DESIGN STUDY OF AN INTEGRATED AIRBORNE TELEMETRY SYSTEM
Abstract
Research was continued on an integrated airborne telemeter system. Research of various missile and space vehicle data measurements was conducted to provide a basis for specific PCM system design parameters. For detail analysis of the measurement data content, the measurements were separated into the following 3 categories of classification: (1) type of measurements versus number of measurements, (2) measurements versus frequency response, and (3) measurements versus acceptable error. The breakdown of these measurement requirements are shown in diagrams. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 31, 1960
- Accession Number
- AD0259828
Entities
People
- Hugh Pruss