AEROSPACE SHANGHAI, Volume. 41, Issue 3, 47(2024)
Overview of Takeover Control Technology for Failed Spacecraft
Fig. 3. Diagram of the attitude/orbit takeover control for a failed spacecraft[8]
Fig. 4. Diagram of the takeover control by a rigid manipulator[25]
Fig. 5. Typical projects of the takeover control by rigid manipulators[26]
Fig. 6. Diagram of the takeover control for the failed spacecraft based on cellular robots[27]
Fig. 7. On-orbit demonstration validation scenario for the Phoenix Program[30]
Fig. 9. System composition of the space cellular robot proposed by Northwestern Polytechnical University[32]
Fig. 10. Diagram of the takeover control by the traditional space net system[41]
Fig. 12. Diagram of the takeover control by a maneuverable space net robot[55]
Fig. 13. Diagram of the takeover control by a tethered space robot
Fig. 14. Diagram of the structural components of a space tethered robotic mechanism[63]
Fig. 15. Diagram of the electromagnetic-based takeover control for space targets[25]
Fig. 16. Experimental equipment of Japan JAXA eddy current takeover control system
Fig. 17. Ground experiment system of single-degree-of-freedom eddy current takeover control conducted by Northwestern Polytechnical University[70]
Fig. 18. Diagram of the takeover control based on non-contact electrostatic Coulomb forc[80]
Fig. 19. Diagram of the takeover control by an ion beam impact-based spacecraft[25]
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Panfeng HUANG, Yingbo LU, Fan ZHANG, Ya LIU. Overview of Takeover Control Technology for Failed Spacecraft[J]. AEROSPACE SHANGHAI, 2024, 41(3): 47
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Received: Mar. 25, 2024
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Published Online: Sep. 3, 2024
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