Position Control for Precise Formation Flying

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概要

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• A position control method for precise formation flying is proposed and evaluated in this paper. We focus on a simple case where the distance between two spacecraft in the along-track direction must be kept constant. Major perturbations such as the J2 gravitational perturbation and atmospheric drag are taken into account, and the control effort necessary to maintain the distance constant is estimated. Numerical simulations validate the analytical results.

著者

• Yoshikawa Shoji

  Mitsubishi Electric Corp. Advanced Technology R&d Center

• YAMADA Katsuhiko

  Nagoya University

• SHIMA Takeya

  Mitsubishi Electric Corporation

関連論文

• Optical Testing of Star Sensor (II) : Alignment of Star Sensor from Off-Line Pictures Taken in Orbital Test
• Optical Testing of Star Sensor (I) : Defocus Spot Measuring Technique for Ground-Based Test
• Position Control for Precise Formation Flying
• Effects of Perturbation on Formation Flights around an Eccentric Reference Orbit

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