Analytical performance prediction for large antennas
Abstract
A linear mathematical modeling of the static and dynamic characteristics of a deployable offset wrap rib antenna was attempted using small motions in an effort to simulate the surface distortion resulting from thermal loading and transient oscillations from control. Both cyclic symmetry and model synthesis were used for parametric analysis. Although the ribs can be modeled as slender beams varying cross sections and equivalent linear material properties, the mesh poses a problem since its equivalent stress strain relations are highly nonlinear and sensitive to the biaxial prestressed state. Consequently, the macroscopic material properties were measured experimentally in the neighborhood of the design prestress. An equivalent tangent modulus technique was then adopted about this equilibrium state and assumed to be valid within a small range of incremental stresses.
- Publication:
-
Large Space Systems Technology, 1980
- Pub Date:
- February 1981
- Bibcode:
- 1981lsst....1..325E
- Keywords:
-
- Antenna Design;
- Design Analysis;
- Furlable Antennas;
- Large Space Structures;
- Numerical Analysis;
- Prediction Analysis Techniques;
- Contours;
- Distortion;
- Dynamic Response;
- Finite Element Method;
- Temperature Effects;
- Launch Vehicles and Space Vehicles