Flexible satellite attitude maneuver control method based on binomial approximation model
A technology of approximate model and satellite attitude, applied in the direction of motor vehicles, space navigation equipment, space navigation aircraft, etc., to achieve the effect of strong function, improved simplicity and effectiveness, and broad engineering application prospects
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0046] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0047] At present, in the study of attitude control of flexible satellites, how to design a simple and feasible control law to complete the attitude maneuver of the satellite is an important issue to enhance the application of satellites. In the present invention:
[0048] Such as figure 1 As shown, firstly, the expected maneuvering path of the satellite’s three axes is introduced, and the sampler is used to sample the output of the satellite’s attitude gyroscope to obtain the sampling value of the three-axis attitude; value, construct a discrete approximate model of the satellite attitude, on this basis, shift and make difference with the sampling value of the expected path, obtain an approximate model of the expected error, and further design a sampling control law based on this model; pass this control law through the zero-order The hold...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
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