Time-optimal reorientation for rigid satellite with reaction wheels

DOI10.1080/00207179.2012.688873zbMath1255.49069OpenAlexW2162770377MaRDI QIDQ4897711

Eng Kee Poh, Baolin Wu, Hao Zhou, Wang, Danwei

Publication date: 27 December 2012

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207179.2012.688873

zbMATH Keywords

optimal controlpseudospectral methodsatellite attitude controlreaction wheels

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90)

Related Items (7)

Switching time-optimal control of spacecraft equipped with reaction wheels and gas jet thrusters ⋮ 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 ⋮ Robust ℋ₂ controller with parametric uncertainties applied to a reaction wheel unicycle ⋮ Gradient method using pseudospectral collocation scheme for two-stage optimal control with an unspecified switching time ⋮ Optimal integral sliding mode control scheme based on pseudospectral method for robotic manipulators

Cites Work

• Minimal energy maneuvering control of a rigid spacecraft with momentum transfer
• The attitude control problem
• Fuel/Time Optimal Control of Spacecraft Maneuvers
• The pseudospectral Legendre method for discretizing optimal control problems

This page was built for publication: Time-optimal reorientation for rigid satellite with reaction wheels