Analytical approximate solution of the problem of a spacecraft's optimal turn with arbitrary boundary conditions
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Publication:499123
DOI10.1134/S1064230715030144zbMath1367.70056OpenAlexW974453311MaRDI QIDQ499123
A. V. Molodenkov, Ya. G. Sapunkov
Publication date: 30 September 2015
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1134/s1064230715030144
Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Control problems involving ordinary differential equations (34H05)
Related Items (8)
Optimal orientation control of a space vehicle with restrictions on the control and phase variables ⋮ Control of the rotation of a solid (spacecraft) with a combined optimality criterion based on quaternions ⋮ 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 ⋮ Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions ⋮ Analytical quasi-optimal solution of the problem of the time-optimal rotation of a spacecraft ⋮ Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions ⋮ Optimal control of rigid body's rotation movement with a combined quality criterion
Cites Work
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- 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
- A shooting method for solving two-point boundary-value problems arising from non-singular bang-bang optimal control problems
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