Mass property estimation for control of asymmetrical satellites

DOI10.2514/3.20243zbMath0629.93065OpenAlexW2092483578MaRDI QIDQ3767230

Bruce K. Walker, D. R. Levy, E. V. Bergmann

Publication date: 1987

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.20243

zbMATH Keywords

rate of convergenceKalman filterspacecraft controlstochastic estimationsecond-order filtercenter-of-mass location vectorinverse inertia matrixmass-property parametersReal-time algorithms

Mathematics Subject Classification ID

Filtering in stochastic control theory (93E11) Nonlinear systems in control theory (93C10) Adaptive control/observation systems (93C40) Estimation and detection in stochastic control theory (93E10) Identification in stochastic control theory (93E12) Orbital mechanics (70M20)

Related Items (3)

Identification of the inertia matrix of a rotating body based on errors-in-variables models ⋮ Application of discrete time sliding mode control to a spacecraft in 6DoF with parameter identification ⋮ Rigid body inertia estimation using extended Kalman and Savitzky-Golay filters

This page was built for publication: Mass property estimation for control of asymmetrical satellites