A THEORY OF APPROXIMATIONS IN SIMULATOR BEHAVIOR
Abstract
A mathematical expression is written for the changes in transient frequency and damping which result when the feedback branch of a single loop system is altered slightly. The result is applied in a general discussion of the accuracy of aerodynamic simulators with numerical examples of roll simulation, and suggested experiments to evaluate the approximations involved in practice.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1946
- Accession Number
- AD0659093
Entities
People
- Mark G. Foster
Organizations
- Calspan