The Frequency Response of a Particular Gimbal System to Coherent Rotation and Acceleration Excitation
Abstract
The general theoretical expression for the frequency response of a gimbal system to a joint rotation/acceleration driving force is derived. Theoretical estimates of physical system parameters are made for particular gimbal system. Experimental verification of these theories is obtained by measurements of the rotationally excited response of the gimbal system.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1978
- Accession Number
- ADA073153
Entities
People
- R. F. Dancer