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Innovative Mars EDL GNC technologies for future China Mars exploration

机译:创新的火星EDL GNC技术可用于未来的中国火星探索

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All Mars landers to date continue to rely on the entry, descent and landing (EDL) technologies developed for the Viking missions in the mid-seventies of the last century. Viking-like landers adopt inertial measurement unit (IMU) based navigation mode and unguided ballistic trajectory entry without lift control, which lead to larger landing error ellipse and lower altitude landing site restriction. Future Mars missions, such as Mars sample return, manned Mars landing and Mars base, need to achieve the pin-point Mars landing (safe landing within tens of meters to 100 m of a preselected target site). Since the current EDL system and GNC methods can not satisfy the requirements for future pinpoint Mars landing missions, the next generation of EDL system and GNC methodologies are required in order to deliver the largest and most capable lander/rover to date to the surface of Mars. In this paper, we will report the latest progress on Mars EDL navigation, guidance and control in China. In order to overcome the defect of traditional IMU based navigation, we develop the new estimation methods and integrated navigation for Mars entry, descent and landing. External navigation observation information from radio, radar and camera are included in the integrated navigation scheme to improve the navigation accuracy. At the same time, active entry guidance methods are proposed to improve the guidance performance with the larger parameter uncertainties using robust and adaptive control theory.
机译:迄今为止,所有火星着陆器都继续依赖于上世纪70年代中期为维京任务开发的进入,下降和着陆(EDL)技术。类维京人着陆器采用基于惯性测量单元(IMU)的导航模式和无升程控制的无制导弹道输入,从而导致更大的着陆误差椭圆和更低的高度着陆点限制。未来的火星飞行任务,例如火星样本返回,载人火星着陆和火星基地,都需要实现精确的火星着陆(在预先选择的目标地点的数十米至100 m内安全着陆)。由于当前的EDL系统和GNC方法无法满足未来精确的火星登陆任务的要求,因此需要下一代EDL系统和GNC方法论,以便向火星表面提供迄今为止最大,能力最强的着陆器/流动站。在本文中,我们将报告中国火星EDL导航,制导和控制的最新进展。为了克服传统的基于IMU的导航的缺陷,我们针对火星的进入,下降和着陆开发了新的估计方法和集成导航。集成导航方案中包括来自无线电,雷达和摄像机的外部导航观测信息,以提高导航精度。同时,基于鲁棒自适应控制理论,提出了主动进入制导方法,以提高参数不确定性时的制导性能。

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