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Izvestiya of Saratov University.
Mathematics. Mechanics. Informatics
ISSN 18169791 (Print)
ISSN 25419005 (Online)
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оптимальное управление
On renormalization of the approximate solution of the orbital coordinate system equations of orientation
Optimal solution in the model of control over an economic system in the condition of a mass disease
The new algorithm of quasioptimal reorientation of a spacecraft
Approximation of the orientation equations of the orbital coordinate system by the weighted residuals method
The problem of optimal control for singularly perturbed system with delay with integral quadratic constraints
Determination of the Boundary in the Local Charzynski–Tammi Conjecture for the Fifth Coefficient
About a problem of spacecraft's orbit optimal reorientation
Using Galerkin Method for Solving Linear Optimal Control Problems
Analytical Solution of Equations of Nearcircular Spacecraft’s Orbit Orientation
Solution of a Problem of Spacecraft’s Orbit Optimal Reorientation Using Quaternion Equations of Orbital System of Coordinates Orientation
Approximation of Control for Singularly Perturbed System with Delay with Geometric Constraints
Global Improvement Method for Hamiltonian Systems with Controllable Coefficients
Solving Kinematic Problem of Optimal Nonlinear Stabilization of Arbitrary Program Movement of Free Rigid Body
Iterative Procedure of Constructing Optimal Solving in the Minimax Problem of Control for Singularly Perturbed System with Delay with Geometric Constraints
Investigation of the Problem of Optimal Correction of Angular Elements of the Spacecraft Orbit Using Quaternion Differential Equation of Orbit Orientation
On Iterative Method of Constructing Optimal Control for Singularly Perturbed Systems with Delay
Approximate Solution of an Optimal Control Problem with Linear Nonhomogeneous Control System in Hilbert Space
On Iterative Method of Constructing Optimal Control for Singularly Perturbed Systems with Delay with Quadratic Constraints
Analytical Solution of Differential Equations of Circular Spacecraft Orbit Orientation
Applicathion the Pontryagin‘s Maximum Principle to Optimal Economics Models
Approximation of Control for Singularly Perturbed System with Delay with Integral Quadratic Constraints
Quaternion Models and Algorithms for Solving the General Problem of Optimal Reorientation of Spacecraft Orbit
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