Design and Fabricate Rocket Attitude Control System (ACS) for Accurate Payload Orientation and Control Functions.
Abstract
Three (3) Attitude Control Systems (ACS) were designed and built for SPICE, IRBS, ZIP, and FIRSSE (Background Measurements) programs. They utilized star tracker, IRU, and MIDAS platforms. The IRU system gives state-of-the-art accuracy. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 14, 1982
- Accession Number
- ADA123735
Entities
People
- Robert E. Scarboro