TECHNIQUES FOR MAPPING NON-LINEAR VECTOR-DYADIC FLIGHT SYSTEM EQUATIONS TO STATE-VECTOR FORM FOR COMPUTER MECHANIZATION,
Abstract
State vector methods for mathematically representing aerospace flight systems are rapidly becoming accepted practice. Modern multi-variable optimal control system design studies extensively utilize matrix analysis. This report presents techniques for mapping the non-linear invariant vector-dyadic system design equations to state-vector form, thereby furnishing a most convenient guide for computer mechanization and solution of these complex systems. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 03, 1963
- Accession Number
- AD0423057
Entities
People
- James S. Pappas.
- Jesus E. Carrillo