system and an embedded operating system are separately designed, because the development difficulty of jointly compatible two operating system software into one task management computer is higher, the compatibility and stability requirements of the software and the hardware system are higher, the existing airborne task management system is not integrated, and the universality of the two operating systems cannot be realized.
Disclosure of Invention
The invention aims to provide an extensible universal type airborne task management system which has the function of being universal for manned aircrafts and unmanned aircrafts, can be adapted according to different load equipment requirements, does not need to be developed for different load equipment for the second time, and has a strong extension function.
The technical scheme for realizing the purpose of the invention is as follows: an extensible universal type machine-borne task management system comprises a main controller module, a power supply module, a load data interface module, a data transmission interface module, a storage downloading module and a reserved extension module;
the main controller module is connected with other modules and external equipment, and comprises a first main controller module running with an unmanned aerial vehicle embedded operating system and a second main controller module running with a man-machine Windows operating system, and is used for completing basic functions of a computer;
the power supply module supplies power to other modules;
the load data interface module is used for connecting an external task load at one end and accessing and distributing a load target data signal, and the other end is connected with the data transmission interface module to convert and transmit data;
one end of the data transmission interface module is used for connecting link equipment to finish access and distribution of remote control and telemetry data and inertial navigation data;
the storage downloading module is used for storing and downloading task data;
the reserved expansion module is used for carrying different load equipment installation expansion board cards according to requirements.
Further, the task load is one or more of an SAR radar, a photoelectric platform, a camera, an airborne voice radio and an answering machine.
Furthermore, the main controller module is connected with other modules through PCIe and SATA buses and is connected with external equipment through a network port or a serial port.
Further, the task management module comprises a task management unit, a load device monitoring unit, an access and distribution unit and a data storage and download unit;
the task management unit realizes the functions of uploading, loading, returning and modifying the task data;
the load equipment monitoring unit is used for controlling a load instruction, sending the control instruction to the task load equipment through the bus to realize load equipment control, receiving load working state data sent by the load data interface module through the bus, and monitoring the load working state and data, including initialization data and real-time flight data;
an access and distribution unit: the access, automatic distribution, audio signal management and conversion of signals and data of the load data interface module and the data transmission interface module, and the access, acquisition and transmission of bus data are realized;
the data storage and downloading unit is used for automatically storing videos, synchronous data and bus data and has a data downloading function.
Further, the task data comprises a task route planning, a mounting scheme, a load initialization parameter, an air traffic control equipment configuration parameter and a signal mapping relation.
Further, the uploading, loading, returning and modifying of the task data specifically comprises: the method comprises the following steps that a task management unit uploads or locally checks software to load task data through a data link before flying, can change the task data in the flying process, receives and analyzes a control instruction from a data transmission interface module, switches a control mode between a program control mode and an instruction mode according to the control instruction, and generates the control instruction according to a control authority, the control mode, a mounting scheme and a task route condition; when a plurality of independent data chains exist, managing the control authority of the ground control commands from different data chains; in the manned machine, the control authority from the ground load remote control command and the onboard display control system is managed.
Further, the real-time flight data in the load device monitoring unit comprises position, attitude and speed.
Further, the signals and data received and distributed by the access and distribution unit include: video signals, synchronization data, telemetry data, and pulse-per-second signals.
Further, the accessing and distributing unit specifically is: the method comprises the steps of configuring the mapping relation of video signal input and output, realizing automatic forwarding of video signals and composite data, configuring the mapping relation of analog audio signals and digital audio data input and output, completing automatic conversion of analog audio and digital audio, configuring the mapping relation of bus input and output, and realizing automatic forwarding of bus data.
Compared with the prior art, the invention has the following remarkable advantages: compared with a conventionally used airborne task management system, the system has the advantages that the general functions of the manned aircraft and the unmanned aircraft are added, the system can be adapted according to different load equipment requirements, secondary development is not needed for different load equipment, and the system has strong expansion functions, so that the design cost of products is reduced; the task management computer in the task management system adopts a modular design concept, has a simplified structure, is easy to manufacture, maintain and replace, has low failure rate and high safety and reliability, can reduce the consumption of airborne equipment on the resources such as the size, the weight, the power consumption and the like of the airplane, and is well applied to manned and unmanned airplanes.
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FIG. 1 is a block diagram of the system of the present invention.
Fig. 2 is a diagram of the architecture for connecting the system of the present invention to external devices.
FIG. 3 is a schematic diagram of the communication between the system and an external device according to the present invention.
Detailed Description
The extensible universal type machine-mounted task management system mainly comprises a task management hardware part (a task management computer) and a task management module.
The task management computer is an airborne control center for uniformly managing the aircraft task load equipment, performs bidirectional data communication with the task load equipment to realize load monitoring and control functions, monitors the load working state and provides working conditions required by the load equipment. The task management computer receives target data of all loads, optionally converts and distributes the target data, and transmits the target data to the ground command control system through the measurement and control system; this task management computer is mainly the universal platform who is applicable to there being man-machine and unmanned aerial vehicle, at the compatible two type aircraft demands of hardware aspect, realize switching fast between someone and unmanned aerial vehicle through loading airborne software, because unmanned aerial vehicle is far greater than there being man-machine to task management system's functional requirement, therefore, this universal type task management computer should design to unmanned aerial vehicle, it has man-machine user demand to cover, switching between someone mode and the unmanned mode is realized through loading different airborne software.
With reference to fig. 1, 2 and 3, the task management computer includes a main controller module 1 (computer module), a power module 2, a load data interface module 3, a data transmission interface module 4, a storage downloading module 5 and a reservation extension module 6;
the main controller module is connected with other modules and external equipment, the main controller module comprises a first main controller module running with an unmanned aerial vehicle embedded operating system and a second main controller module running with an unmanned aerial vehicle Windows operating system, and is used for completing basic functions of a computer, and meanwhile, the first main controller module and the second main controller module can be provided with different task management modules according to different airplane types and are used for realizing task management control functions;
a power supply module: providing power supply for the module of the whole task management computer;
the load data interface module is used for connecting an external task load at one end and accessing and distributing a load target data signal, and the other end is connected with the data transmission interface module to convert and transmit data;
the data transmission interface module: the system is used for connecting link equipment and completing access and distribution of remote control and remote measurement data and inertial navigation data;
the storage downloading module is used for storing and downloading load signals and bus data;
the reserved expansion module is used for carrying different load equipment installation expansion board cards according to requirements.
The system main controller module is connected with other modules to realize highest level control, mainly communicates with other modules through PCIe and SATA buses, and is connected with external equipment through a network port or a serial port (mainly applied to a man-machine part); one end of the load data interface module is connected with external load equipment to control the load equipment to work, meanwhile, the task and the equipment state data returned by the equipment are read, the other end of the load data interface module is connected with the data transmission interface data transmission module, and the data is sent to the airborne link terminal through the data transmission interface data transmission module to finish the data return to the ground station equipment.
The task management module comprises a task management unit, a load equipment monitoring unit, an access and distribution unit and a data storage and downloading unit;
a task management unit: the functions of uploading, loading, returning and modifying the task data are realized, and the capacity of uploading the task data through a data link before flight or locally detecting software and changing the task plan data in flight is realized; the mission plan data includes: the method comprises the following steps of (1) carrying out task route, mounting scheme, load initialization parameter, air traffic control equipment configuration parameter and signal mapping relation; receiving and analyzing control instructions from a link remote control and airborne display control system, switching between a program control mode and an instruction mode according to a control mode switching strategy, and generating the control instructions according to conditions such as control authority, a control mode, a mounting scheme, a task route and the like. When a plurality of independent data chains exist, managing the control authority of the ground control commands from different data chains; in the manned machine, the control authority from the ground load remote control command and the onboard display control system is managed.
The load equipment monitoring unit is used for controlling a load instruction, and sending the control instruction to the task load equipment through the bus to realize load equipment control; the state data sent by the task load is received through the bus, and load working state monitoring and load working data support are achieved, wherein the load working state monitoring and the load working data support comprise initialization data injection and real-time flight data, and the real-time flight data comprise position, attitude, speed and the like.
An access and distribution unit: the access, automatic distribution and conversion of signals and data of the load data interface module and the data transmission interface module are realized; the method comprises the steps of video signal access and automatic distribution, synchronous data access and automatic distribution (multiple input multiple output, configurable), audio signal management, remote control and remote measurement data access and automatic distribution, second pulse signal access and automatic distribution, bus data access, acquisition and transmission, data distribution control and video input and output mapping relation configuration, automatic video forwarding, automatic composite data forwarding, analog audio signal and digital audio signal input and output mapping relation configuration, automatic analog audio and digital audio conversion, bus input and output mapping relation configuration and automatic bus data forwarding.
A data storage unit: the video, the synchronous RS422 data and the bus data are automatically stored, and the data downloading function is achieved.
According to different airplane types of the airplane, the first main controller module and the second main controller module can select different software units from the task management module to be installed, and the system is applied in an unmanned aerial vehicle mode as follows: the task management computer has the same management function for task loads, the management function for an air management system and the power supply control function for load equipment are added, and the communication function of a display control console is omitted. The task management computer acquires the position and attitude information of the airplane through the flight control system, acquires target and state data of task loads such as a photoelectric platform, an SAR radar and the like through a video interface and a data transmission interface module, sends a control instruction, selectively converts and distributes the target data to an airborne measurement and control data chain for transmission, and receives a ground control instruction from the data chain. The task management computer has an analog-to-digital conversion function of conversation voice, is matched with an airborne radio station and a data chain to realize a relay air traffic control conversation function of the unmanned aerial vehicle, and is matched with an answering machine to realize an airplane information reporting function.
The system is applied in a man-machine mode as follows: the task management computer acquires airplane position and attitude information through a flight control system, acquires target and state data of task loads such as a photoelectric platform and an SAR through a video interface and a data interface, sends a control instruction, selectively converts and distributes the target data to an airborne measurement and control data chain for transmission, and receives a ground control instruction from the data chain.
Claims (9)
1. An extensible universal type machine-borne task management system is characterized by comprising a main controller module, a power supply module, a load data interface module, a data transmission interface module, a storage downloading module and a reserved extension module;
the main controller module is connected with other modules and external equipment, and comprises a first main controller module running with an unmanned aerial vehicle embedded operating system and a second main controller module running with a man-machine Windows operating system, and is used for completing basic functions of a computer;
the power supply module supplies power to other modules;
the load data interface module is used for connecting an external task load at one end and accessing and distributing a load target data signal, and the other end is connected with the data transmission interface module to convert and transmit data;
one end of the data transmission interface module is used for connecting link equipment to finish access and distribution of remote control and telemetry data and inertial navigation data;
the storage downloading module is used for storing and downloading task data;
the reserved expansion module is used for carrying different load equipment installation expansion board cards according to requirements.
2. The extensible universal machine-borne task management system according to claim 1, wherein the task load is one or more of a SAR radar, a photovoltaic platform, a camera, an onboard voice station, and a transponder.
3. The extensible generalized type on-board task management system of claim 1, wherein the main controller module is connected to other modules via PCIe and SATA buses, and to external devices via a network port or a serial port.
4. The extensible generalized type in-flight task management system of claim 1, wherein the task management module includes a task management unit, a load device monitoring unit, an access and distribution unit, and a data storage download unit;
the task management unit realizes the functions of uploading, loading, returning and modifying the task data;
the load equipment monitoring unit is used for controlling a load instruction, sending the control instruction to the task load equipment through the bus to realize load equipment control, receiving load working state data sent by the load data interface module through the bus, and monitoring the load working state and data, including initialization data and real-time flight data;
an access and distribution unit: the access, automatic distribution, audio signal management and conversion of signals and data of the load data interface module and the data transmission interface module, and the access, acquisition and transmission of bus data are realized;
the data storage and downloading unit is used for automatically storing videos, synchronous data and bus data and has a data downloading function.
5. The extensible generalized type on-board task management system of claim 4, wherein the task data includes mission route planning, mounting schemes, load initialization parameters, air traffic control equipment configuration parameters, signal mapping relationships.
6. The extensible universal machine-borne task management system according to claim 4, wherein the uploading, loading, returning, and modifying of the task data are specifically: the method comprises the following steps that a task management unit uploads or locally checks software to load task data through a data link before flying, can change the task data in the flying process, receives and analyzes a control instruction from a data transmission interface module, switches a control mode between a program control mode and an instruction mode according to the control instruction, and generates the control instruction according to a control authority, the control mode, a mounting scheme and a task route condition; when a plurality of independent data chains exist, managing the control authority of the ground control commands from different data chains; in the manned machine, the control authority from the ground load remote control command and the onboard display control system is managed.
7. The extensible generalized type on-board task management system of claim 4, wherein the real-time flight data in the load device monitoring unit includes position, attitude, and velocity.
8. The extensible generalized type on-board task management system of claim 4, wherein the signals and data accepted and distributed by the access and distribution unit include: video signals, synchronization data, telemetry data, and pulse-per-second signals.
9. The extensible generalized type on-board task management system of claim 8, wherein the access and distribution unit is specifically: the method comprises the steps of configuring the mapping relation of video signal input and output, realizing automatic forwarding of video signals and composite data, configuring the mapping relation of analog audio signals and digital audio data input and output, completing automatic conversion of analog audio and digital audio, configuring the mapping relation of bus input and output, and realizing automatic forwarding of bus data.
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| CN113359841A (en) * | 2021-06-29 | 2021-09-07 | 西北工业大学 | Unified driving model for unmanned aerial vehicle heterogeneous load equipment |
| CN113608467A (en) * | 2021-07-29 | 2021-11-05 | 西安超越申泰信息科技有限公司 | Unmanned aerial vehicle machine carries task manager realization device |
| CN113778643A (en) * | 2021-08-13 | 2021-12-10 | 中电科芜湖通用航空产业技术研究院有限公司 | Unmanned aerial vehicle task management computer software architecture system and configuration switching method |
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| CN114490500A (en) * | 2021-12-29 | 2022-05-13 | 西北工业大学 | Comprehensive intelligent flight control computing platform for smart application |
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| CN113359841A (en) * | 2021-06-29 | 2021-09-07 | 西北工业大学 | Unified driving model for unmanned aerial vehicle heterogeneous load equipment |
| CN113608467A (en) * | 2021-07-29 | 2021-11-05 | 西安超越申泰信息科技有限公司 | Unmanned aerial vehicle machine carries task manager realization device |
| CN113778643A (en) * | 2021-08-13 | 2021-12-10 | 中电科芜湖通用航空产业技术研究院有限公司 | Unmanned aerial vehicle task management computer software architecture system and configuration switching method |
| CN113922862A (en) * | 2021-09-16 | 2022-01-11 | 中国电子科技集团公司电子科学研究院 | Unmanned aerial vehicle synthesizes task management and control system |
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