Publication Date:
2019-07-13
Description:
Preliminary results on the design of decentralized controllers for the COFS I Mast are reported. A nine mode finite element model is used along with second order model of the actuators. It is shown that without actuator dynamics, the system is stable with collocated rate feedback and has acceptable performace. However, when actuator dynamics are included, the system is unstable.
Keywords:
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Type:
1987 American Control Conference; Jun 10, 1987 - Jun 12, 1987; Minneapolis, MN; United States
Format:
text
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