Application of Complex Functional of Quality in Optimal Control of Spacecraft Motion
The problem of optimal control of the reorientation of a spacecraft as a solid body from an arbitrary initial position into a prescribed final angular position is considered and solved. The case is studied in detail when the minimized index combines, in a given proportion, the integral of modulus...
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| Format: | Article |
| Language: | English |
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Shahid Chamran University of Ahvaz
2021-01-01
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| Series: | Journal of Applied and Computational Mechanics |
| Subjects: | |
| Online Access: | https://jacm.scu.ac.ir/article_15974_09e54e4fdfed9aff81b4872c7cce80b7.pdf |