Title:
POD PERFORMANCE TEST SYSTEM AND METHOD OF NEAR SPACE AEROSTAT
Document Type and Number:
WIPO Patent Application WO/2023/098442
Kind Code:
A1
Abstract:
A pod (60) performance test system (1) and method of a near space aerostat. The system (1) comprises: a human-computer interaction test control device (10), a motion simulation control device (20), a suspension device (30), and a motion simulation countertwisting mechanism (40). The human-computer interaction test control device (10) is electrically connected to the motion simulation control device (20), the motion simulation countertwisting mechanism (40), and a pod (60) of the near space aerostat, respectively. The motion simulation control device (20) is electrically connected to the motion simulation countertwisting mechanism (40). The motion simulation countertwisting mechanism (40) is connected to the pod (60) by means of a connecting member (50). On the basis of motion control parameters sent by the human-computer interaction test control device (10), the motion simulation control device (20) can control the motion simulation countertwisting mechanism (40) to simulate multiple complex motion states, so that the pod (60) is in multiple complex motion states. When the pod (60) is in multiple complex motion states, performance test is performed on the pod (60) and performance test results corresponding to the multiple motion states are obtained.
Inventors:
FENG HUI (CN)
CUI YANXIANG (CN)
ZHANG DONGHUI (CN)
LIN WENLIANG (CN)
LI BOEN (CN)
ZHOU JIN (CN)
CUI YANXIANG (CN)
ZHANG DONGHUI (CN)
LIN WENLIANG (CN)
LI BOEN (CN)
ZHOU JIN (CN)
Application Number:
PCT/CN2022/131040
Publication Date:
June 08, 2023
Filing Date:
November 10, 2022
Export Citation:
Assignee:
AEROSPACE INFORMATION RESEARCH INSTITUTE CHINESE ACADEMY OF SCIENCES (CN)
International Classes:
B64F5/60
Foreign References:
| CN114368492A | 2022-04-19 | |||
| CN112729342A | 2021-04-30 | |||
| CN2539985Y | 2003-03-12 | |||
| CN112650193A | 2021-04-13 | |||
| CN113483978A | 2021-10-08 | |||
| US20140191893A1 | 2014-07-10 | |||
| CN106124147A | 2016-11-16 |
Other References:
ZHANG, DAWEI ET AL.: "A Simplified Design of Decoupling Control System in Balloon Gondola", AEROSPACE CONTROL, vol. 34, no. 4, 15 August 2016 (2016-08-15), XP009546827, ISSN: 1006-3242
Attorney, Agent or Firm:
BEIJING XINKEHUALING IP SERVICE AGENT (CN)
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