Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

A method for autonomous and continuous planning of satellite missions

A mission and satellite technology, applied in three-dimensional position/channel control and other directions, can solve problems such as unsafe cancellation or delayed execution of satellite missions, and achieve the effect of ensuring continuous execution and reducing risks

Active Publication Date: 2017-09-29
AEROSPACE DONGFANGHONG SATELLITE
View PDF3 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The technical problem of the present invention is to overcome the problems caused by the traditional satellite working mode that is mainly based on manual intervention and is constrained by ground measurement and control resource conditions, and provides an autonomous and continuous planning method for satellite tasks. Information such as satellite discharge depth, illumination status, resource status, and safety status of the entire satellite can be used to carry out autonomous and continuous planning of on-board load tasks, execute tasks when the satellite status is safe, and cancel or delay the execution of satellite tasks when it is not safe, so as to solve the problem that satellites do not rely on the outside world Control and information injection, accurately perceive its own state and external environment, autonomously control satellites to complete various tasks, improve the satellite’s autonomous mission planning capabilities in orbit, and reduce the risk of fatal satellite failures

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • A method for autonomous and continuous planning of satellite missions
  • A method for autonomous and continuous planning of satellite missions
  • A method for autonomous and continuous planning of satellite missions

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0070] Embodiment 1: with figure 2 As shown, the satellite performs mission planning at time t0, and finds that the satellite will enter a specific area for work after 15 minutes. This is a short-term mission. At this time, analyze whether the resources and status of the satellite meet the mission start conditions. If so, it can be included in the new mission. task set P'. This mission needs to start the data transmission warm-up in advance, so the data transmission is turned on for warm-up 10 minutes before the mission execution. The time when the satellite enters the target control area is t1, which is the start time of the mission, and the payload equipment starts to start taking pictures. The moment when the satellite leaves the target control area is t2. At this time, the payload equipment is turned off, and the payload task ends. The work of the entire load task is driven by whether the satellite enters the target control area. The time length from t1 to t2 is 20 minut...

Embodiment 2

[0077] Embodiment 2: as image 3 As shown in , the satellite performs mission planning at a certain time t0, and plans the payload mission within 100 minutes. Assume that a load task with ID ZaiHeTask enters the target control area set G, and the start time is 99 minutes. At this time, it is a long-term task, which is directly included in the new task set P’. Every time the satellite performs mission planning between t0 and t1, the payload mission is a long-term mission, which is directly included in the new mission set P' until the time t1 is reached. At this time, when the task is planned, the starting time of the task becomes 60 minutes, and the task becomes a mid-term task. At this time, the task planning needs to be carried out in combination with the safety state of the whole satellite and the discharge depth of the satellite in the state set S. If the safety state of the whole star is If it is safe, and the discharge depth of the satellite is greater than the discharge...

Embodiment 3

[0080] Embodiment 3: Take the public resource "digital transmission" as an example, such as Figure 4 As shown, task 1 turns on data transmission at time T0 and turns off data transmission at time T2; task 2 turns on data transmission at time T1 and turns off data transmission at time T3. The execution process of the two tasks overlaps, and both use the "digital transmission" resource, and there is a resource conflict. If this resource conflict is not considered during task planning, and the two tasks are executed separately, for task 2, although the data transmission is turned on at T1, it is turned off by the command of task 1 at T2, so task 2 cannot work normally. implement. If the conflict resolution strategy is adopted, the task instructions can be adjusted during task planning, and the normal execution of the two tasks can be guaranteed without executing the "on data transmission" command of task 2 and the "off data transmission" command of task 1.

[0081] If two task...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

An autonomous and continuous planning method for satellite tasks. At a certain moment, the satellite calculates the executable tasks that enter the set G according to the satellite orbit and the target control area set G, and plans the tasks according to the hierarchy of long-term tasks, medium-term tasks, and short-term tasks method, combined with the current state set S of the satellite, to determine whether the task can be included in the new task set P'. If there is a resource conflict in the execution of multiple tasks, the conflict will be resolved according to the pre-established rules. Update the current task set P to be consistent with the set P', and extract the short-term tasks in the set P that reach the start time for the real-time system to execute. Finally, set G and set S are updated. The invention solves the problem that the satellite does not rely on external control and information injection, accurately perceives its own state and external environment, and independently controls the satellite to complete various tasks, improves the autonomous working ability of the satellite, and reduces the risk of fatal failure of the satellite.

Description

technical field [0001] The present invention proposes a method for autonomous and continuous planning of satellite missions, and particularly relates to a method for autonomously carrying out on-board load missions by using information such as the satellite's position, orbit, satellite discharge depth, illumination status, resource status, and satellite safety status independently obtained by the satellite. Continuous planning reduces ground intervention and control and enhances satellite reliability. Background technique [0002] At present, most of the on-orbit mission management of satellites still requires ground control. This kind of control has many factors that affect the safety and reliability of satellite in-orbit operation, specifically in the following aspects: [0003] 1. Earth observation satellites mostly use sun-synchronous orbits, which are characterized by short controllable arcs (more than ten minutes each time) and long effective control intervals (about 1...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
Inventor 李娟王旭李志刚
Owner AEROSPACE DONGFANGHONG SATELLITE
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com