Optimal magnetic momentum control for inertially pointing spacecraft

DOI10.1016/S0947-3580(01)70936-3zbMath1293.49085OpenAlexW2023196811MaRDI QIDQ2512130

Lovera, Marco

Publication date: 7 August 2014

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

Full work available at URL: https://doi.org/10.1016/s0947-3580(01)70936-3

zbMATH Keywords

optimal controlperiodic controlattitude controlmomentum management

Mathematics Subject Classification ID

(H^infty)-control (93B36) Variable mass, rockets (70P05) Linear-quadratic optimal control problems (49N10)

Related Items (5)

Robust \(\mathcal H_2\) performance analysis and synthesis of linear polytopic discrete-time periodic systems via LMIs ⋮ A projection-based controller for fast spacecraft detumbling using magnetic actuation ⋮ Optimal magnetic momentum control for inertially pointing spacecraft ⋮ Attitude control of rigid spacecraft with disturbance generated by time varying exosystems ⋮ Schemes of momentum/reaction wheels unloading by mechanical restructuring and gearbox for spacecraft

Cites Work

• Unnamed Item
• Unnamed Item
• The Riccati equation
• Fully magnetic attitude control for spacecraft subject to gravity gradient
• Optimal magnetic momentum control for inertially pointing spacecraft
• Active Magnetic Damping Attitude Control for Gravity Gradient Stabilized Spacecraft
• Lyapunov and Riccati equations: Periodic inertia theorems
• Orbit-averaged behavior of magnetic control laws for momentum unloading
• The attitude control problem
• Adaptive control applied to momentum unloading using the low earth orbital environment

This page was built for publication: Optimal magnetic momentum control for inertially pointing spacecraft