Published
A Newton Euler approach to modeling of a quad-rotor autonomous airship - Preliminary results
Published on - 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
The objective of this paper is to present the preliminary results of a model of a quadrotor airship, taking into account wind effect as well as the varying mass effects, using Newton formulation. Euler angles are used for kinematics. For dynamics, a mathematical description of a dirigible flight must contain the necessary information about aerodynamic, structural and other internal dynamic effects (engine, actuation) that influence the response of the airship to the controls.