Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality
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Publication:786106
DOI10.1134/S1064230719040105zbMath1448.93087OpenAlexW3005454889MaRDI QIDQ786106
Publication date: 12 August 2020
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1134/s1064230719040105
Application models in control theory (93C95) Synthesis problems (93B50) Existence theories for optimal control problems involving ordinary differential equations (49J15) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (4)
Analytical quasi-optimal algorithm for the programmed control of the angular motion of a spacecraft ⋮ 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 ⋮ Analytical quasi-optimal solution of the problem of the time-optimal rotation of a spacecraft ⋮ Objects changing the spatial orientation of a solid body by using mobile mass
Cites Work
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- On optimal spacecraft damping
- A special case of spacecraft optimal attitude control
- Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft
- Synthesis of spacecraft reorientation algorithms using the concept of the inverse dynamic problem
- Quadratic optimal control in reorienting a spacecraft in a fixed time period in a dynamic problem statement
- A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
- Special control regime in optimal turn problem of spherically symmetric spacecraft
- Fuel/Time Optimal Control of Spacecraft Maneuvers
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