An alternative flight control system for an unmanned aircraft whose flight control system fails during a longitudinal flight with constant forward velocity

Abstract

In this paper we build up a flight control system for an unmanned aircraft whose flightcontrol system fails during a longitudinal flight with constant forward velocity. This task isaccomplished using only the system of differential equations, which governs the movement of theaircraft around its center of mass. Numerical simulation is given.

Keywords

• Oscillations
• Unmanned aircraft
• Flight control
• Longitudinal flight with constant forward velocity.