火星科学实验室2018年火星任务的进入制导改进研究

E. García-Llama, M. Ivanov, R. Winski, M. Grover, J. Shidner, R. Prakash
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引用次数: 10

摘要

2011年,火星科学实验室(MSL)发射升空,执行一项任务,将迄今为止最大、能力最强的火星车送到火星表面。msl衍生的后续任务被称为火星2018,计划于2018年发射。与2011年火星科学实验室的任务相比,2018年火星正在研究进入、下降和着陆(EDL)系统的性能增强。本文将讨论拟议的火星2018 EDL初步设计的主要元素,这些元素正在考虑提高任务进入阶段的性能。具体而言,通过修改进入参考弹道设计、飞行器升阻比、降落伞展开触发逻辑设计以及附加导航硬件的影响,以提高降落伞展开高度,从而在随后的下降和着陆阶段有更多的时间余量,增加进入质量,并减小降落伞展开时的交付椭圆尺寸为目标进行了讨论。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Mars Science Laboratory entry guidance improvements study for the Mars 2018 mission
In 2011, the Mars Science Laboratory (MSL) was launched in a mission to deliver the largest and most capable rover to date to the surface of Mars. A follow on MSL-derived mission, referred to as Mars 2018, is being proposed to launch in 2018. Mars 2018 is investigating performance enhancements of the Entry, Descent and Landing (EDL) system over that of its predecessor MSL mission of 2011. This paper will discuss the main elements of the proposed Mars 2018 EDL preliminary design that are being considered to increase performance on the entry phase of the mission. In particular, these elements are discussed with the goals of increasing the parachute deploy altitude to allow for more time margin during the subsequent descent and landing phases, increasing the entry mass, and reducing the delivery ellipse size at parachute deploy, through modifications in the entry reference trajectory design, vehicle's lift to drag ratio, parachute deploy trigger logic design, and the effect of additional navigation hardware.
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