Conceptual Designing of Control System for an Unmanned Martian Airship for Exploration

Abstract

This research focuses on the flight dynamics of a Martian airship designed for planetary exploration, with special attention to the unique atmospheric challenges presented by the Red Planet. The study delves into the intricacies of flight stability, buoyancy control, aerodynamic drag, and propulsion. By employing MATLAB Simulink simulations, we model the airship's ascent, hovering, and descent cycles to evaluate thrust requirements and optimal fuel management. Through a detailed examination of aerodynamic forces, we present a holistic view of the airship’s flight mechanics and control systems, including an innovative Pneumatic Propulsion System.