SIMULATION OF AN ATTITUDE DETERMINING SYSTEM UTILIZING MAGNETOMETERS AND EARTH'S HORIZON SENSOR
Abstract
This report presents experimental data obtained by partial simulation of a missile attitude determination system consisting of magnetometers sensing the earth's magnetic field and a sensor responding to the earth's horizon. The contribution of various errors to system error is outlined. A basis is provided for possible future work concerning the affect of on-board interference.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 31, 1965
- Accession Number
- AD0466549
Entities
People
- William F. Baxter