Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft
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Publication:734154
DOI10.1134/S1064230708060117zbMath1173.49018MaRDI QIDQ734154
Publication date: 19 October 2009
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)
Related Items (17)
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 ⋮ On optimal spacecraft damping ⋮ A special case of spacecraft optimal attitude control ⋮ 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 ⋮ Optimal control of a spacecraft orientation taking into account the energy of rotation ⋮ Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional ⋮ On the problem of optimal spacecraft attitude control ⋮ Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions ⋮ Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions ⋮ Kinematically optimal spacecraft attitude control ⋮ Restricted quadratic optimal control of a spacecraft turning in a fixed time period ⋮ Optimal control of rigid body's rotation movement with a combined quality criterion ⋮ Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality ⋮ Analytical quasi-optimal solution of the slew problem for an axially symmetric rigid body with a combined performance index
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