NONLINEAR FEEDBACK CONTROL OF SPACECRAFT SLEW MANEUVERS.
- Additional Document Info
- View All
A polynomial feedback control law for large-angle attitude maneuvers is presented, with a recursive algorithm for calculating the control gains. By formulating the kinematics in terms of Euler parameters, low-order nonlinear controls are found to be adequate, and single- and three-axis maneuvers are demonstrated.
author list (cited authors)
Carrington, C. K., & Junkins, J. L.