Analysis of Influence of Stratospheric Airship’s Key Parameter Perturbation on Motion Mode

Author:

Tang Jiwei1ORCID,Bai Shilong2,Xie Weicheng3ORCID,Wu Junjie3,Jiang Hanjie4ORCID,Sun Yuxuan1

Affiliation:

1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China

2. Chongqing Near Space Innovation R&D Center, Shanghai Jiao Tong University, Chongqing 401135, China

3. Aerospace System Engineering Shanghai, Shanghai 201108, China

4. School of Aerospace Engineering, Universiti Sains Malaysia, Nibong Tebal 14300, Malaysia

Abstract

The stratospheric airship is taken as the research object, and the motion mode analysis of the stratospheric airship is carried out. The influence of key parameters such as the center of mass, the center of buoyance, and the aerodynamic stability moment on the motion mode of stratospheric airship are analyzed and summarized in detail. According to the simulation and analysis results, unlike high-speed and high-dynamic aircrafts such as airplanes, the motion modes of the stratospheric airship are hardly affected by the perturbation of aerodynamic stability moment; the perturbations of the vertical center of mass and the vertical center of buoyancy have a great influence on the pitch pendulum motion modes, and their parameter perturbations affect the frequency of the pitch pendulum motion and also the stability of the pitch pendulum motion; the axial mass center location perturbation not only changes the damping of pitch pendulum motion but also affects the frequency of the yaw motion attitude motion mode to a certain extent.

Funder

National Natural Science Foundation of China

Publisher

MDPI AG

Subject

Aerospace Engineering

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