Analytical quasi-optimal solution of the slew problem for an axially symmetric rigid body with a combined performance index
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Publication:786160
DOI10.1134/S1064230720030107zbMath1453.93111OpenAlexW3041933852MaRDI QIDQ786160
A. V. Molodenkov, Ya. G. Sapunkov
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/s1064230720030107
Existence theories for optimal control problems involving ordinary differential equations (49J15) Control/observation systems governed by ordinary differential equations (93C15)
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Cites Work
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- Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft
- Quadratic optimal control in reorienting a spacecraft in a fixed time period in a dynamic problem statement
- Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions
- Analytic controlling reorientation of a spacecraft using a combined criterion of optimality
- Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions
- Optimal control of rigid body's rotation movement with a combined quality criterion
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