Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions

DOI10.1134/S1064230718020120zbMath1433.70041OpenAlexW2796504669MaRDI QIDQ1795633

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/s1064230718020120

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 (9)

Optimal orientation control of a space vehicle with restrictions on the control and phase variables ⋮ Optimal control of the reorientation of a spacecraft in the given time with a quadratic performance criterion related to the control and phase variables ⋮ Control of the rotation of a solid (spacecraft) with a combined optimality criterion based on quaternions ⋮ Optimal control of the angular momentum for a solid (spacecraft) performing a spatial turn ⋮ Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional ⋮ Analytical quasi-optimal solution of the problem of the time-optimal rotation of a spacecraft ⋮ On improving the maneuverability of a space vehicle managed by inertial executive bodies ⋮ Optimal control of rigid body's rotation movement with a combined quality criterion ⋮ Analytical quasi-optimal solution of the slew problem for an axially symmetric rigid body with a combined performance index

Cites Work

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