Dynamics of spacecraft attitude considering high-fidelity solar radiation pressure
Dynamics of spacecraft attitude considering high-fidelity solar radiation pressure
Solar radiation pressure (SRP) is a major disturbance for a spacecraft operated in deep space missions, affecting its orbit and attitude, and high accuracy of the SRP calculation is required. The accuracy of SRP calculation is affected by the shape and surface characteristics of the satellite. However, existing computational models do not sufficiently take into account the exact reflective properties of the satellite surface. A detailed reflection model and considering the optical characteristics yield a different SRP and its torque from the conventional ones, resulting in a different attitude motion. In this study, an SRP calculation method that considers the exact reflective properties is applied to investigate the attitude dynamics.
Attitude Dynamics, Bidirectional Reflectance Distribution Functions, Cook-Torrance model, Generalized Sail Dynamics Model, Solar Radiation Pressure
Masaki, Kakeru
6648dc95-7d61-4977-90b9-53f8f96819d4
Yoshimura, Yasuhiro
bee6a581-5176-46a6-8793-d539fa664489
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Hanada, Toshiya
6a914261-4634-4e52-8605-7c7579869145
September 2022
Masaki, Kakeru
6648dc95-7d61-4977-90b9-53f8f96819d4
Yoshimura, Yasuhiro
bee6a581-5176-46a6-8793-d539fa664489
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Hanada, Toshiya
6a914261-4634-4e52-8605-7c7579869145
Masaki, Kakeru, Yoshimura, Yasuhiro, Chen, Hongru and Hanada, Toshiya
(2022)
Dynamics of spacecraft attitude considering high-fidelity solar radiation pressure.
In Proceedings of International Aeronautical Congress (IAC 2022).
Record type:
Conference or Workshop Item
(Paper)
Abstract
Solar radiation pressure (SRP) is a major disturbance for a spacecraft operated in deep space missions, affecting its orbit and attitude, and high accuracy of the SRP calculation is required. The accuracy of SRP calculation is affected by the shape and surface characteristics of the satellite. However, existing computational models do not sufficiently take into account the exact reflective properties of the satellite surface. A detailed reflection model and considering the optical characteristics yield a different SRP and its torque from the conventional ones, resulting in a different attitude motion. In this study, an SRP calculation method that considers the exact reflective properties is applied to investigate the attitude dynamics.
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Published date: September 2022
Venue - Dates:
73rd International Astronautical Congress, IAC 2022, , Paris, France, 2022-09-18 - 2022-09-22
Keywords:
Attitude Dynamics, Bidirectional Reflectance Distribution Functions, Cook-Torrance model, Generalized Sail Dynamics Model, Solar Radiation Pressure
Identifiers
Local EPrints ID: 497569
URI: http://eprints.soton.ac.uk/id/eprint/497569
ISSN: 0074-1795
PURE UUID: a1f9a127-7a62-40b1-b1c3-5f749ae21e16
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Date deposited: 27 Jan 2025 18:01
Last modified: 28 Jan 2025 03:13
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Contributors
Author:
Kakeru Masaki
Author:
Yasuhiro Yoshimura
Author:
Hongru Chen
Author:
Toshiya Hanada
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