Feedback control for slew maneuver using on-off thrusters

Citation
H. Bang et al., Feedback control for slew maneuver using on-off thrusters, J GUID CON, 22(6), 1999, pp. 816-822
Citations number
24
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
ISSN journal
07315090 → ACNP
Volume
22
Issue
6
Year of publication
1999
Pages
816 - 822
Database
ISI
SICI code
0731-5090(199911/12)22:6<816:FCFSMU>2.0.ZU;2-I
Abstract
A new output-feedback control approach for the single-axis rotational maneu ver of a flexible structure by use of on-off thrusters is discussed. The ta rget Structural model represents a large-space-structure type with relative ly low natural frequencies. The large overshoot induced by phase error of t he applied torque input is minimized by the new control law. The thruster o utput is modulated in pulse width so that the output profile is similar to continuously smoothed control histories. The main idea of the new controlle r is based on a dosed-loop switching function that is constructed from a ne ar-minimum-time output-feedback tracking control law. The preposed control law has advantages of robustness as an output-feedback law as web as enhanc ed performance for the slew maneuver of flexible structures by use of on-of f actuators.