Special control mode in the problem of optimal turn of an arbitrary rigid body (spacecraft)

DOI10.1134/S1064230712010121zbMath1311.49106OpenAlexW2121834521MaRDI QIDQ2263415

A. V. Molodenkov, Ya. G. Sapunkov

Publication date: 18 March 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/s1064230712010121

zbMATH Keywords

angular velocityspacecraftangular positionoptimal turn

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (3)

Analytical approximate solution of the problem of a spacecraft's optimal turn with arbitrary boundary conditions ⋮ Analytical solution of a linear quadratic optimal control problem with control value constraints ⋮ Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions

Cites Work

• Special control regime in optimal turn problem of spherically symmetric spacecraft
• Special control regime in the problem of optimal turn of an axially symmetric spacecraft
• A shooting method for solving two-point boundary-value problems arising from non-singular bang-bang optimal control problems
• Unnamed Item

This page was built for publication: Special control mode in the problem of optimal turn of an arbitrary rigid body (spacecraft)