Title :
Invariant poles feedback control of flexible highly variable spacecraft
Author_Institution :
McDonnell Douglas Astronautics Company, Huntington Beach, CA, USA
fDate :
12/1/1972 12:00:00 AM
Abstract :
This paper describes a technique for single-axis control of a model of a highly flexible Space Station. Active damping of lower frequency flexibility modes is employed. In the control technique, referred to as invariant poles feedback control (IPFC), feedback gains are adjusted so that the closed-loop system characteristic.
Keywords :
Adaptive control; Pole assignment; Space-vehicle control; Actuators; Control systems; Damping; Equations; Feedback control; Filtering; Frequency; NASA; Space stations; Space vehicles;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.1972.1100161
