Accession Number : ADA119637

Title :   Dynamic Stability of Flight Vehicles.

Descriptive Note : Master's thesis,

Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA

Personal Author(s) : Pouliezos,Dimitrios Panagiotis

PDF Url : ADA119637

Report Date : Jun 1982

Pagination or Media Count : 257

Abstract : The thesis presents an analytical treatment of the dynamics of the flight vehicle and might be used as a textbook for a Dynamic Stability and Control advanced class. Concentration is given to derivation of equations of motion, investigation of particular modes of motion, stability derivatives, aerodynamic transfer functions and digital computer solutions. (Author)

Descriptors :   *Attitude control systems, *Flight envelope, *Aerodynamic stability, Rotary wing aircraft, Fixed wing aircraft, Dynamic response, Equations of motion, Degrees of freedom, Theses, Guided missile trajectories

Subject Categories : Helicopters
      Numerical Mathematics
      Guided Missile Dynam, Config & Cntrl Surfaces
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE