Quasioptimal Spacecraft Attitude Control Constructed According to the Poinsot Concept
نویسندگان
چکیده
The problem of attitude optimal control a spacecraft as solid body with the energy spent on maneuvering taken quadratic functional, and fixed transition time, is investigated. dynamic configuration boundary conditions an angular velocity are arbitrary; function not limited. According to Poinsot concept from theoretical mechanics interpretation motion around point help Pontryagin maximum principle, quasioptimal analytical solution obtained, which brought algorithm. Numerical examples provided that confirm closeness problem.
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ژورنال
عنوان ژورنال: Aerospace
سال: 2023
ISSN: ['2226-4310']
DOI: https://doi.org/10.3390/aerospace10050402