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

Verification system of autonomous orbit control algorithm

A technology of control algorithm and autonomous orbit, which is applied in the field of satellite control, can solve problems such as inability to verify autonomous orbit control algorithms, and achieve the effect of verification of validity and accuracy

Inactive Publication Date: 2016-10-26
SHANGHAI ENG CENT FOR MICROSATELLITES
View PDF8 Cites 6 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the shortcomings of the prior art described above, the purpose of the present invention is to provide a verification system for autonomous orbit control algorithms, which is used to solve the problem that the autonomous orbit control algorithms cannot be effectively verified on the ground in the prior art

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
  • Verification system of autonomous orbit control algorithm
  • Verification system of autonomous orbit control algorithm

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0024] Embodiments of the present invention are described below through specific examples, and those skilled in the art can easily understand other advantages and effects of the present invention from the content disclosed in this specification. The present invention can also be implemented or applied through other different specific implementation modes, and various modifications or changes can be made to the details in this specification based on different viewpoints and applications without departing from the spirit of the present invention. It should be noted that, in the case of no conflict, the following embodiments and features in the embodiments can be combined with each other.

[0025] It should be noted that the diagrams provided in the following embodiments are only schematically illustrating the basic ideas of the present invention, and only the components related to the present invention are shown in the diagrams rather than the number, shape and number of componen...

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

The invention provides a verification system of an autonomous orbit control algorithm. Through a simulation computer, a spaceborne computer, a navigational star simulator and a GPS receiver, an autonomous orbit control closed loop test system is established on the ground. The spaceborne computer carries out calculation according to current position information sent by the GPS receiver, and controls and determines whether the autonomous orbit control algorithm is effective according to a result of comparing current attitude data fed back by the simulation computer, current orbit data, preset attitude data and orbit data. The test system can be established on the ground, and effectiveness and accuracy of autonomous orbit control algorithm operation are verified.

Description

technical field [0001] The invention relates to the field of satellite control, in particular to a verification system for an autonomous orbit control algorithm. Background technique [0002] During the satellite's in-orbit operation, the satellite-ground circuit is generally used to control the satellite attitude and orbit, generate or issue control commands according to a given control law, and generate control forces and moments for the satellite through the on-board actuators. Due to the constraints of satellite missions, the traditional satellite-earth loop control method cannot be used for orbit control. It does not rely on ground intervention and is completely autonomously controlled by spaceborne instruments. Therefore, an autonomous track control system needs to be built and verified on the ground. [0003] There is an autonomous orbit control algorithm running in the autonomous orbit control system. The autonomous orbit control algorithm plays a key role in the co...

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
IPC IPC(8): G05D1/08
CPCB64G1/244
Inventor 朱让剑吴宅莲孙宁本立言周美江
Owner SHANGHAI ENG CENT FOR MICROSATELLITES
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