深空探测学报（中英文）2025，Vol.12Issue(6)：629-638,10.DOI:10.3724/j.issn.2096-9287.2025.20250045
面向火星精确着陆的多维开伞窗口设计
Multi-Dimensional Parachute Deployment Box for Mars Precision Landing
摘要
Abstract
The parachute deployment conditions during the terminal entry phase in Mars landing missions exhibit critical impact on landing precision.In this article,aiming at the requirements of safe parachute deployment and accurate landing,a multi-dimensional parachute deployment box for determining deployment condition during Mars landing was proposed.First,an extreme-range optimization model was established,synthesizing the dynamics and constraints of both parachute descent and powered descent phases.Then,on the basis of the two-dimensional altitude-velocity deployment box,a multi-dimensional parachute deployment box characterized by altitude,velocity,flight-path angle,and extreme range was constructed through the integration of extreme range information.Furthermore,an evaluation index for landing precision was formulated and a deployment control logic was proposed for minimizing landing deviation.Finally,the proposed deployment box was simulated in a Mars landing mission.The results demonstrate that the proposed box effectively satisfies safe deployment and landing precision demands,eliminating the range-to-go error at the terminal of the entry phase.关键词
火星探测/精确着陆/多约束/开伞窗口/开伞控制Key words
Mars exploration/precision landing/multiple constraints/parachute deployment box/parachute deployment control分类
航空航天引用本文复制引用
邢哲豪,梁子璇..面向火星精确着陆的多维开伞窗口设计[J].深空探测学报（中英文）,2025,12(6):629-638,10.基金项目
Supported by the National Natural Science Foundation of China(62073034) （62073034）
