On-orbit spacecraft sensitive shortcut operation control planning mode design method and system
Through the "two-layer planning, phased iteration" design of the operation control planning process of the in-orbit spacecraft, the problem that the operation control planning process in the existing technology is difficult to meet multiple constraints, and efficient and agile scientific detection task planning is achieved, and task efficiency and safety are improved.
Patent Information
- Application Number
- CN202510371420.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-27
- Publication Date
- 2025-07-18
AI Technical Summary
The operation control planning process of the existing technology in-orbit spacecraft is difficult to operate effectively on a wide range of time scales and cannot meet multiple constraints, resulting in insufficient efficiency and safety of scientific detection tasks.
Adopt the design strategy of "two-layer planning, phased iteration" to determine the spacecraft operation control planning process design strategy and establish an information interaction model to ensure the efficient and agility of the operation control planning process, covering the entire process from scientific detection proposals to scientific detection sequence implementation planning.
It realizes efficient and agility in the operation control planning process of in-orbit spacecraft, ensures the safety and accuracy of scientific detection tasks, meets multiple constraints, and improves the efficiency of scientific detection.
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Figure CN120337519A_ABST
Abstract
Description
Background Art
[0002] The operation and control planning method of on-orbit spacecraft determines the final output efficiency of its achievements. On April 24, 1990, the United States deployed the Hubble Space Telescope in a low Earth orbit. Since it operates outside the Earth's atmosphere, avoiding the interference of the atmosphere, it has achieved results that ground-based telescopes cannot match. On December 25, 2021, the United States deployed the James Webb Space Telescope in the working orbit of the Sun-Earth Lagrangian L2 point, 1.5 million kilometers away from the Earth. The James Webb Space Telescope is the new generation of orbiting infrared observatory of the National Aeronautics and Space Administration (NASA) of the United States. It is the largest and most powerful space telescope ever built, with a primary mirror diameter of about 6.5 meters. It is a complement and extension of the Hubble Space Telescope, exploring the universe with a longer wavelength coverage and higher sensitivity. Webb will study every stage of the history of the universe, from the inner solar system to the most distant detectable galaxies in the early universe, and explore a wide range of scientific questions to help us understand the origin of the universe and our place in it.
[0003] An important technology for on-orbit spacecraft to implement space mission exploration is the design of the operation and control planning process. Designing a reasonable scientific exploration planning process can produce efficient scientific exploration results and bring extremely high scientific benefits. The operation and control planning process must operate effectively on a wide time scale, formulate a detection implementation plan that meets all scientific exploration constraints, handle and avoid emergency situations, and generate safe and accurate scientific exploration control sequence instructions.
[0004] In the long-term on-orbit scientific exploration mission of a spacecraft, multiple constraint conditions such as the attitude adjustment characteristics of the platform, energy constraints, space environment conditions, TT&C resource coverage constraints, and orbital regions need to be considered; generally, the main systems (institutions) involved in spacecraft operation and control planning include the operation management center (management institution), ground operation and control center, spacecraft platform system (platform management), and spacecraft scientific exploration system (scientific exploration planning). According to the characteristics of on-orbit scientific exploration of spacecraft, an agile operation and control planning process for spacecraft is designed. Summary of the Invention
[0005] The present application provides a method and system for designing an agile operation and control planning mode of an on-orbit spacecraft to ensure the high efficiency and agility of the implementation of the operation and control planning process.
[0006] In the first aspect, a method for designing an agile operation and control planning mode of an on-orbit spacecraft is provided, including the following steps:
[0007] Determine the design strategy of the spacecraft operation and control planning process;
[0008] Design the operation and control planning process;
[0009] Establish an information interaction model between the operation and control planning implementation systems;
[0010] Determine the implementation method of the operation and control planning process.
[0011] In the above technical solution, by determining the design strategy of the spacecraft operation and control planning process; designing the operation and control planning process; establishing an information interaction model between operation and control planning implementation systems; determining the implementation method of the operation and control planning process; the operation and control planning process adopts a "two-layer planning, phased iteration" design strategy, establishing a step-by-step information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process; designing the upload implementation planning stage from the scientific exploration proposal to the scientific exploration sequence, covering the entire process of operation and control planning for carrying out scientific exploration tasks.
[0012] In a specific and feasible implementation plan, formulate the design strategy of the operation and control planning process in a hierarchical iteration manner.
[0013] In a specific and feasible implementation plan, based on the hierarchical design strategy, determine the operation and control planning process according to the planning process nodes.
[0014] In a specific and feasible implementation plan, establish an information interaction model for the operation and control planning interface, and establish an information interface interaction model in a step-by-step manner.
[0015] In a specific and feasible implementation plan, based on the interface information interaction model, convert the planning process information into an executable configuration file model to implement the final planning result.
[0016] In a specific and feasible implementation plan, formulate the design strategy of the planning process from the top layer and determine the planning design constraints.
[0017] In a specific and feasible implementation plan, based on the control planning process design strategy, design an agile operation and control planning process for on-orbit implementation of scientific exploration tasks; based on the operation and control planning process, determine the scientific exploration operation and control implementation and information interaction content.
[0018] In the second aspect, an agile operation and control planning mode design system for on-orbit spacecraft is provided, including:
[0019] An operation and control planning process design strategy module for determining the design strategy of the spacecraft operation and control planning process;
[0020] An operation and control planning process module for designing the operation and control planning process;
[0021] An information interaction model module for establishing an information interaction model between operation and control planning implementation systems;
[0022] An implementation method module for determining the implementation method of the operation and control planning process.
[0023] In the above technical solution, by determining the design strategy of the spacecraft operation and control planning process; designing the operation and control planning process; establishing an information interaction model between the operation and control planning implementation systems; determining the implementation method of the operation and control planning process; the operation and control planning process adopts a "two-layer planning, phased iteration" design strategy, establishing a step-by-step progressive information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process; designing an upload implementation planning stage from the scientific exploration proposal to the scientific exploration sequence, covering the entire process of the operation and control planning for carrying out scientific exploration tasks.
[0024] In a third aspect, an electronic device is provided. The electronic device includes a processor, the processor is coupled with a memory, and at least one computer program is stored in the memory. The at least one computer program is loaded and executed by the processor so that the electronic device implements any one of the on-orbit spacecraft agile operation and control planning mode design methods.
[0025] In the above technical solution, by determining the design strategy of the spacecraft operation and control planning process; designing the operation and control planning process; establishing an information interaction model between the operation and control planning implementation systems; determining the implementation method of the operation and control planning process; the operation and control planning process adopts a "two-layer planning, phased iteration" design strategy, establishing a step-by-step progressive information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process; designing an upload implementation planning stage from the scientific exploration proposal to the scientific exploration sequence, covering the entire process of the operation and control planning for carrying out scientific exploration tasks.
[0026] In a fourth aspect, a computer-readable storage medium is provided. At least one computer program is stored in the computer-readable storage medium. The at least one computer program is loaded and executed by a processor so that the computer-readable storage medium implements any one of the on-orbit spacecraft agile operation and control planning mode design methods.
[0027] In the above technical solution, by determining the design strategy of the spacecraft operation and control planning process; designing the operation and control planning process; establishing an information interaction model between the operation and control planning implementation systems; determining the implementation method of the operation and control planning process; the operation and control planning process adopts a "two-layer planning, phased iteration" design strategy, establishing a step-by-step progressive information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process; designing an upload implementation planning stage from the scientific exploration proposal to the scientific exploration sequence, covering the entire process of the operation and control planning for carrying out scientific exploration tasks. BRIEF DESCRIPTION OF THE DRAWINGS
[0028] Figure 1 It is a flowchart of the on-orbit spacecraft agile operation and control planning mode design method provided by the embodiment of the present application;
[0029] Figure 2It is a structural block diagram of the on-orbit spacecraft agile operation and control planning mode design system provided by the embodiment of the present application;
[0030] Figure 3 It is a planning information flow diagram provided by the embodiment of the present application;
[0031] Figure 4 It is a schematic diagram of the hierarchical planning of the operation and control strategy provided by the embodiment of the present application;
[0032] Figure 5 It is a schematic diagram of the establishment of the operation and control planning process provided by the embodiment of the present application;
[0033] Figure 6 It is a schematic diagram of the operation and control planning information interaction model (weekly) provided by the embodiment of the present application;
[0034] Figure 7 It is a schematic diagram of the implementation process of the operation and control planning result provided by the embodiment of the present application. Detailed implementation manners
[0035] The present application will be further described in detail below with reference to the drawings and embodiments. Through these descriptions, the features and advantages of the present application will become more clearly defined.
[0036] The special term "exemplary" here means "serving as an example, embodiment or illustrative". Any embodiment described as "exemplary" here does not have to be construed as superior or better than other embodiments. Although various aspects of the embodiments are shown in the drawings, the drawings do not have to be drawn to scale unless otherwise specified.
[0037] In addition, the technical features involved in different embodiments of the present application described below can be combined with each other as long as they do not conflict with each other.
[0038] To facilitate the understanding of the on-orbit spacecraft agile operation and control planning mode design method and system provided by the embodiments of the present application, its application scenario will be described first. The on-orbit spacecraft agile operation and control planning mode design method and system provided by the embodiments of the present application are used to ensure the high efficiency and agility of the implementation of the operation and control planning process. For an on-orbit spacecraft to carry out scientific exploration, an important technology is the design of the operation and control planning process. Designing a reasonable scientific exploration planning process can produce efficient scientific exploration results and bring extremely high scientific benefits. The operation and control planning process must operate effectively on a wide time scale, formulate a detection implementation plan that meets all scientific exploration constraints, and generate safe and accurate scientific exploration control sequence instructions. During long-term on-orbit scientific exploration missions of spacecraft, multiple constraint conditions such as the attitude adjustment characteristics of the platform, energy constraints, space environment conditions, coverage constraints of measurement and control resources, and orbital regions need to be considered; generally, the main systems (institutions) participating in spacecraft operation and control planning include the operation management center (management institution), the ground operation and control center (spacecraft operation control center), the spacecraft platform system (platform management), and the spacecraft payload system (scientific exploration planning). Therefore, the embodiments of the present application provide an on-orbit spacecraft agile operation and control planning mode design method and system to ensure the high efficiency and agility of the implementation of the operation and control planning process. The following will be described in detail with specific drawings by way of examples.
[0039] Reference Figures 1 to 7 , Figure 1 is the flowchart of the on-orbit spacecraft agile operation and control planning mode design method provided by the embodiments of the present application; Figure 2 is the structural block diagram of the on-orbit spacecraft agile operation and control planning mode design system provided by the embodiments of the present application; Figure 3 is the planning information flow diagram provided by the embodiments of the present application;
[0040] Figure 4 is the schematic diagram of the hierarchical planning of the operation and control strategy provided by the embodiments of the present application; Figure 5 is the schematic diagram of the establishment of the operation and control planning process provided by the embodiments of the present application; Figure 6 is the schematic diagram of the operation and control planning information interaction model (weekly) provided by the embodiments of the present application; Figure 7 is the schematic diagram of the implementation process of the operation and control planning result provided by the embodiments of the present application.
[0041] In Figure 1 , the embodiments of the present application provide an on-orbit spacecraft agile operation and control planning mode design method, including the following steps:
[0042] Determine the design strategy of the spacecraft operation and control planning process;
[0043] Design the operation and control planning process;
[0044] Establish an information interaction model between the operation and control planning implementation systems;
[0045] Determine the implementation method of the operation and control planning process.
[0046] In the above technical solution, by determining the design strategy of the spacecraft operation and control planning process; designing the operation and control planning process; establishing an information interaction model between the operation and control planning implementation systems; determining the implementation method of the operation and control planning process; the operation and control planning process adopts a "two-layer planning, phased iteration" design strategy, establishing a step-by-step information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process; designing the upload implementation planning stage from the scientific exploration proposal to the scientific exploration sequence, covering the entire process of the operation and control planning for carrying out scientific exploration tasks.
[0047] In a specific and feasible implementation plan, formulate the design strategy of the operation and control planning process in a hierarchical iteration manner.
[0048] In a specific and feasible implementation plan, based on the hierarchical design strategy, determine the operation and control planning process according to the planning process nodes.
[0049] In a specific and feasible implementation plan, establish an information interaction model for the operation and control planning interface, and establish an information interface interaction model in a step-by-step progressive manner.
[0050] In a specific and feasible implementation plan, based on the interface information interaction model, convert the planning process information into an executable configuration file model to implement the final planning result.
[0051] In a specific and feasible implementation plan, formulate the design strategy of the planning process from the top layer and determine the planning design constraints.
[0052] In a specific and feasible implementation plan, based on the control planning process design strategy, design an agile operation and control planning process for on-orbit scientific exploration tasks; based on the operation and control planning process, determine the scientific exploration operation and control implementation and information interaction content.
[0053] Specifically, the planning information flow diagram of the design method for the agile operation and control planning mode of the on-orbit spacecraft is as Figure 3 shown. Step one is the input of step two, step two is the input of step three, and steps three and four are the information interaction processes. The planning process strategy design method is as Figure 4 shown. The full-link operation and control planning flow chart for the spacecraft to implement scientific exploration is as Figure 5 shown. The operation and control mode for implementing scientific exploration is as Figure 6 shown. The information interaction of the operation and control planning process is as Figure 7 shown. First, determine the guiding ideology and method strategy for the design of the task planning process; comprehensively determine the constraints for designing the operation and control planning process for the spacecraft to implement scientific exploration tasks; based on the guiding ideology and constraints, determine the agile operation and control planning process for implementing scientific exploration tasks. Specifically include:
[0054] Step 1: Determine the operation and control planning and design strategy. Step 1 is to implement the top-level strategy planning of agile operation and control planning. The "two-layer planning and phased iteration" mode is adopted to carry out the operation and control mode planning, which is divided into a planning layer and an implementation layer. The planning layer mainly conducts medium- and long-term planning. Each system submits its own planning requirement model. The operation and management center determines the medium- and long-term planning event model based on the planning requirement models submitted by each system. After multiple iterations, the final medium- and long-term planning plan is released. The implementation layer decomposes the events based on the plan document released by the planning layer. The implementation layer is also divided into an event layer and an operation layer. In the event layer planning, intelligent methods will be used for conflict resolution and task coordination, that is, according to the execution conditions, resource requirements in the flight control event requirements, and operation and control resource constraints, etc., use intelligent methods to initially arrange the execution times of each flight control event in descending order of priority. If there are conflicts in the flight control events, then perform constraint conflict detection based on the preliminary planning results, compare the priorities of the conflict events, give priority to meeting the requirements of high-priority flight control events, and adjust lower-priority flight control events if necessary to resolve the constraint conflicts; for flight control events with the same priority that have conflicts, make overall arrangements according to conflict resolution strategies such as maximizing the utilization rate of operation and control resources and minimizing the total time cost.
[0055] In the implementation stage planning, multi-party collaboration is also required. The operation and control resources are considered in unified planning with the space station. If there are event conflicts, conflict resolution is carried out according to the priorities. The event layer planning and the operation layer planning are carried out simultaneously. The event layer planning results are adjusted according to the constraint conflicts in the operation layer, and finally a flight control event plan that meets various constraints is obtained.
[0056] As Figure 4 shown, the operation and control planning process adopts the idea of "layered planning and multiple iterations". The event layer planning and the operation layer planning in the implementation layer are described as follows: 1) Event layer planning. The event layer planning takes the flight control events as a whole, coordinates the relationship between the flight control requirements in each field and the available resources and environmental constraints, as well as the resource competition relationship between each flight control event, and clarifies the resource allocation and schedule arrangement of each flight control event. 2) Operation layer planning. The operation layer planning unfolds the specific flight procedures and operation logics in the flight control event model, and optimizes the arrangement and resolves conflicts at the instruction and operation levels. The operation layer planning result is the final executable file for flight control implementation, including instruction plans, injection arrangements, flight procedures, and collaborative work procedures, etc.
[0057] Step 2: Determination of the operation and control planning process. This step is carried out based on the input of Step 1 and also receives the input of Step 3. The operation and control planning process for spacecraft scientific exploration is divided into the scientist proposal stage, proposal conversion stage, medium-term plan generation stage, monthly plan generation stage (short-term plan), weekly plan generation stage, and scientific exploration mission implementation stage. The determination of the planning process before the monthly plan is carried out based on the planning layer, and the determination of the weekly plan planning process is carried out based on the implementation layer. As Figure 5 shown.
[0058] 1) Proposal stage. Scientists put forward scientific exploration requirement proposals according to scientific needs. The proposals should describe the problems that need to be studied for spacecraft scientific exploration and how to solve them. Then, a specific department screens and reviews the proposals to determine the final implementable proposals. The payload system generates the final scientific exploration sequence based on the final proposals and multiple types of constraint conditions.
[0059] 2) Medium-term plan generation. The payload system converts the scientific exploration proposal into a medium-term plan for scientific exploration, puts forward scientific exploration goals and payload upgrade and maintenance plans, and plans to determine future medium-term scientific exploration tasks. The spacecraft platform system puts forward the medium-term plan for the spacecraft platform. Based on the medium- and long-term task planning, an annual plan is formulated. According to the platform work plan, scientific exploration goals, approved exploration proposals, etc., the key work for each month within the next 12 months is refined and generated, including the platform work plan, scientific exploration plan, repair and maintenance plan, etc. When formulating the medium-term plan, other temporary emergency situations such as unexpected events need to be incorporated into risk control.
[0060] 3) Monthly plan formulation and generation. The payload system converts the scientific exploration proposal into a medium- and long-term plan for scientific exploration and divides the medium- and long-term plan into multiple short-term plans. The payload system mainly completes the rough prediction of the scientific exploration window and the weekly task allocation. The spacecraft platform system puts forward the short-term plan for the spacecraft platform. When formulating the monthly plan, the temporary plan adjustments caused by spacecraft platform failures, payload failures, temporary adjustments of TT&C resources, etc. need to be incorporated into risk control.
[0061] 4) Weekly plan formulation and generation. Based on the monthly event plan, the operation and control center determines the weekly flight control event plan according to the flight control requirement applications provided by each party and submits it to each party for joint signature. The weekly operation and control plan is the direct input of the actual execution plan. Each system submits the changes in flight control requirements in accordance with the standard interface format based on the weekly plan working mode. The operation and control center generates and releases the planning results for the next week, applies for TT&C resources accordingly, generates various plans and injection data, and adjusts the uplink and downlink data bandwidth. Some TT&C resources may not be available for application due to other high-priority events. In this case, the TT&C resource application situation is fed back to each system, and each system adjusts the flight control requirement applications again according to TT&C constraints, etc. After multiple iterations, the final weekly flight control plan is confirmed, and each system signs the final confirmed weekly flight control plan.
[0062] 5) Real-time replanning. Replanning is used in emergency situations. The operation control center regenerates various plans in real time according to the handling requirements, and quickly evaluates the impact of the handling situation on the subsequent planning results. Generally, after temporary abnormal event types such as platform failures, payload failures, and emergency collision avoidance occur, it is necessary to evaluate whether real-time replanning is required.
[0063] Step 3: Determination of the operation control planning information interaction model. This step determines the information interaction model based on the input of Step 2, and collaborates with Step 4 in the collaborative planning design. The operation control planning information interaction model is designed in a progressive mode. The systems involved include the operation control center, the payload system, and the spacecraft platform. The system information interaction content is shown in the following table, and the information interaction is as Figure 6 shown. The process of establishing its interaction model is as follows:
[0064] 1) The operation control system collects the operation control event plans of other systems;
[0065] 2) The operation control center conducts the implementation layer planning of the operation control event based on the available TT&C resources and the operation control requirements of each system, and releases the preliminary planning results;
[0066] 3) The operation control center applies for TT&C resources and releases the final TT&C resources to each system. Each system re-plans the operation control event according to the finally released TT&C resources and submits it to the operation control center;
[0067] 4) The operation control center releases the final operation control event planning results;
[0068] 5) Each system signs and confirms the final operation control event planning;
[0069] 6) The operation control center finally implements the operation control planning event;
[0070] 7) Each system provides feedback according to the implementation results of the operation control planning event.
[0071] Step 4: Determination of the implementation method of the operation control planning process. This step is carried out based on the input of Step 2, and collaborates with the operation control planning information interaction model in Step 3 to determine the final implementation method of the operation control planning process. See Figure 7As shown in the figure. The operation and control center converts the weekly flight control event plan into a configuration model, uniformly converts the flight control event configuration model, various orbit forecasts, TT&C network configuration files, etc. into configuration files, and generates an executable execution script based on the configuration files. Based on the executable script, a platform control instruction plan, an in / out station flight procedure, and scientific exploration sequence injection data are generated. Each system conducts confirmation and countersigning on the instruction plan and injection data. Finally, the operation and control center uploads the scientific sequence injection data to implement the scientific exploration mission. The payload system processes and analyzes the scientific exploration downlink data, and the spacecraft platform monitors the platform operation status. Each system gives a specific implementation evaluation effect of the operation and control plan result to determine whether the expected goal is achieved.
[0072] In this embodiment, according to the characteristics of the operation and control of scientific exploration by the spacecraft, the design strategy of the operation and control planning process for scientific exploration is determined, and the "two-layer planning, phased iteration" mode is adopted to carry out the operation and control planning of scientific exploration. Based on the top-level operation and control planning design strategy and principles, the operation and control planning process for the spacecraft to carry out scientific exploration tasks is designed, forming a complete planning process from the scientist's proposal for scientific exploration to the final implementation of the scientific process sequence. During the design process of the planning process, it includes the collaborative work and information interaction elements of multiple systems.
[0073] In the above technical solution, the advantages are mainly manifested in: (1) Completeness. The present invention designs the planning stage from the scientific exploration proposal to the injection and implementation of the scientific exploration sequence, covering the entire process of the operation and control planning for carrying out scientific exploration tasks. (2) High efficiency and agility. The operation and control planning process adopts the "two-layer planning, phased iteration" design strategy, establishing a step-by-step progressive information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process.
[0074] In Figure 2 this application embodiment provides an in-orbit spacecraft agile operation and control planning mode design system, including:
[0075] An operation and control planning process design strategy module, used to determine the operation and control planning process design strategy for the spacecraft;
[0076] An operation and control planning process module, used to design the operation and control planning process;
[0077] An information interaction model module, used to establish an information interaction model between the operation and control planning implementation systems;
[0078] An implementation method module, used to determine the implementation method of the operation and control planning process.
[0079] In the above technical solution, the design strategy of the spacecraft operation and control planning process is determined; the operation and control planning process is designed; an information interaction model between the operation and control planning implementation systems is established; the implementation method of the operation and control planning process is determined; the operation and control planning process adopts a "two-layer planning and phased iteration" design strategy, establishing a step-by-step progressive information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process; the uplink implementation planning stage from the scientific exploration proposal to the scientific exploration sequence is designed, covering the entire process of the operation and control planning for carrying out scientific exploration tasks.
[0080] An embodiment of the present application further provides an electronic device, the electronic device includes a processor, the processor is coupled to a memory, and at least one computer program is stored in the memory, and the at least one computer program is loaded and executed by the processor to enable the electronic device to implement any one of the on-orbit spacecraft agile operation and control planning mode design methods.
[0081] In the above technical solution, the design strategy of the spacecraft operation and control planning process is determined; the operation and control planning process is designed; an information interaction model between the operation and control planning implementation systems is established; the implementation method of the operation and control planning process is determined; the operation and control planning process adopts a "two-layer planning and phased iteration" design strategy, establishing a step-by-step progressive information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process; the uplink implementation planning stage from the scientific exploration proposal to the scientific exploration sequence is designed, covering the entire process of the operation and control planning for carrying out scientific exploration tasks.
[0082] An embodiment of the present application further provides a computer-readable storage medium, and at least one computer program is stored in the computer-readable storage medium, and the at least one computer program is loaded and executed by a processor to enable the computer-readable storage medium to implement any one of the on-orbit spacecraft agile operation and control planning mode design methods.
[0083] In the above technical solution, the design strategy of the spacecraft operation and control planning process is determined; the operation and control planning process is designed; an information interaction model between the operation and control planning implementation systems is established; the implementation method of the operation and control planning process is determined; the operation and control planning process adopts a "two-layer planning and phased iteration" design strategy, establishing a step-by-step progressive information interaction model, ensuring the high efficiency and agility of the implementation of the operation and control planning process; the uplink implementation planning stage from the scientific exploration proposal to the scientific exploration sequence is designed, covering the entire process of the operation and control planning for carrying out scientific exploration tasks.
[0084] Those skilled in the art of the technical field to which the present application pertains know that the present application can be implemented as a system, a method, or a computer program product.
[0085] Accordingly, the present disclosure may be embodied in the following forms, namely: it may be entirely hardware, entirely software (including firmware, resident software, microcode, etc.), or a combination of hardware and software, generally referred to herein as a "circuit", "module" or "system". In addition, in some embodiments, the present application may also be implemented in the form of a computer program product in one or more computer-readable media, which contain computer-readable program code.
[0086] Any combination of one or more computer-readable media may be used. A computer-readable medium may be a computer-readable signal medium or a computer-readable storage medium. A computer-readable storage medium may be, for example, but not limited to, an electrical, magnetic, optical, electromagnetic, infrared, or semiconductor system, apparatus, or device, or any combination of the above. More specific examples (a non-exhaustive list) of the computer-readable storage medium include: an electrical connection having one or more wires, a portable computer disk, a hard disk, a random access memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or flash memory), an optical fiber, a portable compact disk read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the above. In this document, a computer-readable storage medium may be any tangible medium that contains or stores a program that can be used by or in connection with an instruction execution system, apparatus, or device.
[0087] Although the embodiments of the present application have been shown and described above, it can be understood that the above embodiments are exemplary and should not be construed as limiting the present application. Those of ordinary skill in the art can make changes, modifications, substitutions, and variations to the above embodiments within the scope of the present application. On this basis, various substitutions and improvements can be made to the present application, and these all fall within the protection scope of the present application.
Claims
1. A design method for the agile operation and control planning mode of on-orbit spacecraft, characterized in that, It includes the following steps: Determine the design strategy for the operation and control planning process of the spacecraft; Design the operation and control planning process; Establish an information interaction model among the operation and control planning implementation systems; Determine the implementation method of the operation and control planning process.
2. The method for designing an agile operation and control planning mode of an on-orbit spacecraft according to claim 1, wherein Formulate the design strategy for the operation and control planning process in a hierarchical iterative manner.
3. The method for designing an agile operation and control planning mode of an on-orbit spacecraft according to claim 2, characterized in that Based on the hierarchical design strategy, determine the operation and control planning process according to the planning process nodes.
4. The method for designing an agile operation and control planning mode of an on-orbit spacecraft according to claim 3, characterized in that Establish an operation and control planning interface information interaction model, and establish an information interface interaction model in a progressive manner.
5. The method for designing the agile operation and control planning mode of an on-orbit spacecraft according to claim 4, wherein Based on the interface information interaction model, convert the planning process information into an executable configuration file model to implement the final planning result.
6. The method for designing an agile operation and control planning mode of an on-orbit spacecraft according to claim 5, characterized in that, Formulate the planning process design strategy from the top layer and determine the planning design constraints.
7. The design method for the agile operation and control planning mode of an on-orbit spacecraft according to claim 6, wherein Based on the control planning process design strategy, design the agile operation and control planning process for on-orbit scientific exploration missions; Based on the operation and control planning process, determine the scientific exploration operation and control implementation and information interaction content.
8. A design system for an agile operation and control planning mode of an on-orbit spacecraft, characterized in that, It includes: An operation and control planning process design strategy module for determining the design strategy for the operation and control planning process of the spacecraft; An operation and control planning process module for designing the operation and control planning process; An information interaction model module for establishing an information interaction model among the operation and control planning implementation systems; An implementation method module for determining the implementation method of the operation and control planning process.
9. An electronic device, characterized in that, The electronic device includes a processor, the processor is coupled with a memory, and at least one computer program is stored in the memory. The at least one computer program is loaded and executed by the processor so that the electronic device implements the design method for the agile operation and control planning mode of an on-orbit spacecraft according to any one of claims 1 to 7.
10. A computer-readable storage medium, characterized in that, At least one computer program is stored in the computer-readable storage medium, and the at least one computer program is loaded and executed by a processor so that the computer-readable storage medium implements the design method for the agile operation and control planning mode of an on-orbit spacecraft according to any one of claims 1 to 7.