Special control regime in optimal turn problem of spherically symmetric spacecraft
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Publication:1956927
DOI10.1134/S1064230709060057zbMath1198.49015OpenAlexW1985844257MaRDI QIDQ1956927
A. V. Molodenkov, Ya. G. Sapunkov
Publication date: 24 September 2010
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1134/s1064230709060057
Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)
Related Items (9)
Special control regime in the problem of optimal turn of an axially symmetric spacecraft ⋮ Analytical solution of the of optimal slew problem of a spherically symmetric spacecraft in the class of conical motions ⋮ Optimal control of the angular momentum for a solid (spacecraft) performing a spatial turn ⋮ On improving the maneuverability of a space vehicle managed by inertial executive bodies ⋮ Special control mode in the problem of optimal turn of an arbitrary rigid body (spacecraft) ⋮ Analytical solution of the time-optimal slew problem of a spherically symmetric spacecraft in the class of conical motions ⋮ Analytic controlling reorientation of a spacecraft using a combined criterion of optimality ⋮ Restricted quadratic optimal control of a spacecraft turning in a fixed time period ⋮ Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality
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