首页> 外文会议>AAS/AIAA Space Flight Mechanics Meeting Vol.112 Pt.2, Jan 27-30, 2002, San Antonio, Texas >USING INERTIAL MEASUREMENTS FOR THE RECONSTRUCTION OF 6-DOF ENTRY, DESCENT, AND LANDING TRAJECTORY AND ATTITUDE PROFILES
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USING INERTIAL MEASUREMENTS FOR THE RECONSTRUCTION OF 6-DOF ENTRY, DESCENT, AND LANDING TRAJECTORY AND ATTITUDE PROFILES

机译:使用惯性测量来重建6自由度进入,下降和着陆轨迹和姿态轮廓

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摘要

A method was sought for estimating the "stroke" distance between a Mars Exploration Rover (MER) test lander (protected by airbags) and a surface during impact. The authors at JPL have developed a suite of software known as RED Land (for Reconstruction of Entry, Descent and Landing) to accomplish this. REDLand uses data from accelerometers and gyroscopes on board the lander test body as measurements in an extended Kalman filter, in addition to geometric and dynamical constraints, and other data, where available. This paper is a discussion of the formulation of the REDLand filter algorithms and presents results from actual MER airbag-and-lander impact tests made in 2001.
机译:寻求一种方法来估计撞击期间火星探测漫游者(MER)测试着陆器(由安全气囊保护)与地面之间的“行程”距离。 JPL的作者已经开发了一套称为RED Land的软件(用于重建进入,下降和着陆)。除了几何和动态约束以及其他可用数据外,REDLand还将着陆器测试体上的加速度计和陀螺仪的数据用作扩展卡尔曼滤波器中的测量值。本文讨论了REDLand过滤器算法的公式化,并提供了2001年进行的实际MER气囊和着陆器冲击试验的结果。

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