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This chapter describes the design of a Kalman filter using a historical example. It demonstrates how the position and velocity of the Apollo lunar module can be estimated by measuring the position of the lunar lander using four Earth-based Doppler radar stations and the onboard inertial sensors.

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Introductory Example

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  • 发表日期：

    2026年

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  • Sebastian Dingler,
  • Reiner Marchthaler

摘要

This chapter describes the design of a Kalman filter using a historical example. It demonstrates how the position and velocity of the Apollo lunar module can be estimated by measuring the position of the lunar lander using four Earth-based Doppler radar stations and the onboard inertial sensors.