A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
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Publication:1951950
DOI10.1134/S1064230707020189zbMath1263.49046OpenAlexW1996919946MaRDI QIDQ1951950
A. V. Molodenkov, Ya. G. Sapunkov
Publication date: 24 May 2013
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1134/s1064230707020189
Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (11)
Optimal orientation control of a space vehicle with restrictions on the control and phase variables ⋮ Quadratic optimal control in reorienting a spacecraft in a fixed time period in a dynamic problem statement ⋮ Special control regime in the problem of optimal turn of an axially symmetric spacecraft ⋮ Optimal control of the reorientation of a spacecraft in the given time with a quadratic performance criterion related to the control and phase variables ⋮ Optimal control of the angular momentum for a solid (spacecraft) performing a spatial turn ⋮ Optimal control of a spacecraft orientation taking into account the energy of rotation ⋮ Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions ⋮ On improving the maneuverability of a space vehicle managed by inertial executive bodies ⋮ 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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