Basic Equations of Flight Dynamics.

      Аннотация: In the first chapter the required mathematical tools are developed. In the second chapter, a method to find complete movement equations for a deformable vehicle is presented. In the third chapter, reference states for flight are defined and a complete kinematical solution is proved. Also, a method to dynamically compensate or trimm a vehicle on these reference states is proposed. On the fourth chapter, the movement equations for the perturbed state are thorougfully developed and some expressions for stability derivatives are presented.

Ключевые слова: aerodynamics, flight dynamics, flight simulation