Development of an Integrated Development Environment for Flight Control Law Design

초록

Modern aircrafts are completed with virieties of subsystems such as aerodynamics, material, structure, control and propulsion. As the number of subsystms increases, the requirements for mission and maneuver are both difficalt and compicated. The puspose of this paper is to give an IDE(Integrated Development Environment) to designers for saving developing time. The IDE includes analysis of peformance, application of flight control law and calidation of handling qualities.