On improving the maneuverability of a space vehicle managed by inertial executive bodies

DOI10.1134/S1064230720020094zbMath1458.93186OpenAlexW3091772202MaRDI QIDQ1995363

M. V. Levskii

Publication date: 23 February 2021

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230720020094

Mathematics Subject Classification ID

Application models in control theory (93C95) Free motion of a rigid body (70E15)

Related Items (2)

The optimal in terms of fuel consumption approach to reorientation of a spacecraft based on the nonlinear boundary value problem solution ⋮ Optimal control of the reorientation of a spacecraft in the given time with a quadratic performance criterion related to the control and phase variables

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item
• On optimal spacecraft damping
• Synthesis of spacecraft reorientation algorithms using the concept of the inverse dynamic problem
• Threshold absolute value of a relay control when time-optimally bringing a satellite to a gravitationally stable position
• Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions
• A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
• Special control regime in optimal turn problem of spherically symmetric spacecraft

This page was built for publication: On improving the maneuverability of a space vehicle managed by inertial executive bodies