An Attitude Control System for a Large Geosynchronous Earth-Pointing Satellite
Abstract
The proposed attitude control system addresses three principal problem areas: (1) Operation within a high disturbance torque environment; (2) The preservation of vehicle attitude in the event that the optical attitude sensors are destroyed by external means; and (3) System operational longevity.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 05, 1977
- Accession Number
- ADA044822
Entities
People
- Joseph R. Vernau
Organizations
- Massachusetts Institute of Technology