Spacecraft Recovery & Remote Sensing, Volume. 46, Issue 3, 12(2025)
Research on Attitude Stability Control of Parachute Cabin Combination under the Action of Supersonic Deceleration Parachute
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Table 1. RCS rolationrates deadband
View tableView in ArticleTable 1. RCS rolationrates deadband
项目 判断条件 阈值/(°)·s−1 本文研究对象 跨声速 $ ：M\mathit{\mathrm{\mathit{a}}}\gg0.9 $ 40 “天问一号”伞器组合体 大底分离 分离前：50； 分离后：10 “美国科学实验室” 伞器组合体 大底分离 分离前：80； 分离后：50
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Boyi TAN, Liuxin QU, Zhi LIU, Hexi BAOYIN, Yao LI. Research on Attitude Stability Control of Parachute Cabin Combination under the Action of Supersonic Deceleration Parachute[J]. Spacecraft Recovery & Remote Sensing, 2025, 46(3): 12
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Received: Dec. 31, 2024
Accepted: Dec. 31, 2024
Published Online: Jul. 1, 2025
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