| CHEN Li (陈 丽)*,WANG Xiaoliang* **.[J].高技术通讯(英文),2024,30(1):1~12 |
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| Differential pressure difference based altitude control of a stratospheric satellite |
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| DOI：10. 3772 / j. issn. 1006-6748. 2024. 01. 001 |
| 中文关键词: |
| 英文关键词: stratospheric satellite( StratoSat), differential pressure difference (DPD), altitude adjustment, threshold switching strategy, margin of pressure difference (MPD) |
| 基金项目: |
| Author Name | Affiliation | | CHEN Li (陈 丽)* | (* Flight College, Shanghai University of Engineering Science, Shanghai 201620, P. R. China)
(** School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, P. R. China) | | WANG Xiaoliang* ** | |
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| 中文摘要: |
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| 英文摘要: |
| An autonomous altitude adjustment system for a stratospheric satellite(StratoSat) platform is proposed. This platform consists of a helium balloon, a ballonet, and a two-way blower. The helium balloon generates lift to balance the platform gravity. The two-way blower inflates and deflates the ballonet to regulate the buoyancy. Altitude adjustment is achieved by tracking the differential pressure difference (DPD), and a threshold switching strategy is used to achieve blower flow control.The vertical acceleration regulation ability is decided not only by the blower flow rate, but also by the designed margin of pressure difference (MPD). Pressure difference is a slow-varying variable compared with altitude, and it is adopted as the control variable. The response speed of the actuator to disturbance can be delayed, and the overshoot caused by the large inertia of the platform is inhibited.This method can maintain a high tracking accuracy and reduce the complexity of model calculation,thus improving the robustness of controller design. |
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