Synthesis of the Optimal Control of the Spacecraft Orientation Using Combined Criteria of Quality

Author:

Levskii M. V.

Publisher

Pleiades Publishing Ltd

Subject

Applied Mathematics,Computer Networks and Communications,Computer Vision and Pattern Recognition,Information Systems,Theoretical Computer Science,Control and Systems Engineering,Software

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Analytical Quasi-Optimal Algorithm for the Programmed Control of the Angular Motion of a Spacecraft;Journal of Computer and Systems Sciences International;2023-06

2. An attitude control by the functional series in the problem of nanosatellite reorientation;Aerospace Science and Technology;2023-01

3. An Approach to the Control of the Nanosatellite’s Longitudinal Axis Reorientation;2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS);2022-05-30

4. Analytical Quasi-Optimal Solution of the Problem of the Time-Optimal Rotation of a Spacecraft;Journal of Computer and Systems Sciences International;2021-07

5. Control of a Moving Mass with the Initial and Final Position on the Boundary of the Area of Motion in Order to Achieve the Fastest Rotation of a Solid Body;Journal of Computer and Systems Sciences International;2021-07

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