Analytic controlling reorientation of a spacecraft using a combined criterion of optimality

DOI10.1134/S1064230718010069zbMath1433.70040OpenAlexW2797683830MaRDI QIDQ1795632

M. V. Levskii

Publication date: 16 October 2018

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230718010069

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (2)

Threshold absolute value of a relay control when time-optimally bringing a satellite to a gravitationally stable position ⋮ Analytical quasi-optimal solution of the slew problem for an axially symmetric rigid body with a combined performance index

Cites Work

• On optimal spacecraft damping
• Synthesis of spacecraft reorientation algorithms using the concept of the inverse dynamic problem
• 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
• Special control regime in the problem of optimal turn of an axially symmetric spacecraft
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