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2024 | OriginalPaper | Buchkapitel

Design and Verification of Satellite Propulsion Layout with Force Couple for AC and Multi-thrust Options for OC

verfasst von : Linna Chen, Kui Zou, Yifeng Zhang, Chunqing Zhang, Jinhua Hao

Erschienen in: Signal and Information Processing, Networking and Computers

Verlag: Springer Nature Singapore

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Abstract

Considering the requirements of traditional thruster layout, the characteristics of missions and working loads of the satellites, a thruster layout method for attitude controlling (AC) with force couple and orbit controlling (OC) with multi-thrust options is proposed. By making reasonable use of surface space and optimizing configuration quantity of thruster of the satellites, impact on orbit altitude caused by attitude control is reduced as far as possible. With different thrust options, requirements for large impulse orbit transfer and small impulse trajectory maintenance are satisfied. Mathematical simulation and in-orbit flight verification show that the proposed method is effective and feasible.

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Shi, K., Cheng, Y., Zhang, Y.: Research on configuration of attitude control thrusters. Mod. Defense Technol. 2(40), 44–49 (2012)

Cheng, Y., Zhang, Y.: Research on the spacecraft attitude control with the influence of the. Mod. Defense Technol. 5(36), 41–49 (2008)

Hu, W., Jin, H., Wang, Q.: Research on optimizing mounting position of satellite 490N thruster. Spacecraft Eng. 6(12), 44–47 (2013)

Xu, C.,Cui, J., Zhang, L., et al.: Application research of genetic algorithm in installation adjusting optimization of satellite engine. 2(23), 58–63 (2014)

Renwei, Z.: Satellite Orbit Attitude Dynamics and Control. Beihang University Press, Beijing (1998)

Wang, Z.: Design and Performance Research of Orbital Control Thruster for Formation Micro-nano Satellites (2021)

Li, T., Shan, T., Liu, Z., et al.: Design of Configuration and Assembly for High Resolution Agile Remote Sensing Satellite (2022)

Guan, Z., Ruan, W., Liu, W., et al.: Study of trajectory-controlled thrust vector technology application in air defense missile. Air Space Defense 2(3) (2020)

Wei, Y., Guo, S., Zhao, J., et al.: Design characteristic and verification of propulsion system of Change-4 probe. Spacecraft Eng. 4(28) (2019)

10.

Changfu, G.: Spacecraft Dynamics. Science and Technology Press, Beijing (2006)

11.

Chen, Z., Song, Z., Lyu, J., et al.: Equivalent models of liquid sloshing under the excitation of small pulse in microgravity everonment. Aerosp. Control Appl. 48(3), 84–92 (2022)

12.

Liu, X., Nie, W., Zhang, H., et al.: Characterisics of pulse detonation rocket engine with specific impulse and small thrust demand. Aerosp. Control Appl. 48(6), 67–75 (2022)

Titel: Design and Verification of Satellite Propulsion Layout with Force Couple for AC and Multi-thrust Options for OC
verfasst von: Linna Chen
Kui Zou
Yifeng Zhang
Chunqing Zhang
Jinhua Hao
Verlag: Springer Nature Singapore
Buch: Signal and Information Processing, Networking and Computers
Print ISBN: 978-981-9721-15-3

Electronic ISBN: 978-981-9721-16-0

Copyright-Jahr: 2024
DOI: https://doi.org/10.1007/978-981-97-2116-0_45