
Accession Number : ADA319974
Title : Volume II. Flying Qualities Phase. Chapter 3: Differential Equations.
Corporate Author : AIR FORCE TEST PILOT SCHOOL EDWARDS AFB CA
PDF Url : ADA319974
Report Date : FEB 1988
Pagination or Media Count : 109
Abstract : This chapter reviews the mathematical tools and techniques required to solve differential equations. Study of these operations is a prerequisite for courses in aircraft flying qualities and linear control systems taught at the USAF Test Pilot School. Only analysis and solution techniques which have direct application for work at the School will be covered.
Descriptors : *LINEAR DIFFERENTIAL EQUATIONS, MATHEMATICAL MODELS, LINEAR SYSTEMS, PITCH(MOTION), FLIGHT CONTROL SYSTEMS, AERODYNAMIC STABILITY, DAMPING, NUMERICAL INTEGRATION, BOUNDARY VALUE PROBLEMS, POLYNOMIALS, PARTIAL DIFFERENTIAL EQUATIONS, SYSTEMS ANALYSIS, APPLIED MATHEMATICS, DERIVATIVES(MATHEMATICS).
Subject Categories : Numerical Mathematics
Operations Research
Distribution Statement : APPROVED FOR PUBLIC RELEASE