In-Plane Formation Reconfiguration with Radial Maneuvers

Lim, Yeerang; Mok, Sung Hoon

doi:10.2514/1.g004933

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2022

2025

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Cited by 2 publications

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“…is shifting towards the nanosatellites. The solution to these problems involves the creation of low-orbit nanosatellite`s constellations [8][9][10][11]. A nanosatellite-follower of the constellation should have increased manoeuvrability, power supply and autonomy.…”

Section: Introductionmentioning

confidence: 99%

Formation of an Additional Motion Control Loop for the Nanosatellite to Adapt its Onboard Model to the Current Operating Conditions

Ломака

2022

IOP Conf. Ser.: Mater. Sci. Eng.

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The paper presents the formation of additional feedback in the loop of the attitude control system of a nanosatellite. Feedback is based on the assessment of the inertial characteristics of the nanosatellite. The influence of the accuracy of knowledge of the inertial characteristics of a nanosatellite on the formation of an optimal control law in the problem of reorientation was estimated. Statistical modelling has been carried out to assess the effectiveness of nanosatellite on-board sensors in the problem of identifying the inertial characteristics of a nanosatellite. Recommendations for the selection of sensor’s characteristics and time interval of data collection have been formulated.

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Section: Introductionmentioning

confidence: 99%