A model reference adaptive control law is presented for large angle rotational maneuvers of spacecraft using reaction jets. It is assumed that the various parameters of the spacecraft are completely unknown, and unknown but bounded disturbance torques are acting on the spacecraft. The controller includes a dynamic system in the feedback path. Simulation results are presented to show that fast, large angle rotational maneuvers can be performed using the adaptive controller in spite of uncertainty in the system.
Nonlinear adaptive attitude control of spacecraft
1987-05-01
Miscellaneous
No indication
English
Nonlinear adaptive attitude control of spacecraft
Tema Archive | 1987
|Nonlinear Adaptive Attitude Control of Spacecraft
IEEE | 1987
|Adaptive Nonlinear Attitude Control and Momentum Management of Spacecraft
Online Contents | 1997
|Nonlinear Attitude Control for Spacecraft
Trans Tech Publications | 2013
|Nonlinear Adaptive Spacecraft Attitude Control using Solar Radiation Pressure
Online Contents | 2005
|