Study of Tactical Missile Guidance: Accuracy Limitations and Guidance Sensitivities. Volume 1
Abstract
This report covers the results of limiting guidance accuracy studies for nine proposed aided inertial guidance techniques. In each case an optimum information handling scheme was assumed. This provides a consistent framework for comparing alternative schemes and determining the desired lower limit on errors for each technique. The report also develops the sensitivities of missile guidance errors to sensor errors and initial alignment errors for three unaided guidance techniques--inertial guidance and heading command guidance with and without wind compensation. The sensitivity tables provided allow rapid comparisons of different inertial sensors and alignment techniques which may be suggested for use in proposed guidance systems.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 29, 1973
- Accession Number
- AD0916420
Entities
People
- Arthur A. Sutherland Jr.
- Dale W. Klein
Organizations
- TASC, Inc