A general calculation method to specify center-of-buoyancy for the stratospheric airship with multiple gas cells. Issue 8 (15th April 2021)

• Record Type: Journal Article
• Authors: Wang, Jie; Li, Cuichun; Meng, Xiuyun
• Is Part Of: Advances in space research. Volume 67:Issue 8(2021)
• Page Start: 2517
• Page End: 2533
• Publication Date: 2021-04-15
• Subjects: Stratospheric airship -- Double-ellipsoid hull -- Multiple gas cells -- Center-of-buoyancy -- Engineering calculation; Space sciences -- Periodicals; Astronautics -- Periodicals; Geophysics -- Periodicals; 500.505
• DOI: 10.1016/j.asr.2021.01.014
• Languages: English
• ISSNs: 0273-1177

Abstract

Highlights: This study indicates the importance of the multi-gas-cell configuration in the stratospheric airship design. The calculation models in this paper are possibly integrated into the onboard computer to improve the performance. This study may provide a tool to establish the motion simulation model for the airship with multiple. The stability problem of the pitch angle is studied when the coupled effects between the attitude and CB are considered. Further studies about the configuration of gas cells and the pressure regulation could be conducted based on this work. Abstract: As the lighter-than-air (LTA) flight vehicle, the stratospheric airship is a desirable platform to provide communication and surveillance services. During the ascent from sea-level to the mission altitude, the volume of the lifting gas may change significantly, which will result in the change of the center-of-buoyancy (CB). A general calculation method is developed to specify CB for the stratospheric airship with a double-ellipsoid hull and an arbitrary number of the gas cells. The cross-section-integral (CSI) method is used as a basic calculation scenario to specify CB. Considering the complexity in determining the boundary between the helium and air in the gas cell, a searching algorithm is put forward and the specification of CB can be conducted by the iterative calculation. As an important application, the stable condition of the pitch angle is analyzed when the change of CB is involved. Under different initial configurations, the stable pitch angle of the stratospheric airship during the ascent is specified and compared, which shows the advantages of the multi-gas-cell configuration. The results of this paper may provide an important reference for the engineering application of the stratospheric airship.