A Nonlinear Feature Detection Method of Spacecraft Structure Driven by Free Vibration Displacement Response
A technology of spacecraft structure and nonlinear characteristics, which can be used in instruments, complex mathematical operations, calculations, etc.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0041]The technical solution of the present invention will be further described below in conjunction with the drawings and embodiments.
[0042]This embodiment uses a five-degree-of-freedom non-linear spring-damping-mass system to illustrate the process of the method of the present invention, such asfigure 1 The flow chart of the implementation of this method is shown. The masses of the mass blocks are: m1=20kg, m2=10kg, m3=15kg, m4=10kg, m5=5kg; linear spring stiffness coefficient k1=20N / m, k2=10N / m, k3=40N / m, k4=50N / m, k5=100N / m; the stiffness coefficient of the nonlinear spring is shown in Table 1:
[0043]Table 1 Non-linear spring stiffness coefficient parameter values
[0044]
[0045]Using proportional damping, that is, the proportional damping coefficients are 0.01 and 0.01 respectively, the present invention includes the following steps:
[0046](1) Impose initial displacements of different magnitudes on the structure to be inspected, and extract the measured position movement response of ...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More - R&D
- Intellectual Property
- Life Sciences
- Materials
- Tech Scout
- Unparalleled Data Quality
- Higher Quality Content
- 60% Fewer Hallucinations
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2025 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com



