Line-of-sight based spacecraft attitude and position tracking control

DOI10.1016/J.EJCON.2016.04.001zbMath1355.93024OpenAlexW2333915945MaRDI QIDQ508375

Rakesh R. Warier, Arpita Sinha, Srikant Sukumar

Publication date: 10 February 2017

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

Full work available at URL: https://doi.org/10.1016/j.ejcon.2016.04.001

zbMATH Keywords

spacecraft formation flyingcoordinate-free attitude controlline-of-sight based controlspacecraft attitude control

Mathematics Subject Classification ID

Feedback control (93B52) Variable mass, rockets (70P05) Decentralized systems (93A14) Asymptotic stability in control theory (93D20)

Related Items (4)

Particular extremals in the optimal control problems of the reorientation of an asymmetric rotating body ⋮ Line-of-sight based spacecraft attitude and position tracking control ⋮ Velocity-free spacecraft attitude stabilization using two control torques ⋮ Finite time stable attitude estimation of rigid bodies with unknown dynamics

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item
• Almost global attitude stabilization of a rigid body for both internal and external actuation schemes
• Line-of-sight based spacecraft attitude and position tracking control
• Stable synchronization of rigid body networks
• Autonomous rigid body attitude synchronization
• Nonlinear oscillations, dynamical systems, and bifurcations of vector fields
• Tracking for fully actuated mechanical systems: A geometric framework
• Three-axis attitude determination from vector observations
• Synchronization with Partial State Coupling on $SO(n)$
• Inertial Vector Measurements Based Velocity-Free Attitude Stabilization
• A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon

This page was built for publication: Line-of-sight based spacecraft attitude and position tracking control