Effects of Perturbation on Formation Flights around an Eccentric Reference Orbit

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概要

• 論文の詳細を見る

• In this study, we propose a basic method for the construction of a formation flight around an eccentric reference orbit under the influence of gravitational disturbances (J2). The relative motion between two spacecraft in the formation flight is affected by J2. The effects of this perturbing force are analyzed, and the initial conditions of the formation flight for the suppression of these effects are derived on the basis of these analytical results.

• 一般社団法人 日本機械学会の論文

著者

• Yoshikawa Shoji

  Mitsubishi Electric Corp. Advanced Technology R&d Center

• YAMADA Katsuhiko

  Nagoya University

• SHIMA Takeya

  Mitsubishi Electric Corporation

• YOSHIKAWA Shoji

  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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