RESEARCH ON SATELLITE ATTITUDE CONTROL USING PLASMA PINCH ENGINES.
Abstract
This is the final report covering theoretical considerations regarding the application of the Plasma Pinch Engine to Satellite Attitude Control. Both three-axis and two-axis control are considered, with emphasis on two-axis stabilization of a vehicle axis to the local vertical. Stability and cross coupling problems are investigated and methods of damping the free yaw axis are considered. Design rules for implementing such systems are given. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1965
- Accession Number
- AD0474276
Entities
People
- Erwin Vogel