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