Title :
Modeling of stratosphere airship
Author :
Wang, Xiao-liang ; Ye Ma ; Shan, Xue-xiong
Author_Institution :
Sch. of Aeronaut. & Astronaut., Shanghai Jiao Tong Univ., Shanghai, China
Abstract :
The dynamics and kinematics model is very important for the analysis of stability, manipulation and control of stratosphere airship. A full modeling approach that includes the computation of aerodynamics of airship and the added mass for the nonlinear dynamics simulation of stratosphere airships is proposed in this paper. In this approach, the aerodynamics of airship is calculated based on a panel method, an engineering estimation and theory approach. A new numerical method for calculating added masses of airship is developed by using the CFD method. This model can simulate the motion of stratosphere airships quickly and accurately.
Keywords :
aerodynamics; airships; computational fluid dynamics; motion control; nonlinear dynamical systems; stratosphere; CFD method; aerodynamics computation; airship control; motion control; nonlinear dynamics; panel method; stratosphere airship; Acceleration; Aerodynamics; Atmospheric modeling; Boundary conditions; Computational modeling; Force; Mathematical model;
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
DOI :
10.1109/ISSCAA.2010.5633300